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The Jenkins Controller is preparing for shutdown. No new builds can be started.
Started by upstream project "ESP_Beta" build number 710 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/7.7/DARWIN_ARM64 [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] Done Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64 Cleaning local Directory . Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-04-27T17:47:59.928 -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 2480 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP doesn't exist Cleaning local Directory JenkinsESP Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-04-27T17:47:59.928 -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 857 No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [viggen] is in [[macys, macys_VM, 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/jenkins4617548200937919840.sh + arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/ESP_Beta.sh + source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/ESP_Env.sh ++ export OCCTREF=7.6 ++ OCCTREF=7.6 ++ AFLR_VERSION=11.5.14 ++ SU2_VERSION=8.0.0 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.34.0 ++ export PYTHON_VERSION=3.11.6 ++ PYTHON_VERSION=3.11.6 ++ 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/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.6 != '' ]] ++ [[ '' != '' ]] ++ [[ viggen == *\r\e\y\n\o\l\d\s* ]] ++ [[ viggen == *\m\a\c\y\s* ]] ++ [[ viggen == *\v\i\g\g\e\n* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile ++++ /opt/homebrew/bin/brew shellenv +++ eval 'export HOMEBREW_PREFIX="/opt/homebrew"; export HOMEBREW_CELLAR="/opt/homebrew/Cellar"; export HOMEBREW_REPOSITORY="/opt/homebrew"; export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}"; export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:"; export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";' ++++ export HOMEBREW_PREFIX=/opt/homebrew ++++ HOMEBREW_PREFIX=/opt/homebrew ++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ export HOMEBREW_REPOSITORY=/opt/homebrew ++++ HOMEBREW_REPOSITORY=/opt/homebrew ++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ export MANPATH=/opt/homebrew/share/man: ++++ MANPATH=/opt/homebrew/share/man: ++++ export INFOPATH=/opt/homebrew/share/info: ++++ INFOPATH=/opt/homebrew/share/info: +++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]] +++ . /opt/homebrew/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export NETCDF_PATH=/opt/homebrew +++ NETCDF_PATH=/opt/homebrew ++ [[ viggen == *\m\a\c\y\s* ]] ++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/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/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/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-3.34.0-MacOS ++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export SEACAS=/Users/jenkins/util/sandialabs/seacas ++ SEACAS=/Users/jenkins/util/sandialabs/seacas ++ [[ viggen == \v\i\g\g\e\n ]] ++ export NETCDFINC=/opt/homebrew/include ++ NETCDFINC=/opt/homebrew/include ++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' +++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl ++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH; PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB; PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT; PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT; PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;' +++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 +++ export PERL5LIB +++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_LOCAL_LIB_ROOT +++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"' +++ export PERL_MB_OPT +++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_MM_OPT ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/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-3.11.6/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv +++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-cc +++ python-config --includes ++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11' ++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_Beta/7.7/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-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.6 ++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/data + virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv created virtual environment CPython3.11.6.final.0-64 in 211ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/ESP_venv/bin/activate ++ '[' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/ESP_venv ++ '[' darwin23 = cygwin ']' ++ '[' darwin23 = msys ']' ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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) Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB) 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/7.7/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 --2024-04-27 17:48:26-- 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. 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42.3M 5s 12900K .......... .......... .......... .......... .......... 4% 46.9M 5s 12950K .......... .......... .......... .......... .......... 4% 44.8M 5s 13000K .......... .......... .......... .......... .......... 4% 47.0M 5s 13050K .......... .......... .......... .......... .......... 4% 29.3M 5s 13100K .......... .......... .......... .......... .......... 5% 34.7M 5s 13150K .......... .......... .......... .......... .......... 5% 21.6M 5s 13200K .......... .......... .......... .......... .......... 5% 282M 5s 13250K .......... .......... .......... .......... .......... 5% 15.4M 5s 13300K .......... .......... .......... .......... .......... 5% 364M 5s 13350K .......... .......... .......... .......... .......... 5% 53.5M 5s 13400K .......... .......... .......... .......... .......... 5% 79.5M 5s 13450K .......... .......... .......... .......... .......... 5% 28.0M 5s 13500K .......... .......... .......... .......... .......... 5% 47.5M 5s 13550K .......... .......... 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5s 15600K .......... .......... .......... .......... .......... 5% 54.2M 5s 15650K .......... .......... .......... .......... .......... 5% 63.5M 5s 15700K .......... .......... .......... .......... .......... 6% 60.5M 5s 15750K .......... .......... .......... .......... .......... 6% 56.2M 5s 15800K .......... .......... .......... .......... .......... 6% 61.6M 5s 15850K .......... .......... .......... .......... .......... 6% 57.4M 5s 15900K .......... .......... .......... .......... .......... 6% 59.6M 5s 15950K .......... .......... .......... .......... .......... 6% 53.8M 5s 16000K .......... .......... .......... .......... .......... 6% 53.7M 5s 16050K .......... .......... .......... .......... .......... 6% 168M 5s 16100K .......... .......... .......... .......... .......... 6% 46.2M 5s 16150K .......... .......... .......... .......... .......... 6% 57.7M 5s 16200K .......... .......... .......... .......... .......... 6% 48.5M 5s 16250K .......... .......... 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5s 18300K .......... .......... .......... .......... .......... 6% 63.2M 5s 18350K .......... .......... .......... .......... .......... 7% 61.3M 5s 18400K .......... .......... .......... .......... .......... 7% 65.3M 5s 18450K .......... .......... .......... .......... .......... 7% 52.8M 5s 18500K .......... .......... .......... .......... .......... 7% 95.7M 5s 18550K .......... .......... .......... .......... .......... 7% 64.8M 5s 18600K .......... .......... .......... .......... .......... 7% 61.4M 5s 18650K .......... .......... .......... .......... .......... 7% 64.8M 5s 18700K .......... .......... .......... .......... .......... 7% 92.1M 5s 18750K .......... .......... .......... .......... .......... 7% 55.2M 5s 18800K .......... .......... .......... .......... .......... 7% 91.1M 5s 18850K .......... .......... .......... .......... .......... 7% 55.9M 5s 18900K .......... .......... .......... .......... .......... 7% 62.8M 5s 18950K .......... .......... 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.......... .......... .......... 9% 48.2M 4s 25750K .......... .......... .......... .......... .......... 9% 62.0M 4s 25800K .......... .......... .......... .......... .......... 9% 62.7M 4s 25850K .......... .......... .......... .......... .......... 9% 54.3M 4s 25900K .......... .......... .......... .......... .......... 9% 64.5M 4s 25950K .......... .......... .......... .......... .......... 9% 93.7M 4s 26000K .......... .......... .......... .......... .......... 9% 72.4M 4s 26050K .......... .......... .......... .......... .......... 9% 92.1M 4s 26100K .......... .......... .......... .......... .......... 9% 91.3M 4s 26150K .......... .......... .......... .......... .......... 9% 21.7M 4s 26200K .......... .......... .......... .......... .......... 10% 202M 4s 26250K .......... .......... .......... .......... .......... 10% 209M 4s 26300K .......... .......... .......... .......... .......... 10% 346M 4s 26350K .......... .......... .......... .......... .......... 10% 34.1M 4s 26400K .......... .......... .......... .......... .......... 10% 159M 4s 26450K .......... .......... .......... .......... .......... 10% 157M 4s 26500K .......... .......... .......... .......... .......... 10% 76.2M 4s 26550K .......... .......... .......... .......... .......... 10% 37.2M 4s 26600K .......... .......... .......... .......... .......... 10% 245M 4s 26650K .......... .......... .......... .......... .......... 10% 337M 4s 26700K .......... .......... .......... .......... .......... 10% 321M 4s 26750K .......... .......... .......... .......... .......... 10% 143M 4s 26800K .......... .......... .......... .......... .......... 10% 63.0M 4s 26850K .......... .......... .......... .......... .......... 10% 63.2M 4s 26900K .......... .......... .......... .......... .......... 10% 55.3M 4s 26950K .......... .......... .......... .......... .......... 10% 109M 4s 27000K .......... .......... .......... .......... .......... 10% 55.9M 4s 27050K .......... .......... .......... .......... .......... 10% 65.8M 4s 27100K .......... .......... .......... .......... .......... 10% 73.0M 4s 27150K .......... .......... .......... .......... .......... 10% 90.9M 4s 27200K .......... .......... .......... .......... .......... 10% 55.0M 4s 27250K .......... .......... .......... .......... .......... 10% 57.4M 4s 27300K .......... .......... .......... .......... .......... 10% 78.6M 4s 27350K .......... .......... .......... .......... .......... 10% 52.8M 4s 27400K .......... .......... .......... .......... .......... 10% 78.6M 4s 27450K .......... .......... .......... .......... .......... 10% 72.0M 4s 27500K .......... .......... .......... .......... .......... 10% 54.4M 4s 27550K .......... .......... .......... .......... .......... 10% 72.3M 4s 27600K .......... .......... .......... .......... .......... 10% 93.7M 4s 27650K .......... .......... .......... .......... .......... 10% 63.7M 4s 27700K .......... .......... .......... .......... .......... 10% 56.1M 4s 27750K .......... .......... .......... .......... .......... 10% 74.5M 4s 27800K .......... .......... .......... .......... .......... 10% 97.1M 4s 27850K .......... .......... .......... .......... .......... 10% 61.2M 4s 27900K .......... .......... .......... .......... .......... 10% 65.2M 4s 27950K .......... .......... .......... .......... .......... 10% 61.1M 4s 28000K .......... .......... .......... .......... .......... 10% 98.2M 4s 28050K .......... .......... .......... .......... .......... 10% 75.5M 4s 28100K .......... .......... .......... .......... .......... 10% 61.1M 4s 28150K .......... .......... .......... .......... .......... 10% 65.2M 4s 28200K .......... .......... .......... .......... .......... 10% 61.2M 4s 28250K .......... .......... .......... .......... .......... 10% 94.3M 4s 28300K .......... .......... .......... .......... .......... 10% 65.5M 4s 28350K .......... .......... .......... .......... .......... 10% 53.6M 4s 28400K .......... .......... .......... .......... .......... 10% 76.2M 4s 28450K .......... .......... .......... .......... .......... 10% 58.5M 4s 28500K .......... .......... .......... .......... .......... 10% 75.0M 4s 28550K .......... .......... .......... .......... .......... 10% 79.1M 4s 28600K .......... .......... .......... .......... .......... 10% 54.1M 4s 28650K .......... .......... .......... .......... .......... 10% 75.9M 4s 28700K .......... .......... .......... .......... .......... 10% 90.6M 4s 28750K .......... .......... .......... .......... .......... 10% 55.4M 4s 28800K .......... .......... .......... .......... .......... 11% 75.1M 4s 28850K .......... .......... .......... .......... .......... 11% 62.0M 4s 28900K .......... .......... .......... .......... .......... 11% 65.5M 4s 28950K .......... .......... .......... .......... .......... 11% 90.9M 4s 29000K .......... .......... .......... .......... .......... 11% 63.8M 4s 29050K .......... .......... .......... .......... .......... 11% 63.6M 4s 29100K .......... .......... .......... .......... .......... 11% 54.6M 4s 29150K .......... .......... .......... .......... .......... 11% 75.4M 4s 29200K .......... .......... .......... .......... .......... 11% 51.9M 4s 29250K .......... .......... .......... .......... .......... 11% 79.9M 4s 29300K .......... .......... .......... .......... .......... 11% 63.0M 4s 29350K .......... .......... .......... .......... .......... 11% 90.9M 4s 29400K .......... .......... .......... .......... .......... 11% 59.9M 4s 29450K .......... .......... .......... .......... .......... 11% 13.9M 4s 29500K .......... .......... .......... .......... .......... 11% 284M 4s 29550K .......... .......... .......... .......... .......... 11% 328M 4s 29600K .......... .......... .......... .......... .......... 11% 203M 4s 29650K .......... .......... .......... .......... .......... 11% 171M 4s 29700K .......... .......... .......... .......... .......... 11% 219M 4s 29750K .......... .......... .......... .......... .......... 11% 421M 4s 29800K .......... .......... .......... .......... .......... 11% 33.3M 4s 29850K .......... .......... .......... .......... .......... 11% 180M 4s 29900K .......... .......... .......... .......... .......... 11% 47.0M 4s 29950K .......... .......... .......... .......... .......... 11% 184M 4s 30000K .......... .......... .......... .......... .......... 11% 56.4M 4s 30050K .......... .......... .......... .......... .......... 11% 52.3M 4s 30100K .......... .......... .......... .......... .......... 11% 52.1M 4s 30150K .......... .......... .......... .......... .......... 11% 51.9M 4s 30200K .......... .......... .......... .......... .......... 11% 51.5M 4s 30250K .......... .......... .......... .......... .......... 11% 127M 4s 30300K .......... .......... .......... .......... .......... 11% 52.8M 4s 30350K .......... .......... .......... .......... .......... 11% 52.4M 4s 30400K .......... .......... .......... .......... .......... 11% 54.4M 4s 30450K .......... .......... .......... .......... .......... 11% 48.3M 4s 30500K .......... .......... .......... .......... .......... 11% 54.4M 4s 30550K .......... .......... .......... .......... .......... 11% 117M 4s 30600K .......... .......... .......... .......... .......... 11% 48.5M 4s 30650K .......... .......... .......... .......... .......... 11% 58.6M 4s 30700K .......... .......... .......... .......... .......... 11% 50.6M 4s 30750K .......... .......... .......... .......... .......... 11% 53.4M 4s 30800K .......... .......... .......... .......... .......... 11% 61.0M 4s 30850K .......... .......... .......... .......... .......... 11% 47.7M 4s 30900K .......... .......... .......... .......... .......... 11% 51.8M 4s 30950K .......... .......... .......... .......... .......... 11% 59.3M 4s 31000K .......... .......... .......... .......... .......... 11% 98.8M 4s 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.......... .......... .......... .......... 15% 23.5M 4s 39750K .......... .......... .......... .......... .......... 15% 29.9M 4s 39800K .......... .......... .......... .......... .......... 15% 26.0M 4s 39850K .......... .......... .......... .......... .......... 15% 20.7M 4s 39900K .......... .......... .......... .......... .......... 15% 42.3M 4s 39950K .......... .......... .......... .......... .......... 15% 20.9M 4s 40000K .......... .......... .......... .......... .......... 15% 29.0M 4s 40050K .......... .......... .......... .......... .......... 15% 38.9M 4s 40100K .......... .......... .......... .......... .......... 15% 13.0M 4s 40150K .......... .......... .......... .......... .......... 15% 388M 4s 40200K .......... .......... .......... .......... .......... 15% 35.7M 4s 40250K .......... .......... .......... .......... .......... 15% 35.1M 4s 40300K .......... .......... .......... .......... .......... 15% 50.4M 4s 40350K .......... .......... .......... 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46.0M 4s 41050K .......... .......... .......... .......... .......... 15% 28.1M 4s 41100K .......... .......... .......... .......... .......... 15% 26.1M 4s 41150K .......... .......... .......... .......... .......... 15% 31.3M 4s 41200K .......... .......... .......... .......... .......... 15% 47.5M 4s 41250K .......... .......... .......... .......... .......... 15% 26.6M 4s 41300K .......... .......... .......... .......... .......... 15% 27.2M 4s 41350K .......... .......... .......... .......... .......... 15% 28.9M 4s 41400K .......... .......... .......... .......... .......... 15% 39.2M 4s 41450K .......... .......... .......... .......... .......... 15% 29.3M 4s 41500K .......... .......... .......... .......... .......... 15% 15.9M 4s 41550K .......... .......... .......... .......... .......... 15% 315M 4s 41600K .......... .......... .......... .......... .......... 15% 24.3M 4s 41650K .......... .......... .......... .......... .......... 15% 38.8M 4s 41700K .......... .......... .......... .......... .......... 15% 31.0M 4s 41750K .......... .......... .......... .......... .......... 15% 265M 4s 41800K .......... .......... .......... .......... .......... 15% 31.2M 4s 41850K .......... .......... .......... .......... .......... 15% 34.6M 4s 41900K .......... .......... .......... .......... .......... 15% 41.1M 4s 41950K .......... .......... .......... .......... .......... 16% 31.6M 4s 42000K .......... .......... .......... .......... .......... 16% 45.7M 4s 42050K .......... .......... .......... .......... .......... 16% 32.2M 4s 42100K .......... .......... .......... .......... .......... 16% 46.3M 4s 42150K .......... .......... .......... .......... .......... 16% 27.0M 4s 42200K .......... .......... .......... .......... .......... 16% 34.1M 4s 42250K .......... .......... .......... .......... .......... 16% 41.4M 4s 42300K .......... .......... .......... .......... .......... 16% 35.8M 4s 42350K .......... .......... .......... 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49.4M 4s 43050K .......... .......... .......... .......... .......... 16% 58.3M 4s 43100K .......... .......... .......... .......... .......... 16% 80.6M 4s 43150K .......... .......... .......... .......... .......... 16% 19.9M 4s 43200K .......... .......... .......... .......... .......... 16% 287M 4s 43250K .......... .......... .......... .......... .......... 16% 330M 4s 43300K .......... .......... .......... .......... .......... 16% 79.0M 4s 43350K .......... .......... .......... .......... .......... 16% 46.6M 4s 43400K .......... .......... .......... .......... .......... 16% 282M 4s 43450K .......... .......... .......... .......... .......... 16% 70.2M 4s 43500K .......... .......... .......... .......... .......... 16% 303M 4s 43550K .......... .......... .......... .......... .......... 16% 147M 4s 43600K .......... .......... .......... .......... .......... 16% 53.4M 4s 43650K .......... .......... .......... .......... .......... 16% 62.4M 4s 43700K .......... 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64.0M 4s 45050K .......... .......... .......... .......... .......... 17% 73.1M 4s 45100K .......... .......... .......... .......... .......... 17% 78.1M 4s 45150K .......... .......... .......... .......... .......... 17% 77.9M 4s 45200K .......... .......... .......... .......... .......... 17% 53.5M 4s 45250K .......... .......... .......... .......... .......... 17% 100M 4s 45300K .......... .......... .......... .......... .......... 17% 65.7M 4s 45350K .......... .......... .......... .......... .......... 17% 61.5M 4s 45400K .......... .......... .......... .......... .......... 17% 64.7M 4s 45450K .......... .......... .......... .......... .......... 17% 61.5M 4s 45500K .......... .......... .......... .......... .......... 17% 63.4M 4s 45550K .......... .......... .......... .......... .......... 17% 124M 4s 45600K .......... .......... .......... .......... .......... 17% 55.6M 4s 45650K .......... .......... .......... .......... .......... 17% 60.7M 4s 45700K .......... 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168M 4s 47050K .......... .......... .......... .......... .......... 17% 56.4M 4s 47100K .......... .......... .......... .......... .......... 17% 330M 4s 47150K .......... .......... .......... .......... .......... 18% 204M 4s 47200K .......... .......... .......... .......... .......... 18% 43.9M 4s 47250K .......... .......... .......... .......... .......... 18% 171M 4s 47300K .......... .......... .......... .......... .......... 18% 61.1M 4s 47350K .......... .......... .......... .......... .......... 18% 55.3M 4s 47400K .......... .......... .......... .......... .......... 18% 58.3M 4s 47450K .......... .......... .......... .......... .......... 18% 98.4M 4s 47500K .......... .......... .......... .......... .......... 18% 57.2M 4s 47550K .......... .......... .......... .......... .......... 18% 98.2M 4s 47600K .......... .......... .......... .......... .......... 18% 29.4M 4s 47650K .......... .......... .......... .......... .......... 18% 404M 4s 47700K .......... 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53700K .......... .......... .......... .......... .......... 20% 55.2M 4s 53750K .......... .......... .......... .......... .......... 20% 61.6M 4s 53800K .......... .......... .......... .......... .......... 20% 63.3M 4s 53850K .......... .......... .......... .......... .......... 20% 49.6M 4s 53900K .......... .......... .......... .......... .......... 20% 55.5M 4s 53950K .......... .......... .......... .......... .......... 20% 62.6M 4s 54000K .......... .......... .......... .......... .......... 20% 96.1M 4s 54050K .......... .......... .......... .......... .......... 20% 62.4M 4s 54100K .......... .......... .......... .......... .......... 20% 54.4M 4s 54150K .......... .......... .......... .......... .......... 20% 62.6M 4s 54200K .......... .......... .......... .......... .......... 20% 55.5M 4s 54250K .......... .......... .......... .......... .......... 20% 120M 4s 54300K .......... .......... .......... .......... .......... 20% 63.4M 4s 54350K .......... 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54.1M 4s 69000K .......... .......... .......... .......... .......... 26% 61.3M 4s 69050K .......... .......... .......... .......... .......... 26% 52.9M 4s 69100K .......... .......... .......... .......... .......... 26% 54.4M 4s 69150K .......... .......... .......... .......... .......... 26% 53.7M 4s 69200K .......... .......... .......... .......... .......... 26% 54.4M 4s 69250K .......... .......... .......... .......... .......... 26% 127M 4s 69300K .......... .......... .......... .......... .......... 26% 53.3M 4s 69350K .......... .......... .......... .......... .......... 26% 54.3M 4s 69400K .......... .......... .......... .......... .......... 26% 63.2M 4s 69450K .......... .......... .......... .......... .......... 26% 53.4M 4s 69500K .......... .......... .......... .......... .......... 26% 54.8M 4s 69550K .......... .......... .......... .......... .......... 26% 63.0M 4s 69600K .......... .......... .......... .......... .......... 26% 61.7M 4s 69650K .......... 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71000K .......... .......... .......... .......... .......... 27% 53.0M 4s 71050K .......... .......... .......... .......... .......... 27% 44.9M 4s 71100K .......... .......... .......... .......... .......... 27% 53.8M 4s 71150K .......... .......... .......... .......... .......... 27% 53.1M 4s 71200K .......... .......... .......... .......... .......... 27% 58.1M 4s 71250K .......... .......... .......... .......... .......... 27% 53.5M 4s 71300K .......... .......... .......... .......... .......... 27% 55.8M 4s 71350K .......... .......... .......... .......... .......... 27% 53.3M 4s 71400K .......... .......... .......... .......... .......... 27% 54.6M 4s 71450K .......... .......... .......... .......... .......... 27% 38.5M 4s 71500K .......... .......... .......... .......... .......... 27% 63.8M 4s 71550K .......... .......... .......... .......... .......... 27% 48.0M 4s 71600K .......... .......... .......... .......... .......... 27% 48.0M 4s 71650K .......... 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94.8M 4s 73000K .......... .......... .......... .......... .......... 27% 13.8M 4s 73050K .......... .......... .......... .......... .......... 27% 537M 4s 73100K .......... .......... .......... .......... .......... 27% 509M 4s 73150K .......... .......... .......... .......... .......... 27% 444M 4s 73200K .......... .......... .......... .......... .......... 27% 22.0M 4s 73250K .......... .......... .......... .......... .......... 27% 525M 4s 73300K .......... .......... .......... .......... .......... 27% 549M 4s 73350K .......... .......... .......... .......... .......... 27% 63.4M 4s 73400K .......... .......... .......... .......... .......... 28% 183M 4s 73450K .......... .......... .......... .......... .......... 28% 71.6M 4s 73500K .......... .......... .......... .......... .......... 28% 231M 4s 73550K .......... .......... .......... .......... .......... 28% 73.8M 4s 73600K .......... .......... .......... .......... .......... 28% 53.0M 4s 73650K .......... 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39.8M 4s 75000K .......... .......... .......... .......... .......... 28% 96.5M 4s 75050K .......... .......... .......... .......... .......... 28% 62.3M 4s 75100K .......... .......... .......... .......... .......... 28% 46.0M 4s 75150K .......... .......... .......... .......... .......... 28% 62.6M 4s 75200K .......... .......... .......... .......... .......... 28% 59.9M 4s 75250K .......... .......... .......... .......... .......... 28% 98.4M 4s 75300K .......... .......... .......... .......... .......... 28% 62.8M 4s 75350K .......... .......... .......... .......... .......... 28% 48.7M 4s 75400K .......... .......... .......... .......... .......... 28% 63.1M 4s 75450K .......... .......... .......... .......... .......... 28% 54.1M 4s 75500K .......... .......... .......... .......... .......... 28% 61.7M 4s 75550K .......... .......... .......... .......... .......... 28% 94.1M 4s 75600K .......... .......... .......... .......... .......... 28% 54.9M 4s 75650K 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.......... 31% 219M 3s 81650K .......... .......... .......... .......... .......... 31% 72.2M 3s 81700K .......... .......... .......... .......... .......... 31% 54.0M 3s 81750K .......... .......... .......... .......... .......... 31% 119M 3s 81800K .......... .......... .......... .......... .......... 31% 53.1M 3s 81850K .......... .......... .......... .......... .......... 31% 53.8M 3s 81900K .......... .......... .......... .......... .......... 31% 50.5M 3s 81950K .......... .......... .......... .......... .......... 31% 42.9M 3s 82000K .......... .......... .......... .......... .......... 31% 61.4M 3s 82050K .......... .......... .......... .......... .......... 31% 52.4M 3s 82100K .......... .......... .......... .......... .......... 31% 53.9M 3s 82150K .......... .......... .......... .......... .......... 31% 54.9M 3s 82200K .......... .......... .......... .......... .......... 31% 54.1M 3s 82250K .......... .......... .......... .......... .......... 31% 54.0M 3s 82300K .......... .......... .......... .......... .......... 31% 62.8M 3s 82350K .......... .......... .......... .......... .......... 31% 54.4M 3s 82400K .......... .......... .......... .......... .......... 31% 62.2M 3s 82450K .......... .......... .......... .......... .......... 31% 53.8M 3s 82500K .......... .......... .......... .......... .......... 31% 47.6M 3s 82550K .......... .......... .......... .......... .......... 31% 54.7M 3s 82600K .......... .......... .......... .......... .......... 31% 53.2M 3s 82650K .......... .......... .......... .......... .......... 31% 54.9M 3s 82700K .......... .......... .......... .......... .......... 31% 45.9M 3s 82750K .......... .......... .......... .......... .......... 31% 61.7M 3s 82800K .......... .......... .......... .......... .......... 31% 54.0M 3s 82850K .......... .......... .......... .......... .......... 31% 46.2M 3s 82900K .......... .......... .......... .......... .......... 31% 47.0M 3s 82950K .......... .......... .......... .......... .......... 31% 45.6M 3s 83000K .......... .......... .......... .......... .......... 31% 54.1M 3s 83050K .......... .......... .......... .......... .......... 31% 74.7M 3s 83100K .......... .......... .......... .......... .......... 31% 46.5M 3s 83150K .......... .......... .......... .......... .......... 31% 52.8M 3s 83200K .......... .......... .......... .......... .......... 31% 52.8M 3s 83250K .......... .......... .......... .......... .......... 31% 54.2M 3s 83300K .......... .......... .......... .......... .......... 31% 55.4M 3s 83350K .......... .......... .......... .......... .......... 31% 42.2M 3s 83400K .......... .......... .......... .......... .......... 31% 54.9M 3s 83450K .......... .......... .......... .......... .......... 31% 47.0M 3s 83500K .......... .......... .......... .......... .......... 31% 132M 3s 83550K .......... .......... .......... .......... .......... 31% 58.7M 3s 83600K .......... .......... .......... .......... .......... 31% 82.3M 3s 83650K .......... .......... .......... .......... .......... 31% 89.8M 3s 83700K .......... .......... .......... .......... .......... 31% 21.1M 3s 83750K .......... .......... .......... .......... .......... 31% 161M 3s 83800K .......... .......... .......... .......... .......... 31% 188M 3s 83850K .......... .......... .......... .......... .......... 31% 121M 3s 83900K .......... .......... .......... .......... .......... 32% 286M 3s 83950K .......... .......... .......... .......... .......... 32% 39.7M 3s 84000K .......... .......... .......... .......... .......... 32% 35.7M 3s 84050K .......... .......... .......... .......... .......... 32% 474M 3s 84100K .......... .......... .......... .......... .......... 32% 448M 3s 84150K .......... .......... .......... .......... .......... 32% 163M 3s 84200K .......... .......... .......... .......... .......... 32% 77.6M 3s 84250K .......... .......... .......... .......... .......... 32% 92.7M 3s 84300K .......... .......... .......... .......... .......... 32% 588M 3s 84350K .......... .......... .......... .......... .......... 32% 90.1M 3s 84400K .......... .......... .......... .......... .......... 32% 74.3M 3s 84450K .......... .......... .......... .......... .......... 32% 64.2M 3s 84500K .......... .......... .......... .......... .......... 32% 78.9M 3s 84550K .......... .......... .......... .......... .......... 32% 74.7M 3s 84600K .......... .......... .......... .......... .......... 32% 55.5M 3s 84650K .......... .......... .......... .......... .......... 32% 63.4M 3s 84700K .......... .......... .......... .......... .......... 32% 89.6M 3s 84750K .......... .......... .......... .......... .......... 32% 55.5M 3s 84800K .......... .......... .......... .......... .......... 32% 73.9M 3s 84850K .......... .......... .......... .......... .......... 32% 63.4M 3s 84900K .......... .......... .......... .......... .......... 32% 75.1M 3s 84950K .......... .......... .......... .......... .......... 32% 60.3M 3s 85000K .......... .......... .......... .......... .......... 32% 58.3M 3s 85050K .......... .......... .......... .......... .......... 32% 94.4M 3s 85100K .......... .......... .......... .......... .......... 32% 52.4M 3s 85150K .......... .......... .......... .......... .......... 32% 79.4M 3s 85200K .......... .......... .......... .......... .......... 32% 63.2M 3s 85250K .......... .......... .......... .......... .......... 32% 64.7M 3s 85300K .......... .......... .......... .......... .......... 32% 89.4M 3s 85350K .......... .......... .......... .......... .......... 32% 59.4M 3s 85400K .......... .......... .......... .......... .......... 32% 65.8M 3s 85450K .......... .......... .......... .......... .......... 32% 63.7M 3s 85500K .......... .......... .......... .......... .......... 32% 90.4M 3s 85550K .......... .......... .......... .......... .......... 32% 64.1M 3s 85600K .......... .......... .......... 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94.3M 3s 86300K .......... .......... .......... .......... .......... 32% 74.1M 3s 86350K .......... .......... .......... .......... .......... 32% 76.1M 3s 86400K .......... .......... .......... .......... .......... 32% 71.1M 3s 86450K .......... .......... .......... .......... .......... 32% 49.1M 3s 86500K .......... .......... .......... .......... .......... 33% 120M 3s 86550K .......... .......... .......... .......... .......... 33% 54.0M 3s 86600K .......... .......... .......... .......... .......... 33% 55.2M 3s 86650K .......... .......... .......... .......... .......... 33% 99.0M 3s 86700K .......... .......... .......... .......... .......... 33% 54.1M 3s 86750K .......... .......... .......... .......... .......... 33% 177M 3s 86800K .......... .......... .......... .......... .......... 33% 54.9M 3s 86850K .......... .......... .......... .......... .......... 33% 93.9M 3s 86900K .......... .......... .......... .......... .......... 33% 52.3M 3s 86950K .......... 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54.2M 3s 88300K .......... .......... .......... .......... .......... 33% 62.2M 3s 88350K .......... .......... .......... .......... .......... 33% 48.0M 3s 88400K .......... .......... .......... .......... .......... 33% 62.7M 3s 88450K .......... .......... .......... .......... .......... 33% 54.0M 3s 88500K .......... .......... .......... .......... .......... 33% 61.2M 3s 88550K .......... .......... .......... .......... .......... 33% 93.2M 3s 88600K .......... .......... .......... .......... .......... 33% 59.1M 3s 88650K .......... .......... .......... .......... .......... 33% 53.3M 3s 88700K .......... .......... .......... .......... .......... 33% 52.4M 3s 88750K .......... .......... .......... .......... .......... 33% 64.0M 3s 88800K .......... .......... .......... .......... .......... 33% 62.2M 3s 88850K .......... .......... .......... .......... .......... 33% 54.0M 3s 88900K .......... .......... .......... .......... .......... 33% 63.5M 3s 88950K 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34% 364M 3s 90300K .......... .......... .......... .......... .......... 34% 64.1M 3s 90350K .......... .......... .......... .......... .......... 34% 51.2M 3s 90400K .......... .......... .......... .......... .......... 34% 444M 3s 90450K .......... .......... .......... .......... .......... 34% 54.1M 3s 90500K .......... .......... .......... .......... .......... 34% 65.5M 3s 90550K .......... .......... .......... .......... .......... 34% 56.4M 3s 90600K .......... .......... .......... .......... .......... 34% 33.1M 3s 90650K .......... .......... .......... .......... .......... 34% 62.9M 3s 90700K .......... .......... .......... .......... .......... 34% 48.9M 3s 90750K .......... .......... .......... .......... .......... 34% 52.0M 3s 90800K .......... .......... .......... .......... .......... 34% 63.5M 3s 90850K .......... .......... .......... .......... .......... 34% 48.0M 3s 90900K .......... .......... .......... .......... .......... 34% 54.7M 3s 90950K 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.......... 35% 52.4M 3s 92300K .......... .......... .......... .......... .......... 35% 61.1M 3s 92350K .......... .......... .......... .......... .......... 35% 51.4M 3s 92400K .......... .......... .......... .......... .......... 35% 184M 3s 92450K .......... .......... .......... .......... .......... 35% 42.2M 3s 92500K .......... .......... .......... .......... .......... 35% 131M 3s 92550K .......... .......... .......... .......... .......... 35% 127M 3s 92600K .......... .......... .......... .......... .......... 35% 40.7M 3s 92650K .......... .......... .......... .......... .......... 35% 95.4M 3s 92700K .......... .......... .......... .......... .......... 35% 88.0M 3s 92750K .......... .......... .......... .......... .......... 35% 15.7M 3s 92800K .......... .......... .......... .......... .......... 35% 354M 3s 92850K .......... .......... .......... .......... .......... 35% 323M 3s 92900K .......... .......... .......... .......... .......... 35% 509M 3s 92950K 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.......... 35% 126M 3s 94300K .......... .......... .......... .......... .......... 35% 54.4M 3s 94350K .......... .......... .......... .......... .......... 36% 53.8M 3s 94400K .......... .......... .......... .......... .......... 36% 54.3M 3s 94450K .......... .......... .......... .......... .......... 36% 58.5M 3s 94500K .......... .......... .......... .......... .......... 36% 52.7M 3s 94550K .......... .......... .......... .......... .......... 36% 94.3M 3s 94600K .......... .......... .......... .......... .......... 36% 54.2M 3s 94650K .......... .......... .......... .......... .......... 36% 58.5M 3s 94700K .......... .......... .......... .......... .......... 36% 53.7M 3s 94750K .......... .......... .......... .......... .......... 36% 58.7M 3s 94800K .......... .......... .......... .......... .......... 36% 54.6M 3s 94850K .......... .......... .......... .......... .......... 36% 96.9M 3s 94900K .......... .......... .......... .......... .......... 36% 54.1M 3s 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.......... .......... .......... .......... 36% 20.1M 3s 95650K .......... .......... .......... .......... .......... 36% 30.7M 3s 95700K .......... .......... .......... .......... .......... 36% 20.2M 3s 95750K .......... .......... .......... .......... .......... 36% 25.3M 3s 95800K .......... .......... .......... .......... .......... 36% 27.1M 3s 95850K .......... .......... .......... .......... .......... 36% 17.9M 3s 95900K .......... .......... .......... .......... .......... 36% 31.2M 3s 95950K .......... .......... .......... .......... .......... 36% 19.1M 3s 96000K .......... .......... .......... .......... .......... 36% 27.4M 3s 96050K .......... .......... .......... .......... .......... 36% 27.4M 3s 96100K .......... .......... .......... .......... .......... 36% 22.3M 3s 96150K .......... .......... .......... .......... .......... 36% 40.1M 3s 96200K .......... .......... .......... .......... .......... 36% 33.7M 3s 96250K .......... .......... .......... .......... .......... 36% 31.3M 3s 96300K .......... .......... .......... .......... .......... 36% 118M 3s 96350K .......... .......... .......... .......... .......... 36% 13.6M 3s 96400K .......... .......... .......... .......... .......... 36% 50.5M 3s 96450K .......... .......... .......... .......... .......... 36% 171M 3s 96500K .......... .......... .......... .......... .......... 36% 48.3M 3s 96550K .......... .......... .......... .......... .......... 36% 46.8M 3s 96600K .......... .......... .......... .......... .......... 36% 29.1M 3s 96650K .......... .......... .......... .......... .......... 36% 46.3M 3s 96700K .......... .......... .......... .......... .......... 36% 27.6M 3s 96750K .......... .......... .......... .......... .......... 36% 44.9M 3s 96800K .......... .......... .......... .......... .......... 36% 45.5M 3s 96850K .......... .......... .......... .......... .......... 36% 28.7M 3s 96900K .......... .......... .......... .......... .......... 36% 47.1M 3s 96950K .......... .......... .......... .......... .......... 36% 26.9M 3s 97000K .......... .......... .......... .......... .......... 37% 46.6M 3s 97050K .......... .......... .......... .......... .......... 37% 42.4M 3s 97100K .......... .......... .......... .......... .......... 37% 41.3M 3s 97150K .......... .......... .......... .......... .......... 37% 29.2M 3s 97200K .......... .......... .......... .......... .......... 37% 42.2M 3s 97250K .......... .......... .......... .......... .......... 37% 47.0M 3s 97300K .......... .......... .......... .......... .......... 37% 31.2M 3s 97350K .......... .......... .......... .......... .......... 37% 42.3M 3s 97400K .......... .......... .......... .......... .......... 37% 52.1M 3s 97450K .......... .......... .......... .......... .......... 37% 28.2M 3s 97500K .......... .......... .......... .......... .......... 37% 46.8M 3s 97550K .......... .......... .......... .......... .......... 37% 45.9M 3s 97600K .......... .......... .......... .......... .......... 37% 29.1M 3s 97650K .......... .......... .......... .......... .......... 37% 47.0M 3s 97700K .......... .......... .......... .......... .......... 37% 42.0M 3s 97750K .......... .......... .......... .......... .......... 37% 52.9M 3s 97800K .......... .......... .......... .......... .......... 37% 30.7M 3s 97850K .......... .......... .......... .......... .......... 37% 42.8M 3s 97900K .......... .......... .......... .......... .......... 37% 47.8M 3s 97950K .......... .......... .......... .......... .......... 37% 28.9M 3s 98000K .......... .......... .......... .......... .......... 37% 38.2M 3s 98050K .......... .......... .......... .......... .......... 37% 31.7M 3s 98100K .......... .......... .......... .......... .......... 37% 24.4M 3s 98150K .......... .......... .......... .......... .......... 37% 49.4M 3s 98200K .......... .......... .......... .......... .......... 37% 218M 3s 98250K .......... .......... .......... .......... .......... 37% 23.6M 3s 98300K .......... .......... .......... .......... .......... 37% 144M 3s 98350K .......... .......... .......... .......... .......... 37% 284M 3s 98400K .......... .......... .......... .......... .......... 37% 82.2M 3s 98450K .......... .......... .......... .......... .......... 37% 49.0M 3s 98500K .......... .......... .......... .......... .......... 37% 54.7M 3s 98550K .......... .......... .......... .......... .......... 37% 47.4M 3s 98600K .......... .......... .......... .......... .......... 37% 27.0M 3s 98650K .......... .......... .......... .......... .......... 37% 54.7M 3s 98700K .......... .......... .......... .......... .......... 37% 47.7M 3s 98750K .......... .......... .......... .......... .......... 37% 47.3M 3s 98800K .......... .......... .......... .......... .......... 37% 54.6M 3s 98850K .......... .......... .......... .......... .......... 37% 50.7M 3s 98900K .......... .......... .......... .......... .......... 37% 51.3M 3s 98950K .......... .......... .......... .......... .......... 37% 45.0M 3s 99000K .......... .......... .......... .......... .......... 37% 53.5M 3s 99050K .......... .......... .......... .......... .......... 37% 37.3M 3s 99100K .......... .......... .......... .......... .......... 37% 52.8M 3s 99150K .......... .......... .......... .......... .......... 37% 48.5M 3s 99200K .......... .......... .......... .......... .......... 37% 46.2M 3s 99250K .......... .......... .......... .......... .......... 37% 50.9M 3s 99300K .......... .......... .......... .......... .......... 37% 52.3M 3s 99350K .......... .......... .......... .......... .......... 37% 51.6M 3s 99400K .......... .......... .......... .......... .......... 37% 47.8M 3s 99450K .......... .......... .......... .......... .......... 37% 34.3M 3s 99500K .......... .......... .......... .......... .......... 37% 47.8M 3s 99550K .......... .......... .......... .......... .......... 37% 61.7M 3s 99600K .......... .......... .......... .......... .......... 38% 47.6M 3s 99650K .......... .......... .......... .......... .......... 38% 51.9M 3s 99700K .......... .......... .......... .......... .......... 38% 45.0M 3s 99750K .......... .......... .......... .......... .......... 38% 51.0M 3s 99800K .......... .......... .......... .......... .......... 38% 50.8M 3s 99850K .......... .......... .......... .......... .......... 38% 32.9M 3s 99900K .......... .......... .......... .......... .......... 38% 49.7M 3s 99950K .......... .......... .......... .......... .......... 38% 47.7M 3s 100000K .......... .......... .......... .......... .......... 38% 53.8M 3s 100050K .......... .......... .......... .......... .......... 38% 48.2M 3s 100100K .......... .......... .......... .......... .......... 38% 52.6M 3s 100150K .......... .......... .......... .......... .......... 38% 54.4M 3s 100200K .......... .......... .......... .......... .......... 38% 47.2M 3s 100250K .......... .......... .......... .......... .......... 38% 34.5M 3s 100300K .......... .......... .......... .......... .......... 38% 51.7M 3s 100350K .......... .......... .......... .......... .......... 38% 100M 3s 100400K .......... .......... .......... .......... .......... 38% 42.8M 3s 100450K .......... .......... .......... .......... .......... 38% 91.3M 3s 100500K .......... .......... .......... .......... .......... 38% 34.3M 3s 100550K .......... .......... .......... .......... .......... 38% 26.1M 3s 100600K .......... .......... .......... .......... .......... 38% 177M 3s 100650K .......... .......... .......... .......... .......... 38% 34.3M 3s 100700K .......... .......... .......... .......... .......... 38% 102M 3s 100750K .......... .......... .......... .......... .......... 38% 61.8M 3s 100800K .......... .......... .......... .......... .......... 38% 62.5M 3s 100850K .......... .......... .......... .......... .......... 38% 126M 3s 100900K .......... .......... .......... .......... .......... 38% 88.3M 3s 100950K .......... .......... .......... .......... .......... 38% 50.3M 3s 101000K .......... .......... .......... .......... .......... 38% 54.4M 3s 101050K .......... .......... .......... .......... .......... 38% 53.6M 3s 101100K .......... .......... .......... .......... .......... 38% 34.6M 3s 101150K .......... .......... .......... .......... .......... 38% 47.2M 3s 101200K .......... .......... .......... .......... .......... 38% 34.3M 3s 101250K .......... .......... .......... .......... .......... 38% 42.4M 3s 101300K .......... .......... .......... .......... .......... 38% 54.4M 3s 101350K .......... .......... .......... .......... .......... 38% 37.4M 3s 101400K .......... .......... .......... .......... .......... 38% 39.9M 3s 101450K .......... .......... .......... .......... .......... 38% 28.6M 3s 101500K .......... .......... .......... .......... .......... 38% 56.7M 3s 101550K .......... .......... .......... .......... .......... 38% 45.2M 3s 101600K .......... .......... .......... .......... .......... 38% 32.1M 3s 101650K .......... .......... .......... .......... .......... 38% 46.5M 3s 101700K .......... .......... .......... .......... .......... 38% 37.9M 3s 101750K .......... .......... .......... .......... .......... 38% 42.1M 3s 101800K .......... .......... .......... .......... .......... 38% 47.6M 3s 101850K .......... .......... .......... .......... .......... 38% 34.9M 3s 101900K .......... .......... .......... .......... .......... 38% 47.2M 3s 101950K .......... .......... .......... .......... .......... 38% 54.6M 3s 102000K .......... .......... .......... .......... .......... 38% 34.4M 3s 102050K .......... .......... .......... .......... .......... 38% 53.8M 3s 102100K .......... .......... .......... .......... .......... 38% 43.7M 3s 102150K .......... .......... .......... .......... .......... 38% 37.5M 3s 102200K .......... .......... .......... .......... .......... 38% 46.4M 3s 102250K .......... .......... .......... .......... .......... 39% 33.7M 3s 102300K .......... .......... .......... .......... .......... 39% 48.1M 3s 102350K .......... .......... .......... .......... .......... 39% 31.2M 3s 102400K .......... .......... .......... .......... .......... 39% 122M 3s 102450K .......... .......... .......... .......... .......... 39% 42.5M 3s 102500K .......... .......... .......... .......... .......... 39% 13.9M 3s 102550K .......... .......... .......... .......... .......... 39% 334M 3s 102600K .......... .......... .......... .......... .......... 39% 364M 3s 102650K .......... .......... .......... .......... .......... 39% 34.6M 3s 102700K .......... .......... .......... .......... .......... 39% 96.9M 3s 102750K .......... .......... .......... .......... .......... 39% 38.8M 3s 102800K .......... .......... .......... .......... .......... 39% 47.4M 3s 102850K .......... .......... .......... .......... .......... 39% 45.3M 3s 102900K .......... .......... .......... .......... .......... 39% 52.4M 3s 102950K .......... .......... .......... .......... .......... 39% 30.2M 3s 103000K .......... .......... .......... .......... .......... 39% 31.3M 3s 103050K .......... .......... .......... .......... .......... 39% 47.2M 3s 103100K .......... .......... .......... .......... .......... 39% 28.7M 3s 103150K .......... .......... .......... .......... .......... 39% 47.1M 3s 103200K .......... .......... .......... .......... .......... 39% 43.2M 3s 103250K .......... .......... .......... .......... .......... 39% 31.1M 3s 103300K .......... .......... .......... .......... .......... 39% 47.6M 3s 103350K .......... .......... .......... .......... .......... 39% 29.7M 3s 103400K .......... .......... .......... .......... .......... 39% 45.9M 3s 103450K .......... .......... .......... .......... .......... 39% 46.2M 3s 103500K .......... .......... .......... .......... .......... 39% 25.3M 3s 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.......... 40% 63.4M 3s 106850K .......... .......... .......... .......... .......... 40% 54.3M 3s 106900K .......... .......... .......... .......... .......... 40% 63.3M 3s 106950K .......... .......... .......... .......... .......... 40% 55.6M 3s 107000K .......... .......... .......... .......... .......... 40% 63.6M 3s 107050K .......... .......... .......... .......... .......... 40% 63.3M 3s 107100K .......... .......... .......... .......... .......... 40% 53.8M 3s 107150K .......... .......... .......... .......... .......... 40% 94.3M 3s 107200K .......... .......... .......... .......... .......... 40% 52.2M 3s 107250K .......... .......... .......... .......... .......... 40% 62.1M 3s 107300K .......... .......... .......... .......... .......... 40% 62.6M 3s 107350K .......... .......... .......... .......... .......... 40% 52.1M 3s 107400K .......... .......... .......... .......... .......... 40% 55.0M 3s 107450K .......... .......... .......... .......... .......... 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.......... .......... .......... .......... 41% 201M 3s 109500K .......... .......... .......... .......... .......... 41% 81.7M 3s 109550K .......... .......... .......... .......... .......... 41% 86.7M 3s 109600K .......... .......... .......... .......... .......... 41% 63.7M 3s 109650K .......... .......... .......... .......... .......... 41% 63.4M 3s 109700K .......... .......... .......... .......... .......... 41% 54.4M 3s 109750K .......... .......... .......... .......... .......... 41% 73.6M 3s 109800K .......... .......... .......... .......... .......... 41% 61.1M 3s 109850K .......... .......... .......... .......... .......... 41% 48.7M 3s 109900K .......... .......... .......... .......... .......... 41% 94.6M 3s 109950K .......... .......... .......... .......... .......... 41% 61.5M 3s 110000K .......... .......... .......... .......... .......... 41% 54.6M 3s 110050K .......... .......... .......... .......... .......... 41% 73.4M 3s 110100K .......... .......... .......... .......... .......... 42% 53.8M 3s 110150K .......... .......... .......... .......... .......... 42% 64.2M 3s 110200K .......... .......... .......... .......... .......... 42% 90.8M 3s 110250K .......... .......... .......... .......... .......... 42% 63.0M 3s 110300K .......... .......... .......... .......... .......... 42% 53.4M 3s 110350K .......... .......... .......... .......... .......... 42% 53.4M 3s 110400K .......... .......... .......... .......... .......... 42% 69.7M 3s 110450K .......... .......... .......... .......... .......... 42% 53.4M 3s 110500K .......... .......... .......... .......... .......... 42% 94.1M 3s 110550K .......... .......... .......... .......... .......... 42% 63.1M 3s 110600K .......... .......... .......... .......... .......... 42% 61.7M 3s 110650K .......... .......... .......... .......... .......... 42% 54.7M 3s 110700K .......... .......... .......... .......... .......... 42% 61.4M 3s 110750K .......... .......... .......... .......... .......... 42% 63.9M 3s 110800K .......... .......... .......... .......... .......... 42% 78.9M 3s 110850K .......... .......... .......... .......... .......... 42% 61.9M 3s 110900K .......... .......... .......... .......... .......... 42% 55.5M 3s 110950K .......... .......... .......... .......... .......... 42% 63.6M 3s 111000K .......... .......... .......... .......... .......... 42% 67.2M 3s 111050K .......... .......... .......... .......... .......... 42% 57.9M 3s 111100K .......... .......... .......... .......... .......... 42% 43.4M 3s 111150K .......... .......... .......... .......... .......... 42% 120M 3s 111200K .......... .......... .......... .......... .......... 42% 54.7M 3s 111250K .......... .......... .......... .......... .......... 42% 61.9M 3s 111300K .......... .......... .......... .......... .......... 42% 65.2M 3s 111350K .......... .......... .......... .......... .......... 42% 47.4M 3s 111400K .......... .......... .......... .......... .......... 42% 171M 3s 111450K .......... .......... .......... .......... .......... 42% 54.7M 3s 111500K .......... .......... .......... .......... .......... 42% 58.7M 3s 111550K .......... .......... .......... .......... .......... 42% 53.5M 3s 111600K .......... .......... .......... .......... .......... 42% 60.8M 3s 111650K .......... .......... .......... .......... .......... 42% 98.8M 3s 111700K .......... .......... .......... .......... .......... 42% 71.5M 3s 111750K .......... .......... .......... .......... .......... 42% 94.4M 3s 111800K .......... .......... .......... .......... .......... 42% 75.0M 3s 111850K .......... .......... .......... .......... .......... 42% 20.9M 3s 111900K .......... .......... .......... .......... .......... 42% 169M 3s 111950K .......... .......... .......... .......... .......... 42% 80.2M 3s 112000K .......... .......... .......... .......... .......... 42% 474M 3s 112050K .......... .......... .......... .......... .......... 42% 410M 3s 112100K .......... .......... .......... .......... .......... 42% 40.3M 3s 112150K .......... .......... .......... .......... .......... 42% 241M 3s 112200K .......... .......... .......... .......... .......... 42% 139M 3s 112250K .......... .......... .......... .......... .......... 42% 364M 3s 112300K .......... .......... .......... .......... .......... 42% 46.8M 3s 112350K .......... .......... .......... .......... .......... 42% 101M 3s 112400K .......... .......... .......... .......... .......... 42% 514M 3s 112450K .......... .......... .......... .......... .......... 42% 89.8M 3s 112500K .......... .......... .......... .......... .......... 42% 63.9M 3s 112550K .......... .......... .......... .......... .......... 42% 76.3M 3s 112600K .......... .......... .......... .......... .......... 42% 74.9M 3s 112650K .......... .......... .......... .......... .......... 42% 62.8M 3s 112700K .......... .......... .......... .......... .......... 43% 69.2M 3s 112750K .......... .......... .......... .......... .......... 43% 82.9M 3s 112800K .......... .......... .......... .......... .......... 43% 62.6M 3s 112850K .......... .......... .......... .......... .......... 43% 55.9M 3s 112900K .......... .......... .......... .......... .......... 43% 91.8M 3s 112950K .......... .......... .......... .......... .......... 43% 55.4M 3s 113000K .......... .......... .......... .......... .......... 43% 88.0M 3s 113050K .......... .......... .......... .......... .......... 43% 66.1M 3s 113100K .......... .......... .......... .......... .......... 43% 70.0M 3s 113150K .......... .......... .......... .......... .......... 43% 75.7M 3s 113200K .......... .......... .......... .......... .......... 43% 61.8M 3s 113250K .......... .......... .......... .......... .......... 43% 81.7M 3s 113300K .......... .......... .......... .......... .......... 43% 62.8M 3s 113350K .......... .......... .......... .......... .......... 43% 73.8M 3s 113400K .......... .......... .......... .......... .......... 43% 65.3M 3s 113450K .......... .......... .......... .......... .......... 43% 54.5M 3s 113500K .......... .......... .......... .......... .......... 43% 95.2M 3s 113550K .......... .......... .......... .......... .......... 43% 62.8M 3s 113600K .......... .......... .......... .......... .......... 43% 63.4M 3s 113650K .......... .......... .......... .......... .......... 43% 73.6M 3s 113700K .......... .......... .......... .......... .......... 43% 77.0M 3s 113750K .......... .......... .......... .......... .......... 43% 74.4M 3s 113800K .......... .......... .......... .......... .......... 43% 64.1M 3s 113850K .......... .......... .......... .......... .......... 43% 63.0M 3s 113900K .......... .......... .......... .......... .......... 43% 62.8M 3s 113950K .......... .......... .......... .......... .......... 43% 91.4M 3s 114000K .......... .......... .......... .......... .......... 43% 64.6M 3s 114050K .......... .......... .......... .......... .......... 43% 73.5M 3s 114100K .......... .......... .......... .......... .......... 43% 49.8M 3s 114150K .......... .......... .......... .......... .......... 43% 94.6M 3s 114200K .......... .......... .......... .......... .......... 43% 61.0M 3s 114250K .......... .......... .......... .......... .......... 43% 64.7M 3s 114300K .......... .......... .......... .......... .......... 43% 73.3M 3s 114350K .......... .......... .......... .......... .......... 43% 63.6M 3s 114400K .......... .......... .......... .......... .......... 43% 77.6M 3s 114450K .......... .......... .......... .......... .......... 43% 63.7M 3s 114500K .......... .......... .......... .......... .......... 43% 72.2M 3s 114550K .......... .......... .......... .......... .......... 43% 65.5M 3s 114600K .......... .......... .......... .......... .......... 43% 62.8M 3s 114650K .......... .......... .......... .......... .......... 43% 60.7M 3s 114700K .......... .......... .......... .......... .......... 43% 52.3M 3s 114750K .......... .......... .......... .......... .......... 43% 132M 3s 114800K .......... .......... .......... .......... .......... 43% 62.7M 3s 114850K .......... .......... .......... .......... .......... 43% 55.7M 3s 114900K .......... .......... .......... .......... .......... 43% 130M 3s 114950K .......... .......... .......... .......... .......... 43% 72.8M 3s 115000K .......... .......... .......... .......... .......... 43% 96.1M 3s 115050K .......... .......... .......... .......... .......... 43% 54.4M 3s 115100K .......... .......... .......... .......... .......... 43% 23.9M 3s 115150K .......... .......... .......... .......... .......... 43% 379M 3s 115200K .......... .......... .......... .......... .......... 43% 43.6M 3s 115250K .......... .......... .......... .......... .......... 43% 384M 3s 115300K .......... .......... .......... .......... .......... 43% 56.8M 3s 115350K .......... .......... .......... .......... .......... 44% 38.7M 3s 115400K .......... .......... .......... .......... .......... 44% 421M 3s 115450K .......... .......... .......... .......... .......... 44% 417M 3s 115500K .......... .......... .......... .......... .......... 44% 488M 3s 115550K .......... .......... .......... .......... .......... 44% 111M 3s 115600K .......... .......... .......... .......... .......... 44% 55.1M 3s 115650K .......... .......... .......... .......... .......... 44% 121M 3s 115700K .......... .......... .......... .......... .......... 44% 62.7M 3s 115750K .......... .......... .......... .......... .......... 44% 65.0M 3s 115800K .......... .......... .......... .......... .......... 44% 94.3M 3s 115850K .......... .......... .......... .......... .......... 44% 63.4M 3s 115900K .......... .......... .......... .......... .......... 44% 73.9M 3s 115950K .......... .......... .......... .......... .......... 44% 54.6M 3s 116000K .......... .......... .......... .......... .......... 44% 126M 3s 116050K .......... .......... .......... .......... .......... 44% 74.8M 3s 116100K .......... .......... .......... .......... .......... 44% 62.8M 3s 116150K .......... .......... .......... .......... .......... 44% 97.9M 3s 116200K .......... .......... .......... .......... .......... 44% 63.2M 3s 116250K .......... .......... .......... .......... .......... 44% 72.9M 3s 116300K .......... .......... .......... .......... .......... 44% 62.2M 3s 116350K .......... .......... .......... .......... .......... 44% 69.7M 3s 116400K .......... .......... .......... .......... .......... 44% 95.4M 3s 116450K .......... .......... .......... .......... .......... 44% 59.5M 3s 116500K .......... .......... .......... .......... .......... 44% 109M 3s 116550K .......... .......... .......... .......... .......... 44% 65.5M 3s 116600K .......... .......... .......... .......... .......... 44% 61.1M 3s 116650K .......... .......... .......... .......... .......... 44% 68.7M 3s 116700K .......... .......... .......... .......... .......... 44% 97.3M 3s 116750K .......... .......... .......... .......... .......... 44% 63.2M 3s 116800K .......... .......... .......... .......... .......... 44% 73.2M 3s 116850K .......... .......... .......... .......... .......... 44% 64.8M 3s 116900K .......... .......... .......... .......... .......... 44% 95.4M 3s 116950K .......... .......... .......... .......... .......... 44% 62.8M 3s 117000K .......... .......... .......... .......... .......... 44% 63.5M 3s 117050K .......... .......... .......... .......... .......... 44% 75.1M 3s 117100K .......... .......... .......... .......... .......... 44% 90.9M 3s 117150K .......... .......... .......... .......... .......... 44% 64.5M 3s 117200K .......... .......... .......... .......... .......... 44% 62.8M 3s 117250K .......... .......... .......... .......... .......... 44% 63.2M 3s 117300K .......... .......... .......... .......... .......... 44% 76.3M 3s 117350K .......... .......... .......... .......... .......... 44% 94.6M 3s 117400K .......... .......... .......... .......... .......... 44% 63.5M 3s 117450K .......... .......... .......... .......... .......... 44% 74.0M 3s 117500K .......... .......... .......... .......... .......... 44% 62.4M 3s 117550K .......... .......... .......... .......... .......... 44% 114M 3s 117600K .......... .......... .......... .......... .......... 44% 58.3M 3s 117650K .......... .......... .......... .......... .......... 44% 63.2M 3s 117700K .......... .......... .......... .......... .......... 44% 87.3M 3s 117750K .......... .......... .......... .......... .......... 44% 74.0M 3s 117800K .......... .......... .......... .......... .......... 44% 63.3M 3s 117850K .......... .......... .......... .......... .......... 44% 96.3M 3s 117900K .......... .......... .......... .......... .......... 44% 73.6M 3s 117950K .......... .......... .......... .......... .......... 45% 57.4M 3s 118000K .......... .......... .......... .......... .......... 45% 66.8M 3s 118050K .......... .......... .......... .......... .......... 45% 95.7M 3s 118100K .......... .......... .......... .......... .......... 45% 63.2M 3s 118150K .......... .......... .......... .......... .......... 45% 93.7M 3s 118200K .......... .......... .......... .......... .......... 45% 57.9M 3s 118250K .......... .......... .......... .......... .......... 45% 61.5M 3s 118300K .......... .......... .......... .......... .......... 45% 76.4M 3s 118350K .......... .......... .......... .......... .......... 45% 89.9M 3s 118400K .......... .......... .......... .......... .......... 45% 19.2M 3s 118450K .......... .......... .......... .......... .......... 45% 78.6M 3s 118500K .......... .......... .......... .......... .......... 45% 581M 3s 118550K .......... .......... .......... .......... .......... 45% 31.5M 3s 118600K .......... .......... .......... .......... .......... 45% 410M 3s 118650K .......... .......... .......... .......... .......... 45% 79.7M 3s 118700K .......... .......... .......... .......... .......... 45% 60.4M 3s 118750K .......... .......... .......... .......... .......... 45% 432M 3s 118800K .......... .......... .......... .......... .......... 45% 64.2M 3s 118850K .......... .......... .......... .......... .......... 45% 47.2M 3s 118900K .......... .......... .......... .......... .......... 45% 54.0M 3s 118950K .......... .......... .......... .......... .......... 45% 40.8M 3s 119000K .......... .......... .......... .......... .......... 45% 48.1M 3s 119050K .......... .......... .......... .......... .......... 45% 47.6M 3s 119100K .......... .......... .......... .......... .......... 45% 42.2M 3s 119150K .......... .......... .......... .......... .......... 45% 47.2M 3s 119200K .......... .......... .......... .......... .......... 45% 26.7M 3s 119250K .......... .......... .......... .......... .......... 45% 404M 3s 119300K .......... .......... .......... .......... .......... 45% 41.5M 3s 119350K .......... .......... .......... .......... .......... 45% 34.5M 3s 119400K .......... .......... .......... .......... .......... 45% 47.9M 3s 119450K .......... .......... .......... .......... .......... 45% 44.5M 3s 119500K .......... .......... .......... .......... .......... 45% 30.6M 3s 119550K .......... .......... .......... .......... .......... 45% 50.9M 3s 119600K .......... .......... .......... .......... .......... 45% 46.2M 3s 119650K .......... .......... .......... .......... .......... 45% 51.0M 3s 119700K .......... .......... .......... .......... .......... 45% 43.8M 3s 119750K .......... .......... .......... .......... .......... 45% 48.2M 3s 119800K .......... .......... .......... .......... .......... 45% 33.8M 3s 119850K .......... .......... .......... .......... .......... 45% 47.0M 3s 119900K .......... .......... .......... .......... .......... 45% 47.5M 3s 119950K .......... .......... .......... .......... .......... 45% 41.8M 3s 120000K .......... .......... .......... .......... .......... 45% 48.1M 3s 120050K .......... .......... .......... .......... .......... 45% 52.7M 3s 120100K .......... .......... .......... .......... .......... 45% 31.4M 3s 120150K .......... .......... .......... .......... .......... 45% 47.2M 3s 120200K .......... .......... .......... .......... .......... 45% 47.4M 3s 120250K .......... .......... .......... .......... .......... 45% 50.6M 3s 120300K .......... .......... .......... .......... .......... 45% 48.1M 3s 120350K .......... .......... .......... .......... .......... 45% 32.1M 3s 120400K .......... .......... .......... .......... .......... 45% 49.7M 3s 120450K .......... .......... .......... .......... .......... 45% 40.9M 3s 120500K .......... .......... .......... .......... .......... 45% 48.3M 3s 120550K .......... .......... .......... .......... .......... 45% 53.1M 3s 120600K .......... .......... .......... .......... .......... 46% 31.8M 3s 120650K .......... .......... .......... .......... .......... 46% 52.8M 3s 120700K .......... .......... .......... .......... .......... 46% 43.8M 3s 120750K .......... .......... .......... .......... .......... 46% 53.5M 3s 120800K .......... .......... .......... .......... .......... 46% 48.2M 3s 120850K .......... .......... .......... .......... .......... 46% 33.8M 3s 120900K .......... .......... .......... .......... .......... 46% 42.6M 3s 120950K .......... .......... .......... .......... .......... 46% 36.8M 3s 121000K .......... .......... .......... .......... .......... 46% 22.4M 3s 121050K .......... .......... .......... .......... .......... 46% 140M 3s 121100K .......... .......... .......... .......... .......... 46% 36.0M 3s 121150K .......... .......... .......... .......... .......... 46% 39.9M 3s 121200K .......... .......... .......... .......... .......... 46% 166M 3s 121250K .......... .......... .......... .......... .......... 46% 24.4M 3s 121300K .......... .......... .......... .......... .......... 46% 48.5M 3s 121350K .......... .......... .......... .......... .......... 46% 35.1M 3s 121400K .......... .......... .......... .......... .......... 46% 24.7M 3s 121450K .......... .......... .......... .......... .......... 46% 29.7M 3s 121500K .......... .......... .......... .......... .......... 46% 29.2M 3s 121550K .......... .......... .......... .......... .......... 46% 31.7M 3s 121600K .......... .......... .......... .......... .......... 46% 29.5M 3s 121650K .......... .......... .......... .......... .......... 46% 26.2M 3s 121700K .......... .......... .......... .......... .......... 46% 20.6M 3s 121750K .......... .......... .......... .......... .......... 46% 29.2M 3s 121800K .......... .......... .......... .......... .......... 46% 34.1M 3s 121850K .......... .......... .......... .......... .......... 46% 25.5M 3s 121900K .......... .......... .......... .......... .......... 46% 29.3M 3s 121950K .......... .......... .......... .......... .......... 46% 29.2M 3s 122000K .......... .......... .......... .......... .......... 46% 32.1M 3s 122050K .......... .......... .......... .......... .......... 46% 31.2M 3s 122100K .......... .......... .......... .......... .......... 46% 22.1M 3s 122150K .......... .......... .......... .......... .......... 46% 31.2M 3s 122200K .......... .......... .......... .......... .......... 46% 24.0M 3s 122250K .......... .......... .......... .......... .......... 46% 31.2M 3s 122300K .......... .......... .......... .......... .......... 46% 38.8M 3s 122350K .......... .......... .......... .......... .......... 46% 41.7M 3s 122400K .......... .......... .......... .......... .......... 46% 37.1M 3s 122450K .......... .......... .......... .......... .......... 46% 22.0M 3s 122500K .......... .......... .......... .......... .......... 46% 568M 3s 122550K .......... .......... .......... .......... .......... 46% 21.0M 3s 122600K .......... .......... .......... .......... .......... 46% 44.8M 3s 122650K .......... .......... .......... .......... .......... 46% 55.4M 3s 122700K .......... .......... .......... .......... .......... 46% 28.2M 3s 122750K .......... .......... .......... .......... .......... 46% 46.0M 3s 122800K .......... .......... .......... .......... .......... 46% 29.5M 3s 122850K .......... .......... .......... .......... .......... 46% 30.7M 3s 122900K .......... .......... .......... .......... .......... 46% 30.0M 3s 122950K .......... .......... .......... .......... .......... 46% 31.2M 3s 123000K .......... .......... .......... .......... .......... 46% 31.1M 3s 123050K .......... .......... .......... .......... .......... 46% 35.0M 3s 123100K .......... .......... .......... .......... .......... 46% 27.5M 3s 123150K .......... .......... .......... .......... .......... 46% 52.3M 3s 123200K .......... .......... .......... .......... .......... 47% 27.9M 3s 123250K .......... .......... .......... .......... .......... 47% 43.9M 3s 123300K .......... .......... .......... .......... .......... 47% 29.0M 3s 123350K .......... .......... .......... .......... .......... 47% 28.9M 3s 123400K .......... .......... .......... .......... .......... 47% 47.5M 3s 123450K .......... .......... .......... .......... .......... 47% 27.0M 3s 123500K .......... .......... .......... .......... .......... 47% 46.9M 3s 123550K .......... .......... .......... .......... .......... 47% 29.2M 3s 123600K .......... .......... .......... .......... .......... 47% 29.1M 3s 123650K .......... .......... .......... .......... .......... 47% 37.9M 3s 123700K .......... .......... .......... .......... .......... 47% 29.7M 3s 123750K .......... .......... .......... .......... .......... 47% 40.8M 3s 123800K .......... .......... .......... .......... .......... 47% 39.9M 3s 123850K .......... .......... .......... .......... .......... 47% 28.6M 3s 123900K .......... .......... .......... .......... .......... 47% 33.7M 3s 123950K .......... .......... .......... .......... .......... 47% 16.1M 3s 124000K .......... .......... .......... .......... .......... 47% 53.1M 3s 124050K .......... .......... .......... .......... .......... 47% 33.1M 3s 124100K .......... .......... .......... .......... .......... 47% 151M 3s 124150K .......... .......... .......... .......... .......... 47% 31.6M 3s 124200K .......... .......... .......... .......... .......... 47% 22.9M 3s 124250K .......... .......... .......... .......... .......... 47% 64.2M 3s 124300K .......... .......... .......... .......... .......... 47% 33.7M 3s 124350K .......... .......... .......... .......... .......... 47% 30.4M 3s 124400K .......... .......... .......... .......... .......... 47% 60.5M 3s 124450K .......... .......... .......... .......... .......... 47% 24.7M 3s 124500K .......... .......... .......... .......... .......... 47% 30.0M 3s 124550K .......... .......... .......... .......... .......... 47% 27.3M 3s 124600K .......... .......... .......... .......... .......... 47% 27.1M 3s 124650K .......... .......... .......... .......... .......... 47% 43.5M 3s 124700K .......... .......... .......... .......... .......... 47% 29.1M 3s 124750K .......... .......... .......... .......... .......... 47% 26.9M 3s 124800K .......... .......... .......... .......... .......... 47% 31.8M 3s 124850K .......... .......... .......... .......... .......... 47% 45.8M 3s 124900K .......... .......... .......... .......... .......... 47% 28.1M 3s 124950K .......... .......... .......... .......... .......... 47% 27.7M 3s 125000K .......... .......... .......... .......... .......... 47% 30.3M 3s 125050K .......... .......... .......... .......... .......... 47% 46.1M 3s 125100K .......... .......... .......... .......... .......... 47% 27.3M 3s 125150K .......... .......... .......... .......... .......... 47% 29.2M 3s 125200K .......... .......... .......... .......... .......... 47% 29.3M 3s 125250K .......... .......... .......... .......... .......... 47% 26.8M 3s 125300K .......... .......... .......... .......... .......... 47% 48.1M 3s 125350K .......... .......... .......... .......... .......... 47% 27.0M 3s 125400K .......... .......... .......... .......... .......... 47% 27.7M 3s 125450K .......... .......... .......... .......... .......... 47% 34.7M 3s 125500K .......... .......... .......... .......... .......... 47% 20.3M 3s 125550K .......... .......... .......... .......... .......... 47% 32.8M 3s 125600K .......... .......... .......... .......... .......... 47% 56.4M 3s 125650K .......... .......... .......... .......... .......... 47% 42.4M 3s 125700K .......... .......... .......... .......... .......... 47% 36.4M 3s 125750K .......... .......... .......... .......... .......... 47% 31.7M 3s 125800K .......... .......... .......... .......... .......... 47% 42.1M 3s 125850K .......... .......... .......... .......... .......... 48% 29.2M 3s 125900K .......... .......... .......... .......... .......... 48% 29.0M 3s 125950K .......... .......... .......... .......... .......... 48% 41.6M 3s 126000K .......... .......... .......... .......... .......... 48% 28.9M 3s 126050K .......... .......... .......... .......... .......... 48% 48.9M 3s 126100K .......... .......... .......... .......... .......... 48% 25.4M 3s 126150K .......... .......... .......... .......... .......... 48% 29.3M 3s 126200K .......... .......... .......... .......... .......... 48% 41.9M 3s 126250K .......... .......... .......... .......... .......... 48% 27.1M 3s 126300K .......... .......... .......... .......... .......... 48% 47.6M 3s 126350K .......... .......... .......... .......... .......... 48% 28.9M 3s 126400K .......... .......... .......... .......... .......... 48% 29.0M 3s 126450K .......... .......... .......... .......... .......... 48% 41.7M 3s 126500K .......... .......... .......... .......... .......... 48% 30.8M 3s 126550K .......... .......... .......... .......... .......... 48% 41.8M 3s 126600K .......... .......... .......... .......... .......... 48% 27.6M 3s 126650K .......... .......... .......... .......... .......... 48% 26.6M 3s 126700K .......... .......... .......... .......... .......... 48% 41.2M 3s 126750K .......... .......... .......... .......... .......... 48% 29.7M 3s 126800K .......... .......... .......... .......... .......... 48% 29.0M 3s 126850K .......... .......... .......... .......... .......... 48% 41.6M 3s 126900K .......... .......... .......... .......... .......... 48% 53.4M 3s 126950K .......... .......... .......... .......... .......... 48% 34.7M 3s 127000K .......... .......... .......... .......... .......... 48% 14.0M 3s 127050K .......... .......... .......... .......... .......... 48% 400M 3s 127100K .......... .......... .......... .......... .......... 48% 35.4M 3s 127150K .......... .......... .......... .......... .......... 48% 68.5M 3s 127200K .......... .......... .......... .......... .......... 48% 24.3M 3s 127250K .......... .......... .......... .......... .......... 48% 351M 3s 127300K .......... .......... .......... .......... .......... 48% 60.8M 3s 127350K .......... .......... .......... .......... .......... 48% 79.7M 3s 127400K .......... .......... .......... .......... .......... 48% 48.3M 3s 127450K .......... .......... .......... .......... .......... 48% 31.3M 3s 127500K .......... .......... .......... .......... .......... 48% 47.9M 3s 127550K .......... .......... .......... .......... .......... 48% 53.1M 3s 127600K .......... .......... .......... .......... .......... 48% 25.4M 3s 127650K .......... .......... .......... .......... .......... 48% 50.3M 3s 127700K .......... .......... .......... .......... .......... 48% 47.3M 3s 127750K .......... .......... .......... .......... .......... 48% 31.4M 3s 127800K .......... .......... .......... .......... .......... 48% 44.7M 3s 127850K .......... .......... .......... .......... .......... 48% 45.8M 3s 127900K .......... .......... .......... .......... .......... 48% 36.1M 3s 127950K .......... .......... .......... .......... .......... 48% 43.0M 3s 128000K .......... .......... .......... .......... .......... 48% 45.8M 3s 128050K .......... .......... .......... .......... .......... 48% 30.6M 3s 128100K .......... .......... .......... .......... .......... 48% 42.4M 3s 128150K .......... .......... .......... .......... .......... 48% 47.2M 3s 128200K .......... .......... .......... .......... .......... 48% 31.0M 3s 128250K .......... .......... .......... .......... .......... 48% 46.7M 3s 128300K .......... .......... .......... .......... .......... 48% 32.2M 3s 128350K .......... .......... .......... .......... .......... 48% 46.5M 3s 128400K .......... .......... .......... .......... .......... 48% 47.0M 3s 128450K .......... .......... .......... .......... .......... 49% 32.6M 3s 128500K .......... .......... .......... .......... .......... 49% 50.1M 3s 128550K .......... .......... .......... .......... .......... 49% 48.2M 3s 128600K .......... .......... .......... .......... .......... 49% 31.3M 3s 128650K .......... .......... .......... .......... .......... 49% 54.0M 3s 128700K .......... .......... .......... .......... .......... 49% 31.1M 3s 128750K .......... .......... .......... .......... .......... 49% 94.8M 3s 128800K .......... .......... .......... .......... .......... 49% 61.9M 3s 128850K .......... .......... .......... .......... .......... 49% 53.3M 3s 128900K .......... .......... .......... .......... .......... 49% 100M 3s 128950K .......... .......... .......... .......... .......... 49% 30.5M 3s 129000K .......... .......... .......... .......... .......... 49% 465M 3s 129050K .......... .......... .......... .......... .......... 49% 46.0M 3s 129100K .......... .......... .......... .......... .......... 49% 26.6M 3s 129150K .......... .......... .......... .......... .......... 49% 432M 3s 129200K .......... .......... .......... .......... .......... 49% 425M 3s 129250K .......... .......... .......... .......... .......... 49% 373M 3s 129300K .......... .......... .......... .......... .......... 49% 407M 3s 129350K .......... .......... .......... .......... .......... 49% 32.0M 3s 129400K .......... .......... .......... .......... .......... 49% 488M 3s 129450K .......... .......... .......... .......... .......... 49% 61.1M 3s 129500K .......... .......... .......... .......... .......... 49% 32.6M 3s 129550K .......... .......... .......... .......... .......... 49% 51.0M 3s 129600K .......... .......... .......... .......... .......... 49% 49.8M 3s 129650K .......... .......... .......... .......... .......... 49% 46.4M 3s 129700K .......... .......... .......... .......... .......... 49% 31.6M 3s 129750K .......... .......... .......... .......... .......... 49% 54.4M 3s 129800K .......... .......... .......... .......... .......... 49% 37.8M 3s 129850K .......... .......... .......... .......... .......... 49% 45.4M 3s 129900K .......... .......... .......... .......... .......... 49% 43.6M 3s 129950K .......... .......... .......... .......... .......... 49% 31.8M 3s 130000K .......... .......... .......... .......... .......... 49% 54.4M 3s 130050K .......... .......... .......... .......... .......... 49% 53.8M 3s 130100K .......... .......... .......... .......... .......... 49% 46.2M 3s 130150K .......... .......... .......... .......... .......... 49% 48.3M 3s 130200K .......... .......... .......... .......... .......... 49% 37.4M 3s 130250K .......... .......... .......... .......... .......... 49% 46.5M 3s 130300K .......... .......... .......... .......... .......... 49% 47.0M 3s 130350K .......... .......... .......... .......... .......... 49% 38.3M 3s 130400K .......... .......... .......... .......... .......... 49% 60.5M 3s 130450K .......... .......... .......... .......... .......... 49% 32.8M 3s 130500K .......... .......... .......... .......... .......... 49% 54.6M 3s 130550K .......... .......... .......... .......... .......... 49% 47.2M 3s 130600K .......... .......... .......... .......... .......... 49% 31.4M 3s 130650K .......... .......... .......... .......... .......... 49% 61.8M 3s 130700K .......... .......... .......... .......... .......... 49% 31.9M 3s 130750K .......... .......... .......... .......... .......... 49% 53.5M 3s 130800K .......... .......... .......... .......... .......... 49% 49.2M 3s 130850K .......... .......... .......... .......... .......... 49% 35.0M 3s 130900K .......... .......... .......... .......... .......... 49% 54.6M 3s 130950K .......... .......... .......... .......... .......... 49% 47.9M 3s 131000K .......... .......... .......... .......... .......... 49% 53.0M 3s 131050K .......... .......... .......... .......... .......... 50% 40.8M 3s 131100K .......... .......... .......... .......... .......... 50% 93.4M 3s 131150K .......... .......... .......... .......... .......... 50% 17.5M 3s 131200K .......... .......... .......... .......... .......... 50% 376M 3s 131250K .......... .......... .......... .......... .......... 50% 379M 3s 131300K .......... .......... .......... .......... .......... 50% 29.3M 3s 131350K .......... .......... .......... .......... .......... 50% 126M 3s 131400K .......... .......... .......... .......... .......... 50% 62.0M 3s 131450K .......... .......... .......... .......... .......... 50% 47.5M 3s 131500K .......... .......... .......... .......... .......... 50% 332M 3s 131550K .......... .......... .......... .......... .......... 50% 101M 3s 131600K .......... .......... .......... .......... .......... 50% 47.8M 3s 131650K .......... .......... .......... .......... .......... 50% 61.8M 3s 131700K .......... .......... .......... .......... .......... 50% 54.2M 3s 131750K .......... .......... .......... .......... .......... 50% 61.7M 3s 131800K .......... .......... .......... .......... .......... 50% 55.7M 3s 131850K .......... .......... .......... .......... .......... 50% 60.7M 3s 131900K .......... .......... .......... .......... .......... 50% 65.2M 3s 131950K .......... .......... .......... .......... .......... 50% 41.4M 3s 132000K .......... .......... .......... .......... .......... 50% 72.8M 3s 132050K .......... .......... .......... .......... .......... 50% 51.7M 3s 132100K .......... .......... .......... .......... .......... 50% 50.9M 3s 132150K .......... .......... .......... .......... .......... 50% 53.5M 3s 132200K .......... .......... .......... .......... .......... 50% 55.3M 3s 132250K .......... .......... .......... .......... .......... 50% 61.4M 3s 132300K .......... .......... .......... .......... .......... 50% 54.7M 3s 132350K .......... .......... .......... .......... .......... 50% 53.1M 3s 132400K .......... .......... .......... .......... .......... 50% 54.6M 3s 132450K .......... .......... 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.......... 51% 46.2M 3s 133800K .......... .......... .......... .......... .......... 51% 287M 3s 133850K .......... .......... .......... .......... .......... 51% 86.9M 3s 133900K .......... .......... .......... .......... .......... 51% 376M 3s 133950K .......... .......... .......... .......... .......... 51% 34.4M 3s 134000K .......... .......... .......... .......... .......... 51% 31.8M 3s 134050K .......... .......... .......... .......... .......... 51% 388M 3s 134100K .......... .......... .......... .......... .......... 51% 456M 3s 134150K .......... .......... .......... .......... .......... 51% 381M 2s 134200K .......... .......... .......... .......... .......... 51% 52.8M 2s 134250K .......... .......... .......... .......... .......... 51% 59.0M 2s 134300K .......... .......... .......... .......... .......... 51% 64.2M 2s 134350K .......... .......... .......... .......... .......... 51% 54.3M 2s 134400K .......... .......... .......... .......... .......... 51% 64.9M 2s 134450K .......... .......... .......... .......... .......... 51% 53.0M 2s 134500K .......... .......... .......... .......... .......... 51% 63.0M 2s 134550K .......... .......... .......... .......... .......... 51% 62.4M 2s 134600K .......... .......... .......... .......... .......... 51% 54.4M 2s 134650K .......... .......... .......... .......... .......... 51% 97.3M 2s 134700K .......... .......... .......... .......... .......... 51% 53.1M 2s 134750K .......... .......... .......... .......... .......... 51% 62.2M 2s 134800K .......... .......... .......... .......... .......... 51% 54.5M 2s 134850K .......... .......... .......... .......... .......... 51% 61.5M 2s 134900K .......... .......... .......... .......... .......... 51% 55.1M 2s 134950K .......... .......... .......... .......... .......... 51% 60.6M 2s 135000K .......... .......... .......... .......... .......... 51% 81.8M 2s 135050K .......... .......... .......... .......... .......... 51% 63.0M 2s 135100K .......... .......... .......... .......... .......... 51% 54.4M 2s 135150K .......... .......... .......... .......... .......... 51% 62.2M 2s 135200K .......... .......... .......... .......... .......... 51% 54.9M 2s 135250K .......... .......... .......... .......... .......... 51% 62.0M 2s 135300K .......... .......... .......... .......... .......... 51% 54.4M 2s 135350K .......... .......... .......... .......... .......... 51% 54.6M 2s 135400K .......... .......... .......... .......... .......... 51% 120M 2s 135450K .......... .......... .......... .......... .......... 51% 47.9M 2s 135500K .......... .......... .......... .......... .......... 51% 62.1M 2s 135550K .......... .......... .......... .......... .......... 51% 63.2M 2s 135600K .......... .......... .......... .......... .......... 51% 61.6M 2s 135650K .......... .......... .......... .......... .......... 51% 55.4M 2s 135700K .......... .......... .......... .......... .......... 51% 53.4M 2s 135750K .......... .......... .......... .......... .......... 51% 54.7M 2s 135800K .......... .......... .......... .......... .......... 51% 74.5M 2s 135850K .......... .......... .......... .......... .......... 51% 54.9M 2s 135900K .......... .......... .......... .......... .......... 51% 94.3M 2s 135950K .......... .......... .......... .......... .......... 51% 54.4M 2s 136000K .......... .......... .......... .......... .......... 51% 57.9M 2s 136050K .......... .......... .......... .......... .......... 51% 53.2M 2s 136100K .......... .......... .......... .......... .......... 51% 52.5M 2s 136150K .......... .......... .......... .......... .......... 51% 61.1M 2s 136200K .......... .......... .......... .......... .......... 51% 50.9M 2s 136250K .......... .......... .......... .......... .......... 51% 127M 2s 136300K .......... .......... .......... .......... .......... 52% 47.1M 2s 136350K .......... .......... .......... .......... .......... 52% 15.1M 2s 136400K .......... 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.......... .......... .......... 52% 52.7M 2s 137100K .......... .......... .......... .......... .......... 52% 33.2M 2s 137150K .......... .......... .......... .......... .......... 52% 47.0M 2s 137200K .......... .......... .......... .......... .......... 52% 29.4M 2s 137250K .......... .......... .......... .......... .......... 52% 47.0M 2s 137300K .......... .......... .......... .......... .......... 52% 32.1M 2s 137350K .......... .......... .......... .......... .......... 52% 46.1M 2s 137400K .......... .......... .......... .......... .......... 52% 47.2M 2s 137450K .......... .......... .......... .......... .......... 52% 31.9M 2s 137500K .......... .......... .......... .......... .......... 52% 47.5M 2s 137550K .......... .......... .......... .......... .......... 52% 31.7M 2s 137600K .......... .......... .......... .......... .......... 52% 42.9M 2s 137650K .......... .......... .......... .......... .......... 52% 46.4M 2s 137700K .......... .......... .......... .......... .......... 52% 11.1M 2s 137750K .......... .......... .......... .......... .......... 52% 31.7M 2s 137800K .......... .......... .......... .......... .......... 52% 48.2M 2s 137850K .......... .......... .......... .......... .......... 52% 46.5M 2s 137900K .......... .......... .......... .......... .......... 52% 32.3M 2s 137950K .......... .......... .......... .......... .......... 52% 47.8M 2s 138000K .......... .......... .......... .......... .......... 52% 35.3M 2s 138050K .......... .......... .......... .......... .......... 52% 42.2M 2s 138100K .......... .......... .......... .......... .......... 52% 46.9M 2s 138150K .......... .......... .......... .......... .......... 52% 20.8M 2s 138200K .......... .......... .......... .......... .......... 52% 93.4M 2s 138250K .......... .......... .......... .......... .......... 52% 127M 2s 138300K .......... .......... .......... .......... .......... 52% 45.8M 2s 138350K .......... .......... .......... .......... .......... 52% 364M 2s 138400K .......... .......... .......... .......... .......... 52% 30.6M 2s 138450K .......... .......... .......... .......... .......... 52% 101M 2s 138500K .......... .......... .......... .......... .......... 52% 38.3M 2s 138550K .......... .......... .......... .......... .......... 52% 46.4M 2s 138600K .......... .......... .......... .......... .......... 52% 47.0M 2s 138650K .......... .......... .......... .......... .......... 52% 38.8M 2s 138700K .......... .......... .......... .......... .......... 52% 47.0M 2s 138750K .......... .......... .......... .......... .......... 52% 42.0M 2s 138800K .......... .......... .......... .......... .......... 52% 47.7M 2s 138850K .......... .......... .......... .......... .......... 52% 37.6M 2s 138900K .......... .......... .......... .......... .......... 52% 54.8M 2s 138950K .......... .......... .......... .......... .......... 53% 33.4M 2s 139000K .......... .......... .......... .......... .......... 53% 51.8M 2s 139050K .......... .......... .......... .......... .......... 53% 40.7M 2s 139100K .......... .......... .......... .......... .......... 53% 44.8M 2s 139150K .......... .......... .......... .......... .......... 53% 41.7M 2s 139200K .......... .......... .......... .......... .......... 53% 37.6M 2s 139250K .......... .......... .......... .......... .......... 53% 41.5M 2s 139300K .......... .......... .......... .......... .......... 53% 53.4M 2s 139350K .......... .......... .......... .......... .......... 53% 46.9M 2s 139400K .......... .......... .......... .......... .......... 53% 52.7M 2s 139450K .......... .......... .......... .......... .......... 53% 31.9M 2s 139500K .......... .......... .......... .......... .......... 53% 47.3M 2s 139550K .......... .......... .......... .......... .......... 53% 53.8M 2s 139600K .......... .......... .......... .......... .......... 53% 42.1M 2s 139650K .......... .......... .......... .......... .......... 53% 53.4M 2s 139700K .......... .......... .......... .......... .......... 53% 31.5M 2s 139750K .......... .......... .......... .......... .......... 53% 58.8M 2s 139800K .......... .......... .......... .......... .......... 53% 48.4M 2s 139850K .......... .......... .......... .......... .......... 53% 47.1M 2s 139900K .......... .......... .......... .......... .......... 53% 30.7M 2s 139950K .......... .......... .......... .......... .......... 53% 41.2M 2s 140000K .......... .......... .......... .......... .......... 53% 31.2M 2s 140050K .......... .......... .......... .......... .......... 53% 13.9M 2s 140100K .......... .......... .......... .......... .......... 53% 158M 2s 140150K .......... .......... .......... .......... .......... 53% 49.5M 2s 140200K .......... .......... .......... .......... .......... 53% 37.3M 2s 140250K .......... .......... .......... .......... .......... 53% 52.7M 2s 140300K .......... .......... .......... .......... .......... 53% 47.2M 2s 140350K .......... .......... .......... .......... .......... 53% 42.9M 2s 140400K .......... .......... .......... .......... .......... 53% 46.1M 2s 140450K .......... .......... .......... .......... .......... 53% 51.1M 2s 140500K .......... .......... .......... .......... .......... 53% 46.6M 2s 140550K .......... .......... .......... .......... .......... 53% 45.4M 2s 140600K .......... .......... .......... .......... .......... 53% 47.1M 2s 140650K .......... .......... .......... .......... .......... 53% 47.0M 2s 140700K .......... .......... .......... .......... .......... 53% 26.9M 2s 140750K .......... .......... .......... .......... .......... 53% 53.4M 2s 140800K .......... .......... .......... .......... .......... 53% 41.9M 2s 140850K .......... .......... .......... .......... .......... 53% 46.8M 2s 140900K .......... .......... .......... .......... .......... 53% 48.1M 2s 140950K .......... .......... .......... .......... .......... 53% 54.6M 2s 141000K .......... .......... .......... .......... .......... 53% 61.2M 2s 141050K .......... .......... .......... .......... .......... 53% 47.9M 2s 141100K .......... .......... .......... .......... .......... 53% 42.7M 2s 141150K .......... .......... .......... .......... .......... 53% 72.0M 2s 141200K .......... .......... .......... .......... .......... 53% 46.4M 2s 141250K .......... .......... .......... .......... .......... 53% 53.2M 2s 141300K .......... .......... .......... .......... .......... 53% 53.5M 2s 141350K .......... .......... .......... .......... .......... 53% 53.1M 2s 141400K .......... .......... .......... .......... .......... 53% 52.3M 2s 141450K .......... .......... .......... .......... .......... 53% 46.0M 2s 141500K .......... .......... .......... .......... .......... 53% 48.2M 2s 141550K .......... .......... .......... .......... .......... 54% 52.5M 2s 141600K .......... .......... .......... .......... .......... 54% 33.8M 2s 141650K .......... .......... .......... .......... .......... 54% 100M 2s 141700K .......... .......... .......... .......... .......... 54% 34.2M 2s 141750K .......... .......... .......... .......... .......... 54% 94.3M 2s 141800K .......... .......... .......... .......... .......... 54% 54.1M 2s 141850K .......... .......... .......... .......... .......... 54% 32.9M 2s 141900K .......... .......... .......... .......... .......... 54% 72.8M 2s 141950K .......... .......... .......... .......... .......... 54% 268M 2s 142000K .......... .......... .......... .......... .......... 54% 29.1M 2s 142050K .......... .......... .......... .......... .......... 54% 444M 2s 142100K .......... .......... .......... .......... .......... 54% 397M 2s 142150K .......... .......... .......... .......... .......... 54% 106M 2s 142200K .......... .......... .......... .......... .......... 54% 52.7M 2s 142250K .......... .......... .......... .......... .......... 54% 95.9M 2s 142300K .......... .......... .......... .......... .......... 54% 62.5M 2s 142350K .......... .......... .......... .......... .......... 54% 62.4M 2s 142400K .......... .......... .......... .......... .......... 54% 71.2M 2s 142450K .......... .......... .......... .......... .......... 54% 55.6M 2s 142500K .......... .......... .......... .......... .......... 54% 94.8M 2s 142550K .......... .......... .......... .......... .......... 54% 75.1M 2s 142600K .......... .......... .......... .......... .......... 54% 61.0M 2s 142650K .......... .......... .......... .......... .......... 54% 63.3M 2s 142700K .......... .......... .......... .......... .......... 54% 64.4M 2s 142750K .......... .......... .......... .......... .......... 54% 64.8M 2s 142800K .......... .......... .......... .......... .......... 54% 71.1M 2s 142850K .......... .......... .......... .......... .......... 54% 64.3M 2s 142900K .......... .......... .......... .......... .......... 54% 65.5M 2s 142950K .......... .......... .......... .......... .......... 54% 89.8M 2s 143000K .......... .......... .......... .......... .......... 54% 64.6M 2s 143050K .......... .......... .......... .......... .......... 54% 63.6M 2s 143100K .......... .......... .......... .......... .......... 54% 62.5M 2s 143150K .......... .......... .......... .......... .......... 54% 111M 2s 143200K .......... .......... .......... .......... .......... 54% 56.2M 2s 143250K .......... .......... .......... .......... .......... 54% 72.7M 2s 143300K .......... .......... .......... .......... .......... 54% 57.4M 2s 143350K .......... .......... .......... .......... .......... 54% 63.1M 2s 143400K .......... .......... .......... .......... .......... 54% 122M 2s 143450K .......... .......... .......... .......... .......... 54% 51.6M 2s 143500K .......... .......... .......... .......... .......... 54% 71.7M 2s 143550K .......... .......... .......... .......... .......... 54% 69.9M 2s 143600K .......... .......... .......... .......... .......... 54% 70.5M 2s 143650K .......... .......... .......... .......... .......... 54% 63.3M 2s 143700K .......... .......... .......... .......... .......... 54% 62.0M 2s 143750K .......... .......... .......... .......... .......... 54% 55.5M 2s 143800K .......... .......... .......... .......... .......... 54% 64.1M 2s 143850K .......... .......... .......... .......... .......... 54% 60.3M 2s 143900K .......... .......... .......... .......... .......... 54% 124M 2s 143950K .......... .......... .......... .......... .......... 54% 55.4M 2s 144000K .......... .......... .......... .......... .......... 54% 73.8M 2s 144050K .......... .......... .......... .......... .......... 54% 63.6M 2s 144100K .......... .......... .......... .......... .......... 54% 77.6M 2s 144150K .......... .......... .......... .......... .......... 54% 52.8M 2s 144200K .......... .......... .......... .......... .......... 55% 56.1M 2s 144250K .......... .......... .......... .......... .......... 55% 63.9M 2s 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.......... .......... .......... .......... .......... 55% 98.2M 2s 145000K .......... .......... .......... .......... .......... 55% 233M 2s 145050K .......... .......... .......... .......... .......... 55% 80.0M 2s 145100K .......... .......... .......... .......... .......... 55% 72.1M 2s 145150K .......... .......... .......... .......... .......... 55% 52.6M 2s 145200K .......... .......... .......... .......... .......... 55% 381M 2s 145250K .......... .......... .......... .......... .......... 55% 341M 2s 145300K .......... .......... .......... .......... .......... 55% 108M 2s 145350K .......... .......... .......... .......... .......... 55% 54.0M 2s 145400K .......... .......... .......... .......... .......... 55% 64.4M 2s 145450K .......... .......... .......... .......... .......... 55% 76.3M 2s 145500K .......... .......... .......... .......... .......... 55% 63.4M 2s 145550K .......... .......... .......... .......... .......... 55% 76.2M 2s 145600K .......... 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30.9M 2s 148250K .......... .......... .......... .......... .......... 56% 452M 2s 148300K .......... .......... .......... .......... .......... 56% 53.9M 2s 148350K .......... .......... .......... .......... .......... 56% 47.6M 2s 148400K .......... .......... .......... .......... .......... 56% 61.6M 2s 148450K .......... .......... .......... .......... .......... 56% 53.5M 2s 148500K .......... .......... .......... .......... .......... 56% 54.0M 2s 148550K .......... .......... .......... .......... .......... 56% 54.6M 2s 148600K .......... .......... .......... .......... .......... 56% 62.0M 2s 148650K .......... .......... .......... .......... .......... 56% 55.2M 2s 148700K .......... .......... .......... .......... .......... 56% 54.0M 2s 148750K .......... .......... .......... .......... .......... 56% 54.0M 2s 148800K .......... .......... .......... .......... .......... 56% 62.0M 2s 148850K .......... .......... .......... .......... .......... 56% 53.7M 2s 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.......... 68% 54.1M 2s 179800K .......... .......... .......... .......... .......... 68% 46.5M 2s 179850K .......... .......... .......... .......... .......... 68% 37.5M 2s 179900K .......... .......... .......... .......... .......... 68% 48.2M 2s 179950K .......... .......... .......... .......... .......... 68% 53.2M 2s 180000K .......... .......... .......... .......... .......... 68% 42.4M 2s 180050K .......... .......... .......... .......... .......... 68% 37.9M 2s 180100K .......... .......... .......... .......... .......... 68% 119M 2s 180150K .......... .......... .......... .......... .......... 68% 32.1M 2s 180200K .......... .......... .......... .......... .......... 68% 21.8M 2s 180250K .......... .......... .......... .......... .......... 68% 359M 2s 180300K .......... .......... .......... .......... .......... 68% 41.2M 2s 180350K .......... .......... .......... .......... .......... 68% 128M 2s 180400K .......... .......... .......... .......... .......... 68% 52.3M 2s 180450K .......... .......... .......... .......... .......... 68% 66.1M 2s 180500K .......... .......... .......... .......... .......... 68% 182M 2s 180550K .......... .......... .......... .......... .......... 68% 59.1M 2s 180600K .......... .......... .......... .......... .......... 68% 250M 2s 180650K .......... .......... .......... .......... .......... 68% 51.6M 2s 180700K .......... .......... .......... .......... .......... 68% 50.4M 2s 180750K .......... .......... .......... .......... .......... 68% 53.9M 2s 180800K .......... .......... .......... .......... .......... 68% 51.2M 2s 180850K .......... .......... .......... .......... .......... 68% 31.8M 2s 180900K .......... .......... .......... .......... .......... 69% 54.7M 2s 180950K .......... .......... .......... .......... .......... 69% 53.8M 2s 181000K .......... .......... .......... .......... .......... 69% 52.8M 2s 181050K .......... .......... .......... .......... .......... 69% 48.1M 2s 181100K .......... .......... .......... .......... .......... 69% 41.6M 2s 181150K .......... .......... .......... .......... .......... 69% 48.8M 2s 181200K .......... .......... .......... .......... .......... 69% 46.8M 2s 181250K .......... .......... .......... .......... .......... 69% 47.8M 2s 181300K .......... .......... .......... .......... .......... 69% 63.4M 2s 181350K .......... .......... .......... .......... .......... 69% 37.6M 2s 181400K .......... .......... .......... .......... .......... 69% 54.7M 2s 181450K .......... .......... .......... .......... .......... 69% 37.8M 2s 181500K .......... .......... .......... .......... .......... 69% 47.2M 2s 181550K .......... .......... .......... .......... .......... 69% 51.1M 2s 181600K .......... .......... .......... .......... .......... 69% 54.3M 2s 181650K .......... .......... .......... .......... .......... 69% 53.2M 2s 181700K .......... .......... .......... .......... .......... 69% 48.1M 2s 181750K .......... .......... .......... .......... .......... 69% 55.0M 2s 181800K .......... .......... .......... .......... .......... 69% 54.5M 2s 181850K .......... .......... .......... .......... .......... 69% 47.1M 2s 181900K .......... .......... .......... .......... .......... 69% 54.7M 2s 181950K .......... .......... .......... .......... .......... 69% 47.3M 2s 182000K .......... .......... .......... .......... .......... 69% 53.5M 2s 182050K .......... .......... .......... .......... .......... 69% 54.9M 2s 182100K .......... .......... .......... .......... .......... 69% 48.1M 2s 182150K .......... .......... .......... .......... .......... 69% 53.2M 2s 182200K .......... .......... .......... .......... .......... 69% 34.6M 2s 182250K .......... .......... .......... .......... .......... 69% 90.9M 2s 182300K .......... .......... .......... .......... .......... 69% 54.3M 2s 182350K .......... .......... .......... .......... .......... 69% 45.7M 2s 182400K .......... 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.......... .......... .......... 73% 54.6M 1s 192300K .......... .......... .......... .......... .......... 73% 59.3M 1s 192350K .......... .......... .......... .......... .......... 73% 39.3M 1s 192400K .......... .......... .......... .......... .......... 73% 42.3M 1s 192450K .......... .......... .......... .......... .......... 73% 53.0M 1s 192500K .......... .......... .......... .......... .......... 73% 55.7M 1s 192550K .......... .......... .......... .......... .......... 73% 53.4M 1s 192600K .......... .......... .......... .......... .......... 73% 45.9M 1s 192650K .......... .......... .......... .......... .......... 73% 53.8M 1s 192700K .......... .......... .......... .......... .......... 73% 53.4M 1s 192750K .......... .......... .......... .......... .......... 73% 55.0M 1s 192800K .......... .......... .......... .......... .......... 73% 53.8M 1s 192850K .......... .......... .......... .......... .......... 73% 47.2M 1s 192900K .......... .......... .......... 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.......... 73% 88.0M 1s 193600K .......... .......... .......... .......... .......... 73% 42.3M 1s 193650K .......... .......... .......... .......... .......... 73% 88.8M 1s 193700K .......... .......... .......... .......... .......... 73% 212M 1s 193750K .......... .......... .......... .......... .......... 73% 54.1M 1s 193800K .......... .......... .......... .......... .......... 73% 55.8M 1s 193850K .......... .......... .......... .......... .......... 73% 48.3M 1s 193900K .......... .......... .......... .......... .......... 73% 52.2M 1s 193950K .......... .......... .......... .......... .......... 73% 54.1M 1s 194000K .......... .......... .......... .......... .......... 74% 52.0M 1s 194050K .......... .......... .......... .......... .......... 74% 53.4M 1s 194100K .......... .......... .......... .......... .......... 74% 103M 1s 194150K .......... .......... .......... .......... .......... 74% 53.2M 1s 194200K .......... .......... .......... .......... .......... 74% 48.0M 1s 194250K .......... .......... .......... .......... .......... 74% 54.1M 1s 194300K .......... .......... .......... .......... .......... 74% 54.0M 1s 194350K .......... .......... .......... .......... .......... 74% 51.7M 1s 194400K .......... .......... .......... .......... .......... 74% 53.1M 1s 194450K .......... .......... .......... .......... .......... 74% 47.7M 1s 194500K .......... .......... .......... .......... .......... 74% 58.7M 1s 194550K .......... .......... .......... .......... .......... 74% 50.5M 1s 194600K .......... .......... .......... .......... .......... 74% 54.0M 1s 194650K .......... .......... .......... .......... .......... 74% 52.6M 1s 194700K .......... .......... .......... .......... .......... 74% 53.4M 1s 194750K .......... .......... .......... .......... .......... 74% 96.9M 1s 194800K .......... .......... .......... .......... .......... 74% 53.6M 1s 194850K .......... .......... .......... .......... .......... 74% 54.0M 1s 194900K .......... .......... .......... .......... .......... 74% 52.5M 1s 194950K .......... .......... .......... .......... .......... 74% 47.8M 1s 195000K .......... .......... .......... .......... .......... 74% 54.1M 1s 195050K .......... .......... .......... .......... .......... 74% 53.5M 1s 195100K .......... .......... .......... .......... .......... 74% 54.0M 1s 195150K .......... .......... .......... .......... .......... 74% 54.5M 1s 195200K .......... .......... .......... .......... .......... 74% 46.5M 1s 195250K .......... .......... .......... .......... .......... 74% 124M 1s 195300K .......... .......... .......... .......... .......... 74% 52.4M 1s 195350K .......... .......... .......... .......... .......... 74% 54.6M 1s 195400K .......... .......... .......... .......... .......... 74% 48.5M 1s 195450K .......... .......... .......... .......... .......... 74% 51.9M 1s 195500K .......... .......... .......... .......... .......... 74% 52.2M 1s 195550K 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75% 76.1M 1s 198850K .......... .......... .......... .......... .......... 75% 48.2M 1s 198900K .......... .......... .......... .......... .......... 75% 124M 1s 198950K .......... .......... .......... .......... .......... 75% 41.7M 1s 199000K .......... .......... .......... .......... .......... 75% 25.2M 1s 199050K .......... .......... .......... .......... .......... 75% 519M 1s 199100K .......... .......... .......... .......... .......... 75% 514M 1s 199150K .......... .......... .......... .......... .......... 75% 29.3M 1s 199200K .......... .......... .......... .......... .......... 75% 182M 1s 199250K .......... .......... .......... .......... .......... 76% 537M 1s 199300K .......... .......... .......... .......... .......... 76% 31.2M 1s 199350K .......... .......... .......... .......... .......... 76% 151M 1s 199400K .......... .......... .......... .......... .......... 76% 80.4M 1s 199450K .......... .......... .......... .......... .......... 76% 43.1M 1s 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.......... .......... .......... 78% 89.8M 1s 206100K .......... .......... .......... .......... .......... 78% 46.8M 1s 206150K .......... .......... .......... .......... .......... 78% 138M 1s 206200K .......... .......... .......... .......... .......... 78% 41.6M 1s 206250K .......... .......... .......... .......... .......... 78% 181M 1s 206300K .......... .......... .......... .......... .......... 78% 47.9M 1s 206350K .......... .......... .......... .......... .......... 78% 125M 1s 206400K .......... .......... .......... .......... .......... 78% 71.8M 1s 206450K .......... .......... .......... .......... .......... 78% 54.5M 1s 206500K .......... .......... .......... .......... .......... 78% 216M 1s 206550K .......... .......... .......... .......... .......... 78% 51.3M 1s 206600K .......... .......... .......... .......... .......... 78% 41.4M 1s 206650K .......... .......... .......... .......... .......... 78% 42.1M 1s 206700K .......... .......... .......... 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.......... 84% 21.6M 1s 220550K .......... .......... .......... .......... .......... 84% 208M 1s 220600K .......... .......... .......... .......... .......... 84% 45.0M 1s 220650K .......... .......... .......... .......... .......... 84% 432M 1s 220700K .......... .......... .......... .......... .......... 84% 30.7M 1s 220750K .......... .......... .......... .......... .......... 84% 107M 1s 220800K .......... .......... .......... .......... .......... 84% 28.6M 1s 220850K .......... .......... .......... .......... .......... 84% 470M 1s 220900K .......... .......... .......... .......... .......... 84% 568M 1s 220950K .......... .......... .......... .......... .......... 84% 47.2M 1s 221000K .......... .......... .......... .......... .......... 84% 69.7M 1s 221050K .......... .......... .......... .......... .......... 84% 31.4M 1s 221100K .......... .......... .......... .......... .......... 84% 47.0M 1s 221150K .......... .......... .......... .......... .......... 84% 32.3M 1s 221200K .......... .......... .......... .......... .......... 84% 35.9M 1s 221250K .......... .......... .......... .......... .......... 84% 38.4M 1s 221300K .......... .......... .......... .......... .......... 84% 46.7M 1s 221350K .......... .......... .......... .......... .......... 84% 35.9M 1s 221400K .......... .......... .......... .......... .......... 84% 45.6M 1s 221450K .......... .......... .......... .......... .......... 84% 33.4M 1s 221500K .......... .......... .......... .......... .......... 84% 39.7M 1s 221550K .......... .......... .......... .......... .......... 84% 44.4M 1s 221600K .......... .......... .......... .......... .......... 84% 33.9M 1s 221650K .......... .......... .......... .......... .......... 84% 46.6M 1s 221700K .......... .......... .......... .......... .......... 84% 46.2M 1s 221750K .......... .......... .......... .......... .......... 84% 29.1M 1s 221800K .......... .......... .......... .......... .......... 84% 41.6M 1s 221850K .......... .......... .......... .......... .......... 84% 39.6M 1s 221900K .......... .......... .......... .......... .......... 84% 49.7M 1s 221950K .......... .......... .......... .......... .......... 84% 34.2M 1s 222000K .......... .......... .......... .......... .......... 84% 48.5M 1s 222050K .......... .......... .......... .......... .......... 84% 51.5M 1s 222100K .......... .......... .......... .......... .......... 84% 35.3M 1s 222150K .......... .......... .......... .......... .......... 84% 55.2M 1s 222200K .......... .......... .......... .......... .......... 84% 51.8M 1s 222250K .......... .......... .......... .......... .......... 84% 46.0M 1s 222300K .......... .......... .......... .......... .......... 84% 54.0M 1s 222350K .......... .......... .......... .......... .......... 84% 28.7M 1s 222400K .......... .......... .......... .......... .......... 84% 33.8M 1s 222450K .......... .......... .......... .......... .......... 84% 23.0M 1s 222500K .......... .......... .......... .......... .......... 84% 27.4M 1s 222550K .......... .......... .......... .......... .......... 84% 22.1M 1s 222600K .......... .......... .......... .......... .......... 84% 20.2M 1s 222650K .......... .......... .......... .......... .......... 84% 26.2M 1s 222700K .......... .......... .......... .......... .......... 84% 22.9M 1s 222750K .......... .......... .......... .......... .......... 84% 20.9M 1s 222800K .......... .......... .......... .......... .......... 84% 23.8M 1s 222850K .......... .......... .......... .......... .......... 85% 23.4M 1s 222900K .......... .......... .......... .......... .......... 85% 27.5M 1s 222950K .......... .......... .......... .......... .......... 85% 22.3M 1s 223000K .......... .......... .......... .......... .......... 85% 28.0M 1s 223050K .......... .......... .......... .......... .......... 85% 20.7M 1s 223100K .......... .......... .......... .......... .......... 85% 27.1M 1s 223150K .......... .......... .......... .......... .......... 85% 27.1M 1s 223200K .......... .......... .......... .......... .......... 85% 18.7M 1s 223250K .......... .......... .......... .......... .......... 85% 31.0M 1s 223300K .......... .......... .......... .......... .......... 85% 20.1M 1s 223350K .......... .......... .......... .......... .......... 85% 37.8M 1s 223400K .......... .......... .......... .......... .......... 85% 41.9M 1s 223450K .......... .......... .......... .......... .......... 85% 28.8M 1s 223500K .......... .......... .......... .......... .......... 85% 126M 1s 223550K .......... .......... .......... .......... .......... 85% 46.7M 1s 223600K .......... .......... .......... .......... .......... 85% 21.9M 1s 223650K .......... .......... .......... .......... .......... 85% 267M 1s 223700K .......... .......... .......... .......... .......... 85% 36.7M 1s 223750K .......... .......... .......... .......... .......... 85% 394M 1s 223800K .......... .......... .......... .......... .......... 85% 31.3M 1s 223850K .......... .......... .......... .......... .......... 85% 50.9M 1s 223900K .......... .......... .......... .......... .......... 85% 54.1M 1s 223950K .......... .......... .......... .......... .......... 85% 46.5M 1s 224000K .......... .......... .......... .......... .......... 85% 29.4M 1s 224050K .......... .......... .......... .......... .......... 85% 53.8M 1s 224100K .......... .......... .......... .......... .......... 85% 43.0M 1s 224150K .......... .......... .......... .......... .......... 85% 47.3M 1s 224200K .......... .......... .......... .......... .......... 85% 30.1M 1s 224250K .......... .......... .......... .......... .......... 85% 47.9M 1s 224300K .......... .......... .......... .......... .......... 85% 46.9M 1s 224350K .......... .......... .......... .......... .......... 85% 45.5M 1s 224400K .......... .......... .......... .......... .......... 85% 48.5M 1s 224450K .......... .......... .......... 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.......... 85% 36.1M 1s 225150K .......... .......... .......... .......... .......... 85% 46.1M 1s 225200K .......... .......... .......... .......... .......... 85% 46.4M 1s 225250K .......... .......... .......... .......... .......... 85% 31.8M 1s 225300K .......... .......... .......... .......... .......... 85% 54.3M 1s 225350K .......... .......... .......... .......... .......... 85% 42.2M 1s 225400K .......... .......... .......... .......... .......... 85% 54.1M 1s 225450K .......... .......... .......... .......... .......... 86% 41.9M 1s 225500K .......... .......... .......... .......... .......... 86% 42.1M 1s 225550K .......... .......... .......... .......... .......... 86% 17.0M 1s 225600K .......... .......... .......... .......... .......... 86% 349M 1s 225650K .......... .......... .......... .......... .......... 86% 465M 1s 225700K .......... .......... .......... .......... .......... 86% 21.8M 1s 225750K .......... .......... .......... .......... .......... 86% 72.1M 1s 225800K .......... .......... .......... .......... .......... 86% 135M 1s 225850K .......... .......... .......... .......... .......... 86% 36.4M 1s 225900K .......... .......... .......... .......... .......... 86% 64.0M 1s 225950K .......... .......... .......... .......... .......... 86% 42.1M 1s 226000K .......... .......... .......... .......... .......... 86% 53.8M 1s 226050K .......... .......... .......... .......... .......... 86% 31.6M 1s 226100K .......... .......... .......... .......... .......... 86% 48.5M 1s 226150K .......... .......... .......... .......... .......... 86% 52.4M 1s 226200K .......... .......... .......... .......... .......... 86% 47.7M 1s 226250K .......... .......... .......... .......... .......... 86% 47.9M 1s 226300K .......... .......... .......... .......... .......... 86% 53.1M 1s 226350K .......... .......... .......... .......... .......... 86% 29.5M 1s 226400K .......... .......... .......... .......... .......... 86% 47.3M 1s 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.......... .......... .......... .......... .......... 86% 31.2M 1s 227150K .......... .......... .......... .......... .......... 86% 48.9M 1s 227200K .......... .......... .......... .......... .......... 86% 50.5M 1s 227250K .......... .......... .......... .......... .......... 86% 48.1M 1s 227300K .......... .......... .......... .......... .......... 86% 51.7M 1s 227350K .......... .......... .......... .......... .......... 86% 31.3M 1s 227400K .......... .......... .......... .......... .......... 86% 49.7M 1s 227450K .......... .......... .......... .......... .......... 86% 41.2M 1s 227500K .......... .......... .......... .......... .......... 86% 97.7M 1s 227550K .......... .......... .......... .......... .......... 86% 16.8M 1s 227600K .......... .......... .......... .......... .......... 86% 79.4M 1s 227650K .......... .......... .......... .......... .......... 86% 29.2M 1s 227700K .......... .......... .......... .......... .......... 86% 41.2M 1s 227750K .......... 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.......... 87% 42.2M 1s 229750K .......... .......... .......... .......... .......... 87% 28.7M 1s 229800K .......... .......... .......... .......... .......... 87% 41.8M 1s 229850K .......... .......... .......... .......... .......... 87% 30.0M 1s 229900K .......... .......... .......... .......... .......... 87% 46.1M 1s 229950K .......... .......... .......... .......... .......... 87% 27.7M 1s 230000K .......... .......... .......... .......... .......... 87% 31.2M 1s 230050K .......... .......... .......... .......... .......... 87% 45.2M 1s 230100K .......... .......... .......... .......... .......... 87% 27.1M 1s 230150K .......... .......... .......... .......... .......... 87% 39.4M 1s 230200K .......... .......... .......... .......... .......... 87% 26.4M 1s 230250K .......... .......... .......... .......... .......... 87% 39.5M 1s 230300K .......... .......... .......... .......... .......... 87% 31.2M 1s 230350K .......... .......... .......... .......... .......... 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.......... .......... .......... .......... .......... 88% 29.4M 1s 231750K .......... .......... .......... .......... .......... 88% 46.7M 1s 231800K .......... .......... .......... .......... .......... 88% 29.2M 1s 231850K .......... .......... .......... .......... .......... 88% 44.2M 1s 231900K .......... .......... .......... .......... .......... 88% 29.1M 1s 231950K .......... .......... .......... .......... .......... 88% 36.8M 1s 232000K .......... .......... .......... .......... .......... 88% 41.9M 1s 232050K .......... .......... .......... .......... .......... 88% 116M 1s 232100K .......... .......... .......... .......... .......... 88% 29.7M 1s 232150K .......... .......... .......... .......... .......... 88% 22.8M 1s 232200K .......... .......... .......... .......... .......... 88% 34.9M 1s 232250K .......... .......... .......... .......... .......... 88% 119M 1s 232300K .......... .......... .......... .......... .......... 88% 41.6M 1s 232350K .......... 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.......... .......... 89% 52.5M 1s 233700K .......... .......... .......... .......... .......... 89% 31.6M 1s 233750K .......... .......... .......... .......... .......... 89% 48.0M 1s 233800K .......... .......... .......... .......... .......... 89% 61.0M 1s 233850K .......... .......... .......... .......... .......... 89% 42.5M 1s 233900K .......... .......... .......... .......... .......... 89% 53.4M 1s 233950K .......... .......... .......... .......... .......... 89% 31.6M 1s 234000K .......... .......... .......... .......... .......... 89% 60.6M 1s 234050K .......... .......... .......... .......... .......... 89% 100M 1s 234100K .......... .......... .......... .......... .......... 89% 51.4M 1s 234150K .......... .......... .......... .......... .......... 89% 117M 1s 234200K .......... .......... .......... .......... .......... 89% 49.4M 1s 234250K .......... .......... .......... .......... .......... 89% 15.5M 1s 234300K .......... .......... .......... .......... .......... 89% 440M 1s 234350K .......... .......... .......... .......... .......... 89% 432M 1s 234400K .......... .......... .......... .......... .......... 89% 436M 1s 234450K .......... .......... .......... .......... .......... 89% 370M 1s 234500K .......... .......... .......... .......... .......... 89% 31.4M 1s 234550K .......... .......... .......... .......... .......... 89% 414M 1s 234600K .......... .......... .......... .......... .......... 89% 132M 1s 234650K .......... .......... .......... .......... .......... 89% 603M 1s 234700K .......... .......... .......... .......... .......... 89% 52.0M 1s 234750K .......... .......... .......... .......... .......... 89% 124M 1s 234800K .......... .......... .......... .......... .......... 89% 54.0M 1s 234850K .......... .......... .......... .......... .......... 89% 55.0M 1s 234900K .......... .......... .......... .......... .......... 89% 63.3M 1s 234950K .......... .......... .......... .......... .......... 89% 53.4M 1s 235000K .......... .......... .......... .......... .......... 89% 76.4M 1s 235050K .......... .......... .......... .......... .......... 89% 64.2M 1s 235100K .......... .......... .......... .......... .......... 89% 54.2M 1s 235150K .......... .......... .......... .......... .......... 89% 63.1M 1s 235200K .......... .......... .......... .......... .......... 89% 55.2M 1s 235250K .......... .......... .......... .......... .......... 89% 59.0M 1s 235300K .......... .......... .......... .......... .......... 89% 52.8M 1s 235350K .......... .......... .......... .......... .......... 89% 53.7M 1s 235400K .......... .......... .......... .......... .......... 89% 54.6M 1s 235450K .......... .......... .......... .......... .......... 89% 51.9M 1s 235500K .......... .......... .......... .......... .......... 89% 62.5M 1s 235550K .......... .......... .......... .......... .......... 89% 104M 1s 235600K .......... .......... .......... .......... .......... 89% 55.0M 1s 235650K .......... .......... .......... .......... .......... 89% 63.2M 1s 235700K .......... .......... .......... .......... .......... 89% 62.4M 1s 235750K .......... .......... .......... .......... .......... 89% 48.6M 1s 235800K .......... .......... .......... .......... .......... 89% 88.9M 1s 235850K .......... .......... .......... .......... .......... 89% 62.3M 1s 235900K .......... .......... .......... .......... .......... 89% 54.7M 1s 235950K .......... .......... .......... .......... .......... 90% 58.6M 1s 236000K .......... .......... .......... .......... .......... 90% 58.3M 1s 236050K .......... .......... .......... .......... .......... 90% 61.0M 1s 236100K .......... .......... .......... .......... .......... 90% 54.1M 1s 236150K .......... .......... .......... .......... .......... 90% 54.6M 1s 236200K .......... .......... .......... .......... .......... 90% 54.3M 1s 236250K .......... .......... .......... .......... .......... 90% 60.3M 1s 236300K .......... .......... .......... .......... .......... 90% 117M 1s 236350K .......... .......... .......... .......... .......... 90% 52.5M 1s 236400K .......... .......... .......... .......... .......... 90% 53.2M 1s 236450K .......... .......... .......... .......... .......... 90% 54.0M 1s 236500K .......... .......... .......... .......... .......... 90% 57.5M 1s 236550K .......... .......... .......... .......... .......... 90% 59.9M 1s 236600K .......... .......... .......... .......... .......... 90% 54.3M 1s 236650K .......... .......... .......... .......... .......... 90% 54.5M 1s 236700K .......... .......... .......... .......... .......... 90% 53.4M 1s 236750K .......... .......... .......... .......... .......... 90% 62.0M 1s 236800K .......... .......... .......... .......... .......... 90% 96.9M 1s 236850K .......... .......... .......... .......... .......... 90% 61.3M 1s 236900K .......... .......... .......... .......... .......... 90% 97.1M 1s 236950K .......... .......... .......... .......... .......... 90% 54.1M 1s 237000K .......... .......... .......... .......... .......... 90% 23.3M 1s 237050K .......... .......... .......... .......... .......... 90% 47.3M 1s 237100K .......... .......... .......... .......... .......... 90% 161M 1s 237150K .......... .......... .......... .......... .......... 90% 115M 1s 237200K .......... .......... .......... .......... .......... 90% 44.3M 0s 237250K .......... .......... .......... .......... .......... 90% 167M 0s 237300K .......... .......... .......... .......... .......... 90% 226M 0s 237350K .......... .......... .......... .......... .......... 90% 30.7M 0s 237400K .......... .......... .......... .......... .......... 90% 349M 0s 237450K .......... .......... .......... .......... .......... 90% 305M 0s 237500K .......... .......... .......... .......... .......... 90% 105M 0s 237550K .......... .......... .......... .......... .......... 90% 47.1M 0s 237600K .......... .......... .......... .......... .......... 90% 50.7M 0s 237650K .......... .......... .......... .......... .......... 90% 37.3M 0s 237700K .......... .......... .......... .......... .......... 90% 53.8M 0s 237750K .......... .......... .......... .......... .......... 90% 47.4M 0s 237800K .......... .......... .......... .......... .......... 90% 60.5M 0s 237850K .......... .......... .......... .......... .......... 90% 47.6M 0s 237900K .......... .......... .......... .......... .......... 90% 52.8M 0s 237950K .......... .......... .......... .......... .......... 90% 38.6M 0s 238000K .......... .......... .......... .......... .......... 90% 47.3M 0s 238050K .......... .......... .......... .......... .......... 90% 54.7M 0s 238100K .......... .......... .......... .......... .......... 90% 38.9M 0s 238150K .......... .......... .......... .......... .......... 90% 54.6M 0s 238200K .......... .......... .......... .......... .......... 90% 37.0M 0s 238250K .......... .......... .......... .......... .......... 90% 40.4M 0s 238300K .......... .......... .......... .......... .......... 90% 61.3M 0s 238350K .......... .......... .......... .......... .......... 90% 59.5M 0s 238400K .......... .......... .......... .......... .......... 90% 51.8M 0s 238450K .......... .......... .......... .......... .......... 90% 31.7M 0s 238500K .......... .......... .......... .......... .......... 90% 63.7M 0s 238550K .......... .......... .......... .......... .......... 91% 52.7M 0s 238600K .......... .......... .......... .......... .......... 91% 47.8M 0s 238650K .......... .......... .......... .......... .......... 91% 71.6M 0s 238700K .......... .......... .......... .......... .......... 91% 31.9M 0s 238750K .......... .......... .......... .......... .......... 91% 53.8M 0s 238800K .......... .......... .......... .......... .......... 91% 55.2M 0s 238850K .......... .......... .......... .......... .......... 91% 48.1M 0s 238900K .......... .......... .......... .......... .......... 91% 47.1M 0s 238950K .......... .......... .......... .......... .......... 91% 42.2M 0s 239000K .......... .......... .......... .......... .......... 91% 54.3M 0s 239050K .......... .......... .......... .......... .......... 91% 58.1M 0s 239100K .......... .......... .......... .......... .......... 91% 46.9M 0s 239150K .......... .......... .......... .......... .......... 91% 46.8M 0s 239200K .......... .......... .......... .......... .......... 91% 54.0M 0s 239250K .......... .......... .......... .......... .......... 91% 52.5M 0s 239300K .......... .......... .......... .......... .......... 91% 114M 0s 239350K .......... .......... .......... .......... .......... 91% 38.3M 0s 239400K .......... .......... .......... .......... .......... 91% 23.0M 0s 239450K .......... .......... .......... .......... .......... 91% 135M 0s 239500K .......... .......... .......... .......... .......... 91% 488M 0s 239550K .......... .......... .......... .......... .......... 91% 36.1M 0s 239600K .......... .......... .......... .......... .......... 91% 55.3M 0s 239650K .......... .......... .......... .......... .......... 91% 139M 0s 239700K .......... .......... .......... .......... .......... 91% 79.5M 0s 239750K .......... .......... .......... .......... .......... 91% 54.6M 0s 239800K .......... .......... .......... .......... .......... 91% 245M 0s 239850K .......... .......... .......... .......... .......... 91% 38.6M 0s 239900K .......... .......... .......... .......... .......... 91% 75.8M 0s 239950K .......... .......... .......... .......... .......... 91% 53.2M 0s 240000K .......... .......... .......... .......... .......... 91% 39.2M 0s 240050K .......... .......... .......... .......... .......... 91% 70.2M 0s 240100K .......... .......... .......... .......... .......... 91% 41.1M 0s 240150K .......... .......... .......... .......... .......... 91% 62.9M 0s 240200K .......... .......... .......... .......... .......... 91% 39.5M 0s 240250K .......... .......... .......... .......... .......... 91% 40.7M 0s 240300K .......... .......... .......... .......... .......... 91% 96.3M 0s 240350K .......... .......... .......... .......... .......... 91% 53.4M 0s 240400K .......... .......... .......... .......... .......... 91% 54.4M 0s 240450K .......... .......... .......... .......... .......... 91% 61.6M 0s 240500K .......... .......... .......... .......... .......... 91% 48.0M 0s 240550K .......... .......... .......... .......... .......... 91% 62.9M 0s 240600K .......... .......... .......... .......... .......... 91% 52.7M 0s 240650K .......... .......... .......... .......... .......... 91% 55.2M 0s 240700K .......... .......... .......... .......... .......... 91% 54.6M 0s 240750K .......... .......... .......... .......... .......... 91% 52.1M 0s 240800K .......... .......... .......... .......... .......... 91% 49.0M 0s 240850K .......... .......... .......... .......... .......... 91% 54.0M 0s 240900K .......... .......... .......... .......... .......... 91% 60.1M 0s 240950K .......... .......... .......... .......... .......... 91% 49.7M 0s 241000K .......... .......... .......... .......... .......... 91% 59.4M 0s 241050K .......... .......... .......... .......... .......... 91% 54.7M 0s 241100K .......... .......... .......... .......... .......... 91% 54.0M 0s 241150K .......... .......... .......... .......... .......... 91% 52.3M 0s 241200K .......... .......... .......... .......... .......... 92% 62.8M 0s 241250K .......... .......... .......... .......... .......... 92% 54.6M 0s 241300K .......... .......... .......... .......... .......... 92% 61.1M 0s 241350K .......... .......... .......... .......... .......... 92% 48.5M 0s 241400K .......... .......... .......... .......... .......... 92% 54.3M 0s 241450K .......... .......... .......... .......... .......... 92% 55.1M 0s 241500K .......... .......... .......... .......... .......... 92% 61.8M 0s 241550K .......... .......... .......... .......... .......... 92% 48.5M 0s 241600K .......... .......... .......... .......... .......... 92% 62.0M 0s 241650K .......... .......... .......... .......... .......... 92% 61.8M 0s 241700K .......... .......... .......... .......... .......... 92% 79.7M 0s 241750K .......... .......... .......... .......... .......... 92% 54.8M 0s 241800K .......... .......... .......... .......... .......... 92% 117M 0s 241850K .......... .......... .......... .......... .......... 92% 15.6M 0s 241900K .......... .......... .......... .......... .......... 92% 307M 0s 241950K .......... .......... .......... .......... .......... 92% 356M 0s 242000K .......... .......... .......... .......... .......... 92% 346M 0s 242050K .......... .......... .......... .......... .......... 92% 25.9M 0s 242100K .......... .......... .......... .......... .......... 92% 46.1M 0s 242150K .......... .......... .......... .......... .......... 92% 155M 0s 242200K .......... .......... .......... .......... .......... 92% 63.5M 0s 242250K .......... .......... .......... .......... .......... 92% 56.1M 0s 242300K .......... .......... .......... .......... .......... 92% 57.7M 0s 242350K .......... .......... .......... .......... .......... 92% 133M 0s 242400K .......... .......... .......... .......... .......... 92% 41.7M 0s 242450K .......... .......... .......... .......... .......... 92% 24.8M 0s 242500K .......... .......... .......... .......... .......... 92% 59.2M 0s 242550K .......... .......... .......... .......... .......... 92% 48.6M 0s 242600K .......... .......... .......... .......... .......... 92% 46.6M 0s 242650K .......... .......... .......... .......... .......... 92% 53.8M 0s 242700K .......... .......... .......... .......... .......... 92% 44.8M 0s 242750K .......... .......... .......... .......... .......... 92% 34.3M 0s 242800K .......... .......... .......... .......... .......... 92% 53.8M 0s 242850K .......... .......... .......... .......... .......... 92% 45.1M 0s 242900K .......... .......... .......... .......... .......... 92% 47.6M 0s 242950K .......... .......... .......... .......... .......... 92% 46.4M 0s 243000K .......... .......... .......... .......... .......... 92% 54.7M 0s 243050K .......... .......... .......... .......... .......... 92% 54.3M 0s 243100K .......... .......... .......... .......... .......... 92% 34.9M 0s 243150K .......... .......... .......... .......... .......... 92% 53.0M 0s 243200K .......... .......... .......... .......... .......... 92% 46.4M 0s 243250K .......... .......... .......... .......... .......... 92% 47.6M 0s 243300K .......... .......... .......... .......... .......... 92% 54.0M 0s 243350K .......... .......... .......... .......... .......... 92% 47.2M 0s 243400K .......... .......... .......... .......... .......... 92% 53.9M 0s 243450K .......... .......... .......... .......... .......... 92% 34.4M 0s 243500K .......... .......... .......... .......... .......... 92% 46.2M 0s 243550K .......... .......... .......... .......... .......... 92% 52.8M 0s 243600K .......... .......... .......... .......... .......... 92% 45.8M 0s 243650K .......... .......... .......... .......... .......... 92% 51.5M 0s 243700K .......... .......... .......... .......... .......... 92% 50.0M 0s 243750K .......... .......... .......... .......... .......... 92% 51.3M 0s 243800K .......... .......... .......... .......... .......... 93% 34.4M 0s 243850K .......... .......... .......... .......... .......... 93% 47.2M 0s 243900K .......... .......... .......... .......... .......... 93% 47.4M 0s 243950K .......... .......... .......... .......... .......... 93% 42.2M 0s 244000K .......... .......... .......... .......... .......... 93% 37.0M 0s 244050K .......... .......... .......... .......... .......... 93% 20.4M 0s 244100K .......... .......... .......... .......... .......... 93% 49.5M 0s 244150K .......... .......... .......... .......... .......... 93% 425M 0s 244200K .......... .......... .......... .......... .......... 93% 33.4M 0s 244250K .......... .......... .......... .......... .......... 93% 47.9M 0s 244300K .......... .......... .......... .......... .......... 93% 48.2M 0s 244350K .......... .......... .......... .......... .......... 93% 28.1M 0s 244400K .......... .......... .......... .......... .......... 93% 49.8M 0s 244450K .......... .......... .......... .......... .......... 93% 26.7M 0s 244500K .......... .......... .......... .......... .......... 93% 28.8M 0s 244550K .......... .......... .......... .......... .......... 93% 48.1M 0s 244600K .......... .......... .......... .......... .......... 93% 37.5M 0s 244650K .......... .......... .......... .......... .......... 93% 31.2M 0s 244700K .......... .......... .......... .......... .......... 93% 43.0M 0s 244750K .......... .......... .......... .......... .......... 93% 31.6M 0s 244800K .......... .......... .......... .......... .......... 93% 47.1M 0s 244850K .......... .......... .......... .......... .......... 93% 29.8M 0s 244900K .......... .......... .......... .......... .......... 93% 47.4M 0s 244950K .......... .......... .......... .......... .......... 93% 46.7M 0s 245000K .......... .......... .......... .......... .......... 93% 33.2M 0s 245050K .......... .......... .......... .......... .......... 93% 45.3M 0s 245100K .......... .......... .......... .......... .......... 93% 28.6M 0s 245150K .......... .......... .......... .......... .......... 93% 47.2M 0s 245200K .......... .......... .......... .......... .......... 93% 29.1M 0s 245250K .......... .......... .......... .......... .......... 93% 47.9M 0s 245300K .......... .......... .......... .......... .......... 93% 52.6M 0s 245350K .......... .......... .......... .......... .......... 93% 27.3M 0s 245400K .......... .......... .......... .......... .......... 93% 46.1M 0s 245450K .......... .......... .......... .......... .......... 93% 47.6M 0s 245500K .......... 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99% 47.4M 0s 261950K .......... .......... .......... .......... .......... 99% 34.3M 0s 262000K .......... .......... .......... .......... .......... 99% 30.7M 0s 262050K .......... .......... .......... .......... .......... 99% 46.4M 0s 262100K .......... .......... .......... .......... .......... 99% 39.2M 0s 262150K .......... .......... .......... .......... ..... 100% 31.0M=5.3s 2024-04-27 17:48:31 (48.6 MB/s) - ‘ESPbeta.tgz’ saved [268487989/268487989] + tar -xf ESPbeta.tgz + rm -rf EngSketchPad/data/Slugs + python --version Python 3.11.6 + [[ '' == *\.\i\f\o\r\t ]] + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/config/ + ./makeEnv ESP runtime AutoConfigurator CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 with contents: bin include lib share Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin/python found! Info: Python header /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11/Python.h found! Info: Python library /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib/libpython3.11.dylib found! ESP_ARCH = DARWIN_ARM64 ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad EFCOMP = gfortran CARCH = DARWIN_ARM64 CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 CASARCH = . CASREV = 7.7 PYTHONINC= /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 PYTHONLIB= -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 + source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/ESPenv.sh ++ export ESP_ARCH=DARWIN_ARM64 ++ ESP_ARCH=DARWIN_ARM64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export CASARCH=. ++ CASARCH=. ++ export CASREV=7.7 ++ CASREV=7.7 ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.7/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-3.11.6/include/python3.11 ++ PYTHONINC=/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11' ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/SLUGS/Slugs.html' ++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/ESP/ESP.html' ++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/wvClient/wv.html' ++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/wvClient/wv.html' + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src + make (cd EGADS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64 rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64 cp -p ../include/DARWIN_ARM64 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64 touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads_dot.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads_dot.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.inc rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egads.inc touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/emp.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/emp.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/prm.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/prm.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.inc rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsserver.inc touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsss.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/wsss.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTris.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsTris.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -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=7.7 uvmap/main/uvmap.c -Iuvmap \ -o ./uvmap.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 egadsUVmap.c -Iuvmap \ -o ./egadsUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a clang -g -target arm64-apple-darwin -o ./uvmap.exe ./uvmap.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib (cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.7 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a (cd .; \ ar rs /Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include fgadsBase.c -o ./fgadsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsMemory.c -o ./fgadsMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsAttrs.c -o ./fgadsAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTess.c -o ./fgadsTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsHLevel.c -o ./fgadsHLevel.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsGeom.c -o ./fgadsGeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTopo.c -o ./fgadsTopo.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libfgads.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libfgads.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/libfgads.a touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libemp.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libemp.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 ../src/egadsRobust.c \ -o ./egadsRobust.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -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=7.7 -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=7.7 -DLITE ../util/rational.c \ -o ./ratLite.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -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=7.7 -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=7.7 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o ./liteUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib (cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/include fwv.c -o ./fwv.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/include -I. -o ./servertest.o clang++ -g -target arm64-apple-darwin -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib (cd .; clang++ -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/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 7.7 \ -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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include egads2cart.c \ -o ./egads2cart.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include vCurvature.c -o ./vCurvature.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vCurvature ./vCurvature.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib (cd EGADS/examples; make -f vGeom.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include vGeom.c -o ./vGeom.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib (cd EGADS/examples; make -f vTess.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include ../util/retessFaces.c \ -o ./retessFaces.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib (cd OpenCSM; make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. tim.c -o ./tim.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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/7.7/DARWIN_ARM64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bezier.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bezier.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/biconvex.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/biconvex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/box.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/box.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bspline.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bspline.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/catmull.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/catmull.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/compare.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/compare.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createBEM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createBEM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createPoly.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createPoly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/csm.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/csm.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/deform.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/deform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/droop.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/droop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/editAttr.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/editAttr.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ellipse.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ellipse.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flend.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flend.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/freeform.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/freeform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ganged.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ganged.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/guide.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/guide.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hex.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/import.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/import.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/kulfan.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/kulfan.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/linalg.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/linalg.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mechanism.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mechanism.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nacelle.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nacelle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nuscale.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nuscale.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/offset.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/offset.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parsec.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parsec.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pod.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pod.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/poly.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/poly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBbox.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBbox.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBrep.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBrep.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printEgo.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printEgo.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/prop.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/prop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/radwaf.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/radwaf.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sample.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sample.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sew.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sew.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/shadow.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/shadow.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slices.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slices.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stag.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stag.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stiffener.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stiffener.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/supell.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/supell.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester1.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester1.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester2.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vsp3.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vsp3.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/waffle.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/waffle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/warp.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/warp.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/warp.so ./udpWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/PDT2.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/PDT2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/naca456.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ereped.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ereped.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mitten.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mitten.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plotter.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plotter.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plugs.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slugs.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/common.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/common.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udp.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udp.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/esp.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/esp.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/tim.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/tim.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egg.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/egg.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. Tessellate.c \ -o ./Tessellate.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \ ./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads \ -lpthread -lz -lm (cd CAPS; make) /bin/cp Cart3D/M1_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libc3dio.a /bin/cp Cart3D/M1_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libCart3D.a /bin/cp Executables/DARWIN_ARM64/avl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/avl /bin/cp Executables/DARWIN_ARM64/pplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/pplot /bin/cp Executables/DARWIN_ARM64/pxplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/pxplot /bin/cp Executables/DARWIN_ARM64/xfoil /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/xfoil /bin/cp Executables/DARWIN_ARM64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/mastros.exe /bin/cp Executables/DARWIN_ARM64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/ASTRO.D01 /bin/cp Executables/DARWIN_ARM64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/ASTRO.IDX /bin/cp Executables/DARWIN_ARM64/mses /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/mses /bin/cp Executables/DARWIN_ARM64/mset /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/mset /bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include /bin/cp udunits/DARWIN_ARM64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib /bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libudunits2.dylib /bin/cp Libraries/DARWIN_ARM64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/aflr2AIM.so /bin/cp Libraries/DARWIN_ARM64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/aflr3AIM.so /bin/cp Libraries/DARWIN_ARM64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/aflr4AIM.so (cd CAPS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/caps.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/caps.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/capsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimUtil.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimUtil.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimMesh.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aimMesh.h clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../include \ aimMesh.c -o ./aimMesh.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \ ./aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 printObject.c -o ./printObject.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib (cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include testingAIM.c \ -o ./testingAIM.o rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include testingWriter.c \ -o ./testingWriter.o rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include phaseUtil.c \ -o ./phaseUtil.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libutils.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libutils.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/libutils.a mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \ -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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/7.7/DARWIN_ARM64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils astrosCards.c \ -o ./astrosCards.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils awaveAIM.c \ -o ./awaveAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include bodyTess.c -o ./bodyTess.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \ ./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include cart3dTest.c \ -o ./cart3dTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \ ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I. -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include aflr4egads.c \ -o ./aflr4egads.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils delaundoAIM.c \ -o ./delaundoAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils egadsTessAIM.c \ -o ./egadsTessAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils frictionAIM.c \ -o ./frictionAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \ -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \ -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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/7.7/DARWIN_ARM64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \ ./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 \ -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=7.7 \ -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/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. cloudFns.c \ -o ./cloudFns.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so \ ./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils masstranAIM.cpp \ -o ./masstranAIM.o clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include bstlWriter.c \ -o ./bstlWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include bvtkWriter.c \ -o ./bvtkWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include fastWriter.c \ -o ./fastWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include stlWriter.c \ -o ./stlWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include su2Writer.c \ -o ./su2Writer.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include tecplotWriter.c \ -o ./tecplotWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include ugridWriter.c \ -o ./ugridWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include vtkWriter.c \ -o ./vtkWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils mystranUtils.c \ -o ./mystranUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils nastranAIM.c \ -o ./nastranAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/platoAIM.so ./platoAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils hashElement.c \ -o ./hashElement.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 \ -I../meshWriter/libmeshbWriter/libMeshb/sources \ ../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/sierraSDAIM.so ./sierraSDAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/sierraSMAIM.so ./sierraSMAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils skeletonAIM.c \ -o ./skeletonAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 \ -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/7.7/DARWIN_ARM64/EngSketchPad/lib/spinnakerAIM.so ./spinnakerAIM.o ./libmeshb7.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils tacsAIM.c \ -o ./tacsAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \ ./tetgen_Interface.o ./tetgen.o \ ./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \ tsfoilAIM.c -o ./tsfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils \ xfoilAIM.c -o ./xfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/capsMode.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/capsMode.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flowchart.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flowchart.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/viewer.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/viewer.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.7/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=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/include -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 timPyscript.c -o ./timPyscript.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pyscript.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pyscript.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib *** Build Completed! *** + export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data + CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data + cd /Users/jenkins/workspace/ESP_Beta/7.7/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/7.7/DARWIN_ARM64/Verification.sh + bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/Verification.sh + expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/expressions.vfy", so verification is being skipped ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:169]] ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)" ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:176]] ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)" ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:183]] iend must not be less than ibeg when evaluating "slice(e3,4,-1)" ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:384]] index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:402]] index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:418]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:434]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:442]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:450]] column index must be between 1 and 3 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:458]] column index must be between 1 and 3 --> catching signal -262 (illegal_pmtr_index) ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:1914]] signal 1 thrown by user --> catching signal 1 (UNKNOWN) ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/expressions.csm:1924]] vertex and base must be different --> catching signal -225 (illegal_value) ==> serveESP completed successfully with no verification data real 0m0.293s user 0m0.060s sys 0m0.006s + set +x ============================================= ESP verification case 01 passed (as expected) ============================================= + expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/demo2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/demo2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.169s user 0m0.203s sys 0m0.021s + set +x ============================================= ESP verification case 02 passed (as expected) ============================================= + expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m1.341s user 0m1.996s sys 0m0.812s + set +x ============================================= ESP verification case 03 passed (as expected) ============================================= + expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.247s user 0m0.291s sys 0m0.034s + set +x ============================================= ESP verification case 04 passed (as expected) ============================================= + expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/design3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.271s user 0m0.397s sys 0m0.038s + set +x ============================================= ESP verification case 05 passed (as expected) ============================================= + expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.283s user 0m0.426s sys 0m0.021s + set +x ============================================= ESP verification case 06 passed (as expected) ============================================= + expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m1.966s user 0m3.369s sys 0m0.377s + set +x ============================================= ESP verification case 07 passed (as expected) ============================================= + expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/CAPS/verify_7.7.0/myPlane.vfy", so verification is being skipped ==> serveESP completed successfully with 12 warnings and no verification data real 0m15.008s user 0m26.258s sys 0m1.463s + set +x ============================================= ESP verification case 08 passed (as expected) ============================================= + expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/bottle + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/bottle WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.263s user 0m0.340s sys 0m0.012s + set +x ============================================= ESP verification case 09 passed (as expected) ============================================= + expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/wingMultiModel.vfy", so verification is being skipped ==> serveESP completed successfully with 4 warnings and no verification data real 0m19.939s user 0m48.380s sys 0m21.139s + set +x ============================================= ESP verification case 10 passed (as expected) ============================================= + expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/bullet + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/bullet WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/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 0m0.197s user 0m0.159s sys 0m0.017s + set +x ============================================= ESP verification case 11 passed (as expected) ============================================= + expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/connect5 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/connect5 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.370s user 0m0.552s sys 0m0.010s + set +x ============================================= ESP verification case 12 passed (as expected) ============================================= + expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/group2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/group2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.094s user 0m0.110s sys 0m0.005s + set +x ============================================= ESP verification case 13 passed (as expected) ============================================= + expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/csm3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/csm3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.7.0/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 0m0.277s user 0m0.300s sys 0m0.010s + set +x ============================================= ESP verification case 14 passed (as expected) ============================================= + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/testEGADS + make test python --version Python 3.11.6 python -u -m unittest discover .................................................... PCurve Map: 48 (alloc 48)! Surface Map: 12 (alloc 24)! Curve Map: 28 (alloc 28)! Writing PCurves... Writing Curves... Writing Surfaces... Writing 16 Nodes... Writing 28 Edges... Writing 12 Loops... Writing 12 Faces... Writing 1 Shells... EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close! ................... ---------------------------------------------------------------------- Ran 71 tests in 1.273s OK + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/testOCSM + source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/JenkinsESP/test_pyOCSM.sh ++ set -x ++ python -u test_pyOCSM.py -skipHelp real 0m3.339s user 0m5.238s sys 0m0.089s ++ set +x ================================================= test_pyOCSM.py passed (as expected) ================================================= + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/testCAPS + make test python --version Python 3.11.6 python -u -m unittest discover ..Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 143 Number of elements = 282 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 282 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 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 9.014s 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/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/ + make test python --version Python 3.11.6 python -u -m unittest discover --verbose test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.039 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 = 0.037 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23273 Number of elements = 46546 Number of tris = 44322 Number of quad = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.039 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4120 6016 AFLR2 GG : Nodes, Faces = 5820 9416 AFLR2 GG : Nodes, Faces = 7322 12420 AFLR2 GG : Nodes, Faces = 8613 15002 AFLR2 GG : Nodes, Faces = 9793 17362 AFLR2 GG : Nodes, Faces = 10847 19470 AFLR2 GG : Nodes, Faces = 11828 21432 AFLR2 GG : Nodes, Faces = 12749 23274 AFLR2 GG : Nodes, Faces = 13580 24936 AFLR2 GG : Nodes, Faces = 14355 26486 AFLR2 GG : Nodes, Faces = 15088 27952 AFLR2 GG : Nodes, Faces = 15774 29324 AFLR2 GG : Nodes, Faces = 16420 30616 AFLR2 GG : Nodes, Faces = 17013 31802 AFLR2 GG : Nodes, Faces = 17571 32918 AFLR2 GG : Nodes, Faces = 18089 33954 AFLR2 GG : Nodes, Faces = 18573 34922 AFLR2 GG : Nodes, Faces = 19005 35786 AFLR2 GG : Nodes, Faces = 19413 36602 AFLR2 GG : Nodes, Faces = 19779 37334 AFLR2 GG : Nodes, Faces = 20116 38008 AFLR2 GG : Nodes, Faces = 20443 38662 AFLR2 GG : Nodes, Faces = 20756 39288 AFLR2 GG : Nodes, Faces = 21054 39884 AFLR2 GG : Nodes, Faces = 21344 40464 AFLR2 GG : Nodes, Faces = 21621 41018 AFLR2 GG : Nodes, Faces = 21885 41546 AFLR2 GG : Nodes, Faces = 22137 42050 AFLR2 GG : Nodes, Faces = 22387 42550 AFLR2 GG : Nodes, Faces = 22603 42982 AFLR2 GG : Nodes, Faces = 22772 43320 AFLR2 GG : Nodes, Faces = 22912 43600 AFLR2 GG : Nodes, Faces = 23039 43854 AFLR2 GG : Nodes, Faces = 23142 44060 AFLR2 GG : Nodes, Faces = 23205 44186 AFLR2 GG : Nodes, Faces = 23240 44256 AFLR2 GG : Nodes, Faces = 23257 44290 AFLR2 GG : Nodes, Faces = 23269 44314 AFLR2 GG : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.037 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23273 Number of elements = 46546 Number of tris = 44322 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 ok test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.039 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 48 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 10 22 AFLR2 IG : Nodes, Faces = 20 42 AFLR2 IG : Nodes, Faces = 30 62 AFLR2 IG : Nodes, Faces = 40 82 AFLR2 IG : Nodes, Faces = 45 92 AFLR2 IG : Nodes, Faces = 46 94 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 98 AFLR2 IG : Nodes, Faces = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 48 48 AFLR2 GG : Nodes, Faces = 88 128 AFLR2 GG : Nodes, Faces = 109 170 AFLR2 GG : Nodes, Faces = 124 200 AFLR2 GG : Nodes, Faces = 136 224 AFLR2 GG : Nodes, Faces = 148 248 AFLR2 GG : Nodes, Faces = 160 272 AFLR2 GG : Nodes, Faces = 172 296 AFLR2 GG : Nodes, Faces = 182 316 AFLR2 GG : Nodes, Faces = 188 328 AFLR2 GG : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 190 Number of elements = 380 Number of tris = 332 Number of quad = 0 ok test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 344 344 AFLR2 GG : Nodes, Faces = 679 1014 AFLR2 GG : Nodes, Faces = 1006 1668 AFLR2 GG : Nodes, Faces = 1321 2298 AFLR2 GG : Nodes, Faces = 1604 2864 AFLR2 GG : Nodes, Faces = 1886 3428 AFLR2 GG : Nodes, Faces = 2155 3966 AFLR2 GG : Nodes, Faces = 2409 4474 AFLR2 GG : Nodes, Faces = 2649 4954 AFLR2 GG : Nodes, Faces = 2867 5390 AFLR2 GG : Nodes, Faces = 3063 5782 AFLR2 GG : Nodes, Faces = 3243 6142 AFLR2 GG : Nodes, Faces = 3400 6456 AFLR2 GG : Nodes, Faces = 3540 6736 AFLR2 GG : Nodes, Faces = 3665 6986 AFLR2 GG : Nodes, Faces = 3786 7228 AFLR2 GG : Nodes, Faces = 3900 7456 AFLR2 GG : Nodes, Faces = 4010 7676 AFLR2 GG : Nodes, Faces = 4114 7884 AFLR2 GG : Nodes, Faces = 4209 8074 AFLR2 GG : Nodes, Faces = 4292 8240 AFLR2 GG : Nodes, Faces = 4368 8392 AFLR2 GG : Nodes, Faces = 4439 8534 AFLR2 GG : Nodes, Faces = 4503 8662 AFLR2 GG : Nodes, Faces = 4560 8776 AFLR2 GG : Nodes, Faces = 4611 8878 AFLR2 GG : Nodes, Faces = 4650 8956 AFLR2 GG : Nodes, Faces = 4677 9010 AFLR2 GG : Nodes, Faces = 4695 9046 AFLR2 GG : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.004 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.001 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4705 Number of elements = 9410 Number of tris = 9066 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing FAST file .... Finished writing FAST file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing 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 = 0.006 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing 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:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 4371 Number of elements = 24249 Number of triangles = 3010 Number of quadrilatarals = 0 Number of tetrahedrals = 21239 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 10795 Number of elements = 60547 Number of triangles = 6366 Number of quadrilatarals = 0 Number of tetrahedrals = 54181 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 89164 Number of elements = 501194 Number of triangles = 51808 Number of quadrilatarals = 0 Number of tetrahedrals = 449386 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 8 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 9 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 10 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 11 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 12 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 13 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 14 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 15 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 16 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 17 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 18 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 19 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 60123 Number of elements = 350400 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 337972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required ok test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - trailingEdge Done getting mesh sizing parameters ok test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing 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 (17:53:08) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:09) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:09) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:11) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (17:53:12) Linearizing cut-cells (17:53:12) ... done o Number of simultaneous xsensit jobs: 1 (17:53:12) Computing gradients (17:53:20) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:20) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:21) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 3 Objective name - C_D Objective name - C_L Objective name - C_S Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:22) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:23) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:23) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:25) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (17:53:25) Linearizing cut-cells (17:53:25) ... done o Number of simultaneous xsensit jobs: 1 (17:53:25) Computing gradients (17:53:33) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:34) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:35) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_l Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:36) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:37) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:38) 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 (17:53:38) Linearizing cut-cells (17:53:38) ... done o Number of simultaneous xsensit jobs: 1 (17:53:38) Computing gradients (17:53:42) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:43) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:44) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_m Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:45) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:46) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:47) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (17:53:47) Linearizing cut-cells (17:53:47) ... done o Number of simultaneous xsensit jobs: 1 (17:53:47) Computing gradients (17:53:51) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:52) 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_n Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:54) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:53:54) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:53:55) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (17:53:55) Linearizing cut-cells (17:53:55) ... done o Number of simultaneous xsensit jobs: 1 (17:53:55) Computing gradients (17:53:59) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:00) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:01) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_x Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:03) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:03) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:04) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (17:54:04) Linearizing cut-cells (17:54:04) ... done o Number of simultaneous xsensit jobs: 1 (17:54:04) Computing gradients (17:54:08) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:09) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:10) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_y Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:11) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:12) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:13) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (17:54:13) Linearizing cut-cells (17:54:13) ... done o Number of simultaneous xsensit jobs: 1 (17:54:13) Computing gradients (17:54:17) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:17) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:18) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_z Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:19) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:20) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:21) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (17:54:21) Linearizing cut-cells (17:54:21) ... done o Number of simultaneous xsensit jobs: 1 (17:54:22) Computing gradients (17:54:26) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:26) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:27) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) ok test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Getting CFD design variables....... Number of design variables - 2 Design Variable name - Mach Design Variable name - area Done getting CFD design variables Getting CFD functional....... Number of design variables - 3 Objective name - C_A Objective name - C_N Objective name - C_Y Done getting CFD functional Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:28) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:29) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:32) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 2 o Number of simultaneous cutter jobs: 2 (17:54:32) Linearizing cut-cells (17:54:34) ... done o Number of simultaneous xsensit jobs: 2 (17:54:34) Computing gradients Adjusted OMP_NUM_THREADS to 1 for xsensit (17:54:42) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (17:54:43) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (17:54:44) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) ok test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Wing1, index = 1 Name = trailingEdge, index = 2 Writing FAST file .... Finished writing FAST file Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 284003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 284003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 284003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 284003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 284003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 284003000 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! 284003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 284003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ok test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = nodeBody, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing 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: 0.097002 Creating surface mesh ... Surface mesh seconds: 0.013551 Recovering boundaries... Boundary recovery seconds: 0.066719 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.020165 Recovering Delaunayness... Delaunay recovery seconds: 0.034676 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: 1.19391 Smoothing vertices... Mesh smoothing seconds: 0.983716 Improving mesh... Mesh improvement seconds: 0.026108 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.005393 Total running seconds: 2.44154 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: 0.098049 Creating surface mesh ... Surface mesh seconds: 0.013397 Recovering boundaries... Boundary recovery seconds: 0.078267 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.022139 Recovering Delaunayness... Delaunay recovery seconds: 0.037719 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: 1.24965 Smoothing vertices... Mesh smoothing seconds: 1.05881 Improving mesh... Mesh improvement seconds: 0.028674 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.006034 Total running seconds: 2.59306 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/7.7/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/7.7/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/7.7/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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 28 : MAX XYZ DEVIATION 8.51469 TOLERANCE 0.09 AT NODE 2 : INPUT EDGE COORDINATE T 7.85398 : INPUT X,Y,Z COORDINATES 0, 0, 0 : EVALUATED X,Y,Z COORDINATES 8.5, -3.7494e-32, 0.5 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON FACE 13 : MAX XYZ DEVIATION 0.707107 TOLERANCE 0.00707106 AT NODE 4 : INPUT FACE U,V COORDINATES 6.28319, 1.5708 : INPUT X,Y,Z COORDINATES 8.5, -0.5, 0 : EVALUATED X,Y,Z COORDINATES 8.5, -7.4988e-33, 0.5 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON FACE 14 : MAX XYZ DEVIATION 0.707107 TOLERANCE 0.00707106 AT NODE 4 : INPUT FACE U,V COORDINATES 0, 1.5708 : INPUT X,Y,Z COORDINATES 8.5, 0.5, 0 : EVALUATED X,Y,Z COORDINATES 8.5, 0, 0.5 EGADS : TRIAS FOUND WITH NON-MATCHING NORMALS !!! EGADS Error: Face 14 - FindPt+ 2/26 = -1 (EG_setTessFace)! *** EGADS ERROR -1 IN EG_setTessFace *** *** EGADS ERROR -1 *** ERROR 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 324 Number of elements = 1586 Number of triangles = 496 Number of quadrilatarals = 0 Number of tetrahedrals = 1090 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 963 Number of elements = 5141 Number of triangles = 874 Number of quadrilatarals = 0 Number of tetrahedrals = 4267 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2195 Number of elements = 9636 Number of triangles = 3992 Number of quadrilatarals = 0 Number of tetrahedrals = 5644 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 5644 Sideset: 'Farfield', set_id 1, num_entries 12 Sideset: 'Wing1', set_id 2, num_entries 3980 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 17056 Sideset: 'Farfield', set_id 1, num_entries 48 Sideset: 'Wing1', set_id 2, num_entries 3720 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 48717 Sideset: 'Farfield', set_id 1, num_entries 192 Sideset: 'Wing1', set_id 2, num_entries 4100 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- : XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 28 : MAX XYZ DEVIATION 8.51469 TOLERANCE 0.09 AT NODE 2 : INPUT EDGE COORDINATE T 7.85398 : INPUT X,Y,Z COORDINATES 0, 0, 0 : EVALUATED X,Y,Z COORDINATES 8.5, -3.7494e-32, 0.5 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON FACE 13 : MAX XYZ DEVIATION 0.707107 TOLERANCE 0.00707106 AT NODE 4 : INPUT FACE U,V COORDINATES 6.28319, 1.5708 : INPUT X,Y,Z COORDINATES 8.5, -0.5, 0 : EVALUATED X,Y,Z COORDINATES 8.5, -7.4988e-33, 0.5 : XYZ DEVIATION > TOLERANCE AT 1 NODES ON FACE 14 : MAX XYZ DEVIATION 0.707107 TOLERANCE 0.00707106 AT NODE 4 : INPUT FACE U,V COORDINATES 0, 1.5708 : INPUT X,Y,Z COORDINATES 8.5, 0.5, 0 : EVALUATED X,Y,Z COORDINATES 8.5, 0, 0.5 EGADS : TRIAS FOUND WITH NON-MATCHING NORMALS !!! EGADS Error: Face 14 - FindPt+ 2/26 = -1 (EG_setTessFace)! *** EGADS ERROR -1 IN EG_setTessFace *** *** EGADS ERROR -1 *** ERROR 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 76 Number of elements = 330 Number of triangles = 136 Number of quadrilatarals = 0 Number of tetrahedrals = 194 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 296 Number of elements = 1418 Number of triangles = 468 Number of quadrilatarals = 0 Number of tetrahedrals = 950 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 *** ERROR 200212 : duplicate boundary edges found *** ERROR test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... *** ERROR 200212 : duplicate boundary edges found *** FAIL test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... *** ERROR 200212 : duplicate boundary edges found *** FAIL 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 *** ERROR 200212 : duplicate boundary edges found *** ERROR 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 *** ERROR 200212 : duplicate boundary edges found *** ERROR test_reenter (test_su2.TestSU2.test_reenter) ... *** ERROR 200212 : duplicate boundary edges found *** ERROR test_units (test_su2.TestSU2.test_units) ... *** ERROR 200212 : duplicate boundary edges found *** ERROR test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards ok test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 284003000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 284003000 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 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 caps_filter Warning: No bodies with capsAIM = tetgenAIM! Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM caps_filter Warning: No bodies with capsAIM = egadsTessAIM! Body 1 capsAIM = aflr4AIM;aflr3AIM;platoAIM Body 2 capsAIM = aflr4AIM;aflr3AIM;platoAIM ERROR 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 ====================================================================== ERROR: test_all (test_refine.TestREFINE.test_all) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_refine.py", line 812, in test_all xyz = refine.output.xyz ^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1950, in __getattr__ return self._capsItems[name].value ^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 1880, in value return self._valObj.getValue() ^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 1969, in getValue if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: EGADS_NOTFOUND: ================================================================================ aflr3_Interface.c:1458 in aflr3_Volume_Mesh(): Error status = -1 aflr3AIM.c:803 in aimPreAnalysis(): Error status = -1 Problem during volume meshing transferValues for Mesh from Volume_Mesh = -1 ================================================================================ ====================================================================== ERROR: test_fun3d (test_refine.TestREFINE.test_fun3d) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_refine.py", line 880, in test_fun3d refine.runAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: EGADS_NOTFOUND: ================================================================================ aflr3_Interface.c:1458 in aflr3_Volume_Mesh(): Error status = -1 aflr3AIM.c:803 in aimPreAnalysis(): Error status = -1 Problem during volume meshing transferValues for Mesh from Volume_Mesh = -1 ================================================================================ ====================================================================== ERROR: test_inputs (test_su2.TestSU2.test_inputs) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 102, in test_inputs self.myAnalysis.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error): ================================================================================ aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212 aflr4_Interface.c:588 in aflr4_Surface_Mesh(): Error: AFLR4 mesh generation failed... An EGADS file with all AFLR4 parameters has been written to 'aflr4_debug.egads' aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212 Problem during AFLR4 surface meshing transferValues for Surface_Mesh from Surface_Mesh = 200212 transferValues for Mesh from Volume_Mesh = 200212 ================================================================================ ====================================================================== ERROR: test_journal (test_su2.TestSU2.test_journal) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 357, in test_journal line_total = self.run_journal(myProblem, -1) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 310, in run_journal su2.preAnalysis(); line += 1 ^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error): ================================================================================ aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212 aflr4_Interface.c:588 in aflr4_Surface_Mesh(): Error: AFLR4 mesh generation failed... An EGADS file with all AFLR4 parameters has been written to 'aflr4_debug.egads' aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212 Problem during AFLR4 surface meshing transferValues for Surface_Mesh from Surface_Mesh = 200212 transferValues for Mesh from Volume_Mesh = 200212 ================================================================================ ====================================================================== ERROR: test_phase (test_su2.TestSU2.test_phase) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 226, in test_phase su2.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error): ================================================================================ aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212 aflr4_Interface.c:588 in aflr4_Surface_Mesh(): Error: AFLR4 mesh generation failed... An EGADS file with all AFLR4 parameters has been written to 'aflr4_debug.egads' aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212 Problem during AFLR4 surface meshing transferValues for Surface_Mesh from Surface_Mesh = 200212 transferValues for Mesh from Volume_Mesh = 200212 ================================================================================ ====================================================================== ERROR: test_reenter (test_su2.TestSU2.test_reenter) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 152, in test_reenter self.myAnalysis.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error): ================================================================================ aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212 aflr4_Interface.c:588 in aflr4_Surface_Mesh(): Error: AFLR4 mesh generation failed... An EGADS file with all AFLR4 parameters has been written to 'aflr4_debug.egads' aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212 Problem during AFLR4 surface meshing transferValues for Surface_Mesh from Surface_Mesh = 200212 transferValues for Mesh from Volume_Mesh = 200212 ================================================================================ ====================================================================== ERROR: test_units (test_su2.TestSU2.test_units) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 194, in test_units myAnalysis.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2862, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS error code 200212 (undefined error): ================================================================================ aflr4_Interface.c:466 in aflr4_Surface_Mesh(): Error status = 200212 aflr4_Interface.c:588 in aflr4_Surface_Mesh(): Error: AFLR4 mesh generation failed... An EGADS file with all AFLR4 parameters has been written to 'aflr4_debug.egads' aflr4AIM.c:1212 in aimPreAnalysis(): Error status = 200212 Problem during AFLR4 surface meshing transferValues for Surface_Mesh from Surface_Mesh = 200212 transferValues for Mesh from Volume_Mesh = 200212 ================================================================================ ====================================================================== ERROR: test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_tetgen.py", line 167, in test_faceMatch_MultiDomain tetgen.runAnalysis() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/problem.py", line 2144, in runAnalysis self._analysisObj.execute() File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 2901, in execute if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/pyESP/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_SOURCEERR: ================================================================================ egadsTessAIM.c:420 in aimUpdateState(): Error: No Bodies! transferValues for Surface_Mesh from Surface_Mesh = -330 ================================================================================ ====================================================================== FAIL: test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 142, in test_invalidBoundary self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND") AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND' - UNKNOWN_ERROR + CAPS_NOTFOUND ====================================================================== FAIL: test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ---------------------------------------------------------------------- Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/test_su2.py", line 124, in test_invalidBoundaryName self.assertEqual(e.exception.errorName, "CAPS_NOTFOUND") AssertionError: 'UNKNOWN_ERROR' != 'CAPS_NOTFOUND' - UNKNOWN_ERROR + CAPS_NOTFOUND ---------------------------------------------------------------------- Ran 143 tests in 392.320s FAILED (failures=2, errors=8, skipped=10) CAPS Error: Cannot open /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/su2_problem/Scratch/capsRestart/Problem! CAPS Warning: caps_writeProblem = -333 (caps_close)! make: *** [test] Error 1 Build step 'Conditional step (single)' marked build as failure [GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE' [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Skipped based on build state FAILURE Finished: FAILURE