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Started by upstream project "ESP_Beta" build number 713 originally caused by: Started by remote host 18.18.33.14 Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on viggen in workspace /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64 [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64 Cleaning local Directory . Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-02T23:57:55.551 -0400' --quiet Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 2483 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP doesn't exist Cleaning local Directory JenkinsESP Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-02T23:57:55.551 -0400' --quiet Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 860 No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [viggen] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [viggen] is in [[viggen]] Run condition [Execution node ] enabling perform for step [Execute shell] [DARWIN_ARM64] $ /bin/bash -ex /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins16596977926862066438.sh + arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/ESP_Beta.sh + source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/ESP_Env.sh ++ export OCCTREF=7.8 ++ OCCTREF=7.8 ++ AFLR_VERSION=11.5.14 ++ SU2_VERSION=8.0.0 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.38.0 ++ export PYTHON_VERSION=3.11.9 ++ PYTHON_VERSION=3.11.9 ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ [[ viggen == \r\e\y\n\o\l\d\s ]] ++ [[ DARWIN_ARM64 == *\.\i\f\o\r\t ]] ++ '[' -f /opt/intel/oneapi/setvars.sh ']' ++ source /opt/intel/oneapi/setvars.sh ++ '[' -f /Users/jenkins/.bashrc ']' ++ export CAPS_OUTLEVEL=0 ++ CAPS_OUTLEVEL=0 ++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.8 != '' ]] ++ [[ '' != '' ]] ++ [[ viggen == *\r\e\y\n\o\l\d\s* ]] ++ [[ viggen == *\m\a\c\y\s* ]] ++ [[ viggen == *\v\i\g\g\e\n* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile ++++ /opt/homebrew/bin/brew shellenv +++ eval 'export HOMEBREW_PREFIX="/opt/homebrew"; export HOMEBREW_CELLAR="/opt/homebrew/Cellar"; export HOMEBREW_REPOSITORY="/opt/homebrew"; export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}"; export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:"; export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";' ++++ export HOMEBREW_PREFIX=/opt/homebrew ++++ HOMEBREW_PREFIX=/opt/homebrew ++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ export HOMEBREW_REPOSITORY=/opt/homebrew ++++ HOMEBREW_REPOSITORY=/opt/homebrew ++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ export MANPATH=/opt/homebrew/share/man: ++++ MANPATH=/opt/homebrew/share/man: ++++ export INFOPATH=/opt/homebrew/share/info: ++++ INFOPATH=/opt/homebrew/share/info: +++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]] +++ . /opt/homebrew/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export NETCDF_PATH=/opt/homebrew +++ NETCDF_PATH=/opt/homebrew ++ [[ viggen == *\m\a\c\y\s* ]] ++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/udunits/udunits2.xml ++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ [[ viggen == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-arm64 ++ AFLR_ARCH=MacOSX-arm64 ++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ export CART3D_ARCH=OSX64_ICC ++ CART3D_ARCH=OSX64_ICC ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export SEACAS=/Users/jenkins/util/sandialabs/seacas ++ SEACAS=/Users/jenkins/util/sandialabs/seacas ++ [[ viggen == \v\i\g\g\e\n ]] ++ export NETCDFINC=/opt/homebrew/include ++ NETCDFINC=/opt/homebrew/include ++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' +++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl ++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH; PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB; PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT; PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT; PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;' +++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 +++ export PERL5LIB +++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_LOCAL_LIB_ROOT +++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"' +++ export PERL_MB_OPT +++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_MM_OPT ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ [[ viggen == \m\a\c\y\s* ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-*' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv +++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-cc +++ python-config --includes ++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' ++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]] +++ python-config --ldflags --embed ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.9 ++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/data + virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv created virtual environment CPython3.11.9.final.0-64 in 330ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv, clear=False, no_vcs_ignore=False, global=False) seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv) added seed packages: pip==24.0, setuptools==69.2.0, wheel==0.43.0 activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator + . /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/activate ++ '[' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/ESP_Beta.sh ']' ++ deactivate nondestructive ++ unset -f pydoc ++ '[' -z '' ']' ++ '[' -z '' ']' ++ hash -r ++ '[' -z '' ']' ++ unset VIRTUAL_ENV ++ unset VIRTUAL_ENV_PROMPT ++ '[' '!' nondestructive = nondestructive ']' ++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv ++ '[' darwin23 = cygwin ']' ++ '[' darwin23 = msys ']' ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH ++ '[' x '!=' x ']' +++ basename /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv ++ VIRTUAL_ENV_PROMPT=ESP_venv ++ export VIRTUAL_ENV_PROMPT ++ '[' -z '' ']' ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ PS1='(ESP_venv) ' ++ export PS1 ++ alias pydoc ++ true ++ hash -r + pip_install pip + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0) + pip_install f90nml + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml Collecting f90nml Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB) Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB) Installing collected packages: f90nml Successfully installed f90nml-1.4.4 + pip_install numpy + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy Collecting numpy Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (114 kB) Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl (14.0 MB) Installing collected packages: numpy Successfully installed numpy-1.26.4 + pip_install openmdao + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao Collecting openmdao Using cached openmdao-3.31.1-py3-none-any.whl Collecting networkx>=2.0 (from openmdao) Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB) Requirement already satisfied: numpy in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4) Collecting scipy (from openmdao) Using cached scipy-1.13.0-cp311-cp311-macosx_12_0_arm64.whl.metadata (60 kB) Collecting requests (from openmdao) Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB) Collecting packaging (from openmdao) Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB) Collecting charset-normalizer<4,>=2 (from requests->openmdao) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (33 kB) Collecting idna<4,>=2.5 (from requests->openmdao) Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB) Collecting urllib3<3,>=1.21.1 (from requests->openmdao) Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB) Collecting certifi>=2017.4.17 (from requests->openmdao) Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB) Using cached networkx-3.3-py3-none-any.whl (1.7 MB) Using cached packaging-24.0-py3-none-any.whl (53 kB) Using cached requests-2.31.0-py3-none-any.whl (62 kB) Using cached scipy-1.13.0-cp311-cp311-macosx_12_0_arm64.whl (30.3 MB) Using cached certifi-2024.2.2-py3-none-any.whl (163 kB) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_11_0_arm64.whl (118 kB) Using cached idna-3.7-py3-none-any.whl (66 kB) Using cached urllib3-2.2.1-py3-none-any.whl (121 kB) Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.31.1 packaging-24.0 requests-2.31.0 scipy-1.13.0 urllib3-2.2.1 + [[ viggen == *\v\i\g\g\e\n* ]] + export CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib + CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib + export CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0 + CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0 + GCC_MAJOR=11 + export 'CVXOPT_BLAS_EXTRA_LINK_ARGS=/opt/homebrew/opt/gcc/lib/gcc/11/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/11/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/11/gcc/aarch64-apple-darwin21/11/libgcc.a' + CVXOPT_BLAS_EXTRA_LINK_ARGS='/opt/homebrew/opt/gcc/lib/gcc/11/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/11/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/11/gcc/aarch64-apple-darwin21/11/libgcc.a' + pip_install cvxopt + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (1.3 kB) Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl (11.1 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 + pip_install dill + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill Collecting dill Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB) Using cached dill-0.3.8-py3-none-any.whl (116 kB) Installing collected packages: dill Successfully installed dill-0.3.8 + pip_install packaging + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0) + pip_install matplotlib + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.8.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (5.8 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl.metadata (5.8 kB) Collecting cycler>=0.10 (from matplotlib) Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB) Collecting fonttools>=4.22.0 (from matplotlib) Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_universal2.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl.metadata (6.4 kB) Requirement already satisfied: numpy>=1.21 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4) Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.0) Collecting pillow>=8 (from matplotlib) Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (9.2 kB) Collecting pyparsing>=2.3.1 (from matplotlib) Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB) Collecting python-dateutil>=2.7 (from matplotlib) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB) Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib) Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB) Using cached matplotlib-3.8.4-cp311-cp311-macosx_11_0_arm64.whl (7.5 MB) Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl (245 kB) Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB) Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_universal2.whl (2.8 MB) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl (66 kB) Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl (3.4 MB) 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/7.8/DARWIN_ARM64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.0) Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4) + unset PYTHONINC + unset PYTHONLIB + unset UDUNITS2_XML_PATH + unset ESP_BLOC + unset ESP_ROOT + unset ESP_ARCH + unset AWAVE + unset AFLR + unset AFLR_ARCH + wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz --2024-05-03 00:16:00-- https://acdl.mit.edu/ESP/archive/ESPbeta.tgz Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14 Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected. 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.......... .......... 5% 94.4M 4s 13650K .......... .......... .......... .......... .......... 5% 95.9M 4s 13700K .......... .......... .......... .......... .......... 5% 77.3M 4s 13750K .......... .......... .......... .......... .......... 5% 120M 4s 13800K .......... .......... .......... .......... .......... 5% 78.1M 4s 13850K .......... .......... .......... .......... .......... 5% 110M 4s 13900K .......... .......... .......... .......... .......... 5% 105M 4s 13950K .......... .......... .......... .......... .......... 5% 73.5M 4s 14000K .......... .......... .......... .......... .......... 5% 97.1M 4s 14050K .......... .......... .......... .......... .......... 5% 95.7M 4s 14100K .......... .......... .......... .......... .......... 5% 94.1M 4s 14150K .......... .......... .......... .......... .......... 5% 74.9M 4s 14200K .......... .......... .......... .......... .......... 5% 94.1M 4s 14250K .......... .......... .......... .......... .......... 5% 94.4M 4s 14300K .......... .......... .......... .......... .......... 5% 125M 4s 14350K .......... .......... .......... .......... .......... 5% 75.7M 4s 14400K .......... .......... .......... .......... .......... 5% 119M 4s 14450K .......... .......... .......... .......... .......... 5% 64.5M 4s 14500K .......... .......... .......... .......... .......... 5% 117M 4s 14550K .......... .......... .......... .......... .......... 5% 94.4M 4s 14600K .......... .......... .......... .......... .......... 5% 91.6M 4s 14650K .......... .......... .......... .......... .......... 5% 101M 4s 14700K .......... .......... .......... .......... .......... 5% 89.3M 4s 14750K .......... .......... .......... .......... .......... 5% 94.3M 4s 14800K .......... .......... .......... .......... .......... 5% 94.1M 4s 14850K .......... .......... .......... .......... .......... 5% 95.6M 4s 14900K .......... .......... .......... .......... .......... 5% 77.9M 4s 14950K .......... .......... .......... .......... .......... 5% 89.6M 4s 15000K .......... .......... .......... .......... .......... 5% 97.7M 4s 15050K .......... .......... .......... .......... .......... 5% 95.6M 4s 15100K .......... .......... .......... .......... .......... 5% 89.9M 4s 15150K .......... .......... .......... .......... .......... 5% 78.3M 4s 15200K .......... .......... .......... .......... .......... 5% 93.2M 4s 15250K .......... .......... .......... .......... .......... 5% 94.6M 4s 15300K .......... .......... .......... .......... .......... 5% 94.3M 4s 15350K .......... .......... .......... .......... .......... 5% 94.3M 4s 15400K .......... .......... .......... .......... .......... 5% 88.9M 4s 15450K .......... .......... .......... .......... .......... 5% 79.4M 4s 15500K .......... .......... .......... .......... .......... 5% 125M 4s 15550K .......... .......... .......... .......... .......... 5% 115M 4s 15600K .......... .......... .......... .......... .......... 5% 98.8M 4s 15650K .......... .......... .......... .......... .......... 5% 99.6M 4s 15700K .......... .......... .......... .......... .......... 6% 92.8M 4s 15750K .......... .......... .......... .......... .......... 6% 26.6M 4s 15800K .......... .......... .......... .......... .......... 6% 326M 4s 15850K .......... .......... .......... .......... .......... 6% 286M 4s 15900K .......... .......... .......... .......... .......... 6% 29.0M 4s 15950K .......... .......... .......... .......... .......... 6% 301M 4s 16000K .......... .......... .......... .......... .......... 6% 362M 4s 16050K .......... .......... .......... .......... .......... 6% 379M 4s 16100K .......... .......... .......... .......... .......... 6% 268M 3s 16150K .......... .......... .......... .......... .......... 6% 309M 3s 16200K .......... .......... .......... .......... .......... 6% 107M 3s 16250K .......... .......... .......... .......... .......... 6% 90.4M 3s 16300K .......... .......... .......... .......... .......... 6% 99.9M 3s 16350K .......... .......... .......... .......... .......... 6% 43.2M 3s 16400K .......... .......... .......... .......... .......... 6% 70.8M 3s 16450K .......... .......... .......... .......... .......... 6% 94.6M 3s 16500K .......... .......... .......... .......... .......... 6% 93.0M 3s 16550K .......... .......... .......... .......... .......... 6% 91.8M 3s 16600K .......... .......... .......... .......... .......... 6% 45.6M 3s 16650K .......... .......... .......... .......... .......... 6% 121M 3s 16700K .......... .......... .......... .......... .......... 6% 48.0M 3s 16750K .......... .......... .......... .......... .......... 6% 87.3M 3s 16800K .......... .......... .......... .......... .......... 6% 65.5M 3s 16850K .......... .......... .......... .......... .......... 6% 64.8M 3s 16900K .......... .......... .......... .......... .......... 6% 124M 3s 16950K .......... .......... .......... .......... .......... 6% 65.5M 3s 17000K .......... .......... .......... .......... .......... 6% 115M 3s 17050K .......... .......... .......... .......... .......... 6% 88.8M 3s 17100K .......... .......... .......... .......... .......... 6% 92.7M 3s 17150K .......... .......... .......... .......... .......... 6% 98.6M 3s 17200K .......... .......... .......... .......... .......... 6% 64.2M 3s 17250K .......... .......... .......... .......... .......... 6% 104M 3s 17300K .......... .......... .......... .......... .......... 6% 69.7M 3s 17350K .......... .......... .......... .......... .......... 6% 94.3M 3s 17400K .......... .......... .......... .......... .......... 6% 93.4M 3s 17450K .......... .......... .......... .......... .......... 6% 63.5M 3s 17500K .......... .......... .......... .......... .......... 6% 118M 3s 17550K .......... .......... .......... .......... .......... 6% 95.2M 3s 17600K .......... .......... .......... .......... .......... 6% 65.1M 3s 17650K .......... .......... .......... .......... .......... 6% 170M 3s 17700K .......... .......... .......... .......... .......... 6% 63.3M 3s 17750K .......... .......... .......... .......... .......... 6% 99.0M 3s 17800K .......... .......... .......... .......... .......... 6% 74.1M 3s 17850K .......... .......... .......... .......... .......... 6% 89.6M 3s 17900K .......... .......... .......... .......... .......... 6% 72.9M 3s 17950K .......... .......... .......... .......... .......... 6% 80.6M 3s 18000K .......... .......... .......... .......... .......... 6% 94.4M 3s 18050K .......... .......... .......... .......... .......... 6% 75.9M 3s 18100K .......... .......... .......... .......... .......... 6% 86.4M 3s 18150K .......... .......... .......... .......... .......... 6% 103M 3s 18200K .......... .......... .......... .......... .......... 6% 90.9M 3s 18250K .......... .......... .......... .......... .......... 6% 64.8M 3s 18300K .......... .......... .......... .......... .......... 6% 174M 3s 18350K .......... .......... .......... .......... .......... 7% 55.6M 3s 18400K .......... .......... .......... .......... .......... 7% 179M 3s 18450K .......... .......... .......... .......... .......... 7% 65.3M 3s 18500K .......... .......... .......... .......... .......... 7% 94.3M 3s 18550K .......... .......... .......... .......... .......... 7% 93.9M 3s 18600K .......... .......... .......... .......... .......... 7% 90.3M 3s 18650K .......... .......... .......... .......... .......... 7% 75.6M 3s 18700K .......... .......... .......... .......... .......... 7% 95.2M 3s 18750K .......... .......... .......... .......... .......... 7% 63.5M 3s 18800K .......... .......... .......... .......... .......... 7% 107M 3s 18850K .......... .......... .......... .......... .......... 7% 81.7M 3s 18900K .......... .......... .......... .......... .......... 7% 65.3M 3s 18950K .......... .......... .......... .......... .......... 7% 94.6M 3s 19000K .......... .......... .......... .......... .......... 7% 118M 3s 19050K .......... .......... .......... .......... .......... 7% 97.9M 3s 19100K .......... .......... .......... .......... .......... 7% 95.9M 3s 19150K .......... .......... .......... .......... .......... 7% 120M 3s 19200K .......... .......... .......... .......... .......... 7% 90.8M 3s 19250K .......... .......... .......... .......... .......... 7% 102M 3s 19300K .......... .......... .......... .......... .......... 7% 121M 3s 19350K .......... .......... .......... .......... .......... 7% 25.1M 3s 19400K .......... .......... .......... .......... .......... 7% 102M 3s 19450K .......... .......... .......... .......... .......... 7% 112M 3s 19500K .......... .......... .......... .......... .......... 7% 128M 3s 19550K .......... .......... .......... .......... .......... 7% 127M 3s 19600K .......... .......... .......... .......... .......... 7% 109M 3s 19650K .......... .......... .......... .......... .......... 7% 132M 3s 19700K .......... .......... .......... .......... .......... 7% 109M 3s 19750K .......... .......... .......... .......... .......... 7% 128M 3s 19800K .......... .......... .......... .......... .......... 7% 142M 3s 19850K .......... .......... .......... .......... .......... 7% 330M 3s 19900K .......... .......... .......... .......... .......... 7% 339M 3s 19950K .......... .......... .......... .......... .......... 7% 71.5M 3s 20000K .......... .......... .......... .......... .......... 7% 76.7M 3s 20050K .......... .......... .......... .......... .......... 7% 75.5M 3s 20100K .......... .......... .......... .......... .......... 7% 63.3M 3s 20150K .......... .......... .......... .......... .......... 7% 73.4M 3s 20200K .......... .......... .......... .......... .......... 7% 55.7M 3s 20250K .......... .......... .......... .......... .......... 7% 73.2M 3s 20300K .......... .......... .......... .......... .......... 7% 55.5M 3s 20350K .......... .......... .......... .......... .......... 7% 62.5M 3s 20400K .......... .......... .......... .......... .......... 7% 94.8M 3s 20450K .......... .......... .......... .......... .......... 7% 75.6M 3s 20500K .......... .......... .......... .......... .......... 7% 62.9M 3s 20550K .......... .......... .......... .......... .......... 7% 87.8M 3s 20600K .......... .......... .......... .......... .......... 7% 48.6M 3s 20650K .......... .......... .......... .......... .......... 7% 91.1M 3s 20700K .......... .......... .......... .......... .......... 7% 65.5M 3s 20750K .......... .......... .......... .......... .......... 7% 62.0M 3s 20800K .......... .......... .......... .......... .......... 7% 53.4M 3s 20850K .......... .......... .......... .......... .......... 7% 64.6M 3s 20900K .......... .......... .......... .......... .......... 7% 127M 3s 20950K .......... .......... .......... .......... .......... 8% 54.7M 3s 21000K .......... .......... .......... .......... .......... 8% 71.9M 3s 21050K .......... .......... .......... .......... .......... 8% 55.7M 3s 21100K .......... .......... .......... .......... .......... 8% 73.6M 3s 21150K .......... .......... .......... .......... .......... 8% 99.0M 3s 21200K .......... .......... .......... .......... .......... 8% 63.5M 3s 21250K .......... .......... .......... .......... .......... 8% 76.3M 3s 21300K .......... .......... .......... .......... .......... 8% 90.3M 3s 21350K .......... .......... .......... .......... .......... 8% 50.9M 3s 21400K .......... .......... .......... .......... .......... 8% 51.1M 3s 21450K .......... .......... .......... .......... .......... 8% 62.4M 3s 21500K .......... .......... .......... .......... .......... 8% 52.4M 3s 21550K .......... .......... .......... .......... .......... 8% 62.3M 3s 21600K .......... .......... .......... .......... .......... 8% 112M 3s 21650K .......... .......... .......... .......... .......... 8% 51.0M 3s 21700K .......... .......... .......... .......... .......... 8% 63.1M 3s 21750K .......... .......... .......... .......... .......... 8% 119M 3s 21800K .......... .......... .......... .......... .......... 8% 53.8M 3s 21850K .......... .......... .......... .......... .......... 8% 90.8M 3s 21900K .......... .......... .......... .......... .......... 8% 57.8M 3s 21950K .......... .......... .......... .......... .......... 8% 62.1M 3s 22000K .......... .......... .......... .......... .......... 8% 77.8M 3s 22050K .......... .......... .......... .......... .......... 8% 76.3M 3s 22100K .......... .......... .......... .......... .......... 8% 63.2M 3s 22150K .......... .......... .......... .......... .......... 8% 76.2M 3s 22200K .......... .......... .......... .......... .......... 8% 54.0M 3s 22250K .......... .......... .......... .......... .......... 8% 95.4M 3s 22300K .......... .......... .......... .......... .......... 8% 75.7M 3s 22350K .......... .......... .......... .......... .......... 8% 91.8M 3s 22400K .......... .......... .......... .......... .......... 8% 97.9M 3s 22450K .......... .......... .......... .......... .......... 8% 95.7M 3s 22500K .......... .......... .......... .......... .......... 8% 120M 3s 22550K .......... .......... .......... .......... .......... 8% 17.0M 3s 22600K .......... .......... .......... .......... .......... 8% 27.7M 3s 22650K .......... .......... .......... .......... .......... 8% 379M 3s 22700K .......... .......... .......... .......... .......... 8% 337M 3s 22750K .......... .......... .......... .......... .......... 8% 111M 3s 22800K .......... .......... .......... .......... .......... 8% 404M 3s 22850K .......... .......... .......... .......... .......... 8% 356M 3s 22900K .......... .......... .......... .......... .......... 8% 421M 3s 22950K .......... .......... .......... .......... .......... 8% 376M 3s 23000K .......... .......... .......... .......... .......... 8% 391M 3s 23050K .......... .......... .......... .......... .......... 8% 421M 3s 23100K .......... .......... .......... .......... .......... 8% 30.4M 3s 23150K .......... .......... .......... .......... .......... 8% 131M 3s 23200K .......... .......... .......... .......... .......... 8% 54.9M 3s 23250K .......... .......... .......... .......... .......... 8% 354M 3s 23300K .......... .......... .......... .......... .......... 8% 417M 3s 23350K .......... .......... .......... .......... .......... 8% 75.5M 3s 23400K .......... .......... .......... .......... .......... 8% 135M 3s 23450K .......... .......... .......... .......... .......... 8% 123M 3s 23500K .......... .......... .......... .......... .......... 8% 138M 3s 23550K .......... .......... .......... .......... .......... 9% 143M 3s 23600K .......... .......... .......... .......... .......... 9% 119M 3s 23650K .......... .......... .......... .......... .......... 9% 146M 3s 23700K .......... .......... .......... .......... .......... 9% 115M 3s 23750K .......... 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.......... 9% 19.6M 3s 24450K .......... .......... .......... .......... .......... 9% 344M 3s 24500K .......... .......... .......... .......... .......... 9% 38.2M 3s 24550K .......... .......... .......... .......... .......... 9% 67.0M 3s 24600K .......... .......... .......... .......... .......... 9% 35.8M 3s 24650K .......... .......... .......... .......... .......... 9% 79.4M 3s 24700K .......... .......... .......... .......... .......... 9% 58.5M 3s 24750K .......... .......... .......... .......... .......... 9% 77.5M 3s 24800K .......... .......... .......... .......... .......... 9% 130M 3s 24850K .......... .......... .......... .......... .......... 9% 24.8M 3s 24900K .......... .......... .......... .......... .......... 9% 26.9M 3s 24950K .......... .......... .......... .......... .......... 9% 270M 3s 25000K .......... .......... .......... .......... .......... 9% 38.7M 3s 25050K .......... .......... .......... .......... .......... 9% 138M 3s 25100K .......... .......... .......... .......... .......... 9% 12.4M 3s 25150K .......... .......... .......... .......... .......... 9% 145M 3s 25200K .......... .......... .......... .......... .......... 9% 35.9M 3s 25250K .......... .......... .......... .......... .......... 9% 121M 3s 25300K .......... .......... .......... .......... .......... 9% 73.3M 3s 25350K .......... .......... .......... .......... .......... 9% 88.6M 3s 25400K .......... .......... .......... .......... .......... 9% 136M 3s 25450K .......... .......... .......... .......... .......... 9% 18.7M 3s 25500K .......... .......... .......... .......... .......... 9% 294M 3s 25550K .......... .......... .......... .......... .......... 9% 379M 3s 25600K .......... .......... .......... .......... .......... 9% 52.6M 3s 25650K .......... .......... .......... .......... .......... 9% 76.9M 3s 25700K .......... .......... .......... .......... .......... 9% 37.2M 3s 25750K .......... .......... .......... .......... .......... 9% 417M 3s 25800K .......... .......... .......... .......... .......... 9% 22.0M 3s 25850K .......... .......... .......... .......... .......... 9% 227M 3s 25900K .......... .......... .......... .......... .......... 9% 307M 3s 25950K .......... .......... .......... .......... .......... 9% 30.3M 3s 26000K .......... .......... .......... .......... .......... 9% 400M 3s 26050K .......... .......... .......... .......... .......... 9% 16.8M 3s 26100K .......... .......... .......... .......... .......... 9% 323M 3s 26150K .......... .......... .......... .......... .......... 9% 425M 3s 26200K .......... .......... .......... .......... .......... 10% 38.6M 3s 26250K .......... .......... .......... .......... .......... 10% 147M 3s 26300K .......... .......... .......... .......... .......... 10% 94.4M 3s 26350K .......... .......... .......... .......... .......... 10% 77.1M 3s 26400K .......... .......... .......... .......... .......... 10% 81.0M 3s 26450K .......... .......... .......... .......... .......... 10% 132M 3s 26500K .......... .......... .......... .......... .......... 10% 44.7M 3s 26550K .......... .......... .......... .......... .......... 10% 96.9M 3s 26600K .......... .......... .......... .......... .......... 10% 92.1M 3s 26650K .......... .......... .......... .......... .......... 10% 59.8M 3s 26700K .......... .......... .......... .......... .......... 10% 85.2M 3s 26750K .......... .......... .......... .......... .......... 10% 141M 3s 26800K .......... .......... .......... .......... .......... 10% 111M 3s 26850K .......... .......... .......... .......... .......... 10% 60.4M 3s 26900K .......... .......... .......... .......... .......... 10% 150M 3s 26950K .......... .......... .......... .......... .......... 10% 38.6M 3s 27000K .......... .......... .......... .......... .......... 10% 359M 3s 27050K .......... .......... .......... .......... .......... 10% 186M 3s 27100K .......... .......... .......... .......... .......... 10% 12.5M 3s 27150K .......... .......... .......... .......... .......... 10% 397M 3s 27200K .......... .......... .......... .......... .......... 10% 32.9M 3s 27250K .......... .......... .......... .......... .......... 10% 112M 3s 27300K .......... .......... .......... .......... .......... 10% 151M 3s 27350K .......... .......... .......... .......... .......... 10% 42.5M 3s 27400K .......... .......... .......... .......... .......... 10% 80.3M 3s 27450K .......... .......... .......... .......... .......... 10% 132M 3s 27500K .......... .......... .......... .......... .......... 10% 48.1M 3s 27550K .......... .......... .......... .......... .......... 10% 128M 3s 27600K .......... .......... .......... .......... .......... 10% 123M 3s 27650K .......... .......... .......... .......... .......... 10% 64.2M 3s 27700K .......... .......... .......... .......... .......... 10% 97.7M 3s 27750K .......... .......... .......... .......... .......... 10% 54.8M 3s 27800K .......... .......... .......... .......... .......... 10% 163M 3s 27850K .......... .......... .......... .......... .......... 10% 102M 3s 27900K .......... .......... .......... .......... .......... 10% 86.1M 3s 27950K .......... .......... .......... .......... .......... 10% 82.9M 3s 28000K .......... .......... .......... .......... .......... 10% 155M 3s 28050K .......... .......... .......... .......... .......... 10% 100M 3s 28100K .......... .......... .......... .......... .......... 10% 151M 3s 28150K .......... .......... .......... .......... .......... 10% 55.4M 3s 28200K .......... .......... .......... .......... .......... 10% 130M 3s 28250K .......... .......... .......... .......... .......... 10% 86.6M 3s 28300K .......... .......... .......... .......... .......... 10% 58.0M 3s 28350K .......... .......... .......... .......... .......... 10% 373M 3s 28400K .......... .......... .......... .......... .......... 10% 91.6M 3s 28450K .......... .......... .......... .......... .......... 10% 52.8M 3s 28500K .......... .......... .......... .......... .......... 10% 59.1M 3s 28550K .......... .......... .......... .......... .......... 10% 139M 3s 28600K .......... .......... .......... .......... .......... 10% 46.6M 3s 28650K .......... .......... .......... .......... .......... 10% 151M 3s 28700K .......... .......... .......... .......... .......... 10% 42.7M 3s 28750K .......... .......... .......... .......... .......... 10% 115M 3s 28800K .......... .......... .......... .......... .......... 11% 151M 3s 28850K .......... .......... .......... .......... .......... 11% 39.4M 3s 28900K .......... .......... .......... .......... .......... 11% 142M 3s 28950K .......... .......... .......... .......... .......... 11% 126M 3s 29000K .......... .......... .......... .......... .......... 11% 100M 3s 29050K .......... .......... .......... .......... .......... 11% 87.2M 3s 29100K .......... .......... .......... .......... .......... 11% 102M 3s 29150K .......... .......... .......... .......... .......... 11% 68.8M 3s 29200K .......... .......... .......... .......... .......... 11% 72.8M 3s 29250K .......... .......... .......... .......... .......... 11% 146M 3s 29300K .......... .......... .......... .......... .......... 11% 106M 3s 29350K .......... .......... .......... .......... .......... 11% 81.5M 3s 29400K .......... .......... .......... .......... .......... 11% 99.0M 3s 29450K .......... .......... .......... .......... .......... 11% 97.7M 3s 29500K .......... .......... .......... .......... .......... 11% 103M 3s 29550K .......... .......... .......... .......... .......... 11% 137M 3s 29600K .......... .......... .......... .......... .......... 11% 12.6M 3s 29650K .......... .......... .......... .......... .......... 11% 145M 3s 29700K .......... .......... .......... .......... .......... 11% 125M 3s 29750K .......... .......... .......... .......... .......... 11% 12.4M 3s 29800K .......... .......... .......... .......... .......... 11% 110M 3s 29850K .......... .......... .......... .......... .......... 11% 40.5M 3s 29900K .......... .......... .......... .......... .......... 11% 114M 3s 29950K .......... .......... .......... .......... .......... 11% 96.3M 3s 30000K .......... .......... .......... .......... .......... 11% 102M 3s 30050K .......... .......... .......... .......... .......... 11% 122M 3s 30100K .......... .......... .......... .......... .......... 11% 67.0M 3s 30150K .......... .......... .......... .......... .......... 11% 148M 3s 30200K .......... .......... .......... .......... .......... 11% 35.1M 3s 30250K .......... .......... .......... .......... .......... 11% 425M 3s 30300K .......... .......... .......... .......... .......... 11% 452M 3s 30350K .......... .......... .......... .......... .......... 11% 34.4M 3s 30400K .......... .......... .......... .......... .......... 11% 147M 3s 30450K .......... .......... .......... .......... .......... 11% 16.3M 3s 30500K .......... .......... .......... .......... .......... 11% 388M 3s 30550K .......... .......... .......... .......... .......... 11% 417M 3s 30600K .......... .......... .......... .......... .......... 11% 29.3M 3s 30650K .......... .......... .......... .......... .......... 11% 376M 3s 30700K .......... .......... .......... .......... .......... 11% 15.1M 3s 30750K .......... .......... .......... .......... .......... 11% 379M 3s 30800K .......... .......... .......... .......... .......... 11% 164M 3s 30850K .......... .......... .......... .......... .......... 11% 36.7M 3s 30900K .......... .......... .......... .......... .......... 11% 121M 3s 30950K .......... .......... .......... .......... .......... 11% 94.6M 3s 31000K .......... .......... .......... .......... .......... 11% 82.1M 3s 31050K .......... .......... .......... .......... .......... 11% 97.1M 3s 31100K .......... .......... .......... .......... .......... 11% 90.1M 3s 31150K .......... 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.......... 12% 85.7M 3s 31850K .......... .......... .......... .......... .......... 12% 67.3M 3s 31900K .......... .......... .......... .......... .......... 12% 93.7M 3s 31950K .......... .......... .......... .......... .......... 12% 75.8M 3s 32000K .......... .......... .......... .......... .......... 12% 123M 3s 32050K .......... .......... .......... .......... .......... 12% 76.2M 3s 32100K .......... .......... .......... .......... .......... 12% 70.2M 3s 32150K .......... .......... .......... .......... .......... 12% 105M 3s 32200K .......... .......... .......... .......... .......... 12% 72.2M 3s 32250K .......... .......... .......... .......... .......... 12% 78.6M 3s 32300K .......... .......... .......... .......... .......... 12% 128M 3s 32350K .......... .......... .......... .......... .......... 12% 62.9M 3s 32400K .......... .......... .......... .......... .......... 12% 93.9M 3s 32450K .......... .......... .......... .......... .......... 12% 64.0M 3s 32500K .......... .......... .......... .......... .......... 12% 168M 3s 32550K .......... .......... .......... .......... .......... 12% 65.5M 3s 32600K .......... .......... .......... .......... .......... 12% 114M 3s 32650K .......... .......... .......... .......... .......... 12% 96.9M 3s 32700K .......... .......... .......... .......... .......... 12% 65.6M 3s 32750K .......... .......... .......... .......... .......... 12% 61.0M 3s 32800K .......... .......... .......... .......... .......... 12% 187M 3s 32850K .......... .......... .......... .......... .......... 12% 45.6M 3s 32900K .......... .......... .......... .......... .......... 12% 57.5M 3s 32950K .......... .......... .......... .......... .......... 12% 91.4M 3s 33000K .......... .......... .......... .......... .......... 12% 51.8M 3s 33050K .......... .......... .......... .......... .......... 12% 130M 3s 33100K .......... .......... .......... .......... .......... 12% 63.7M 3s 33150K .......... .......... .......... .......... .......... 12% 117M 3s 33200K .......... .......... .......... .......... .......... 12% 64.6M 3s 33250K .......... .......... .......... .......... .......... 12% 95.0M 3s 33300K .......... .......... .......... .......... .......... 12% 91.4M 3s 33350K .......... .......... .......... .......... .......... 12% 78.0M 3s 33400K .......... .......... .......... .......... .......... 12% 119M 3s 33450K .......... .......... .......... .......... .......... 12% 75.9M 3s 33500K .......... .......... .......... .......... .......... 12% 95.7M 3s 33550K .......... .......... .......... .......... .......... 12% 71.5M 3s 33600K .......... .......... .......... .......... .......... 12% 64.5M 3s 33650K .......... .......... .......... .......... .......... 12% 134M 3s 33700K .......... .......... .......... .......... .......... 12% 58.8M 3s 33750K .......... .......... .......... .......... .......... 12% 82.6M 3s 33800K .......... .......... .......... .......... .......... 12% 117M 3s 33850K .......... .......... .......... .......... .......... 12% 94.3M 3s 33900K .......... .......... .......... .......... .......... 12% 90.9M 3s 33950K .......... .......... .......... .......... .......... 12% 66.5M 3s 34000K .......... .......... .......... .......... .......... 12% 120M 3s 34050K .......... .......... .......... .......... .......... 13% 91.3M 3s 34100K .......... .......... .......... .......... .......... 13% 67.3M 3s 34150K .......... .......... .......... .......... .......... 13% 119M 3s 34200K .......... .......... .......... .......... .......... 13% 51.1M 3s 34250K .......... .......... .......... .......... .......... 13% 226M 3s 34300K .......... .......... .......... .......... .......... 13% 63.7M 3s 34350K .......... .......... .......... .......... .......... 13% 93.7M 3s 34400K .......... .......... .......... .......... .......... 13% 74.7M 3s 34450K .......... .......... .......... .......... .......... 13% 93.4M 3s 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.......... .......... .......... 13% 313M 3s 35200K .......... .......... .......... .......... .......... 13% 162M 3s 35250K .......... .......... .......... .......... .......... 13% 332M 3s 35300K .......... .......... .......... .......... .......... 13% 317M 3s 35350K .......... .......... .......... .......... .......... 13% 43.8M 3s 35400K .......... .......... .......... .......... .......... 13% 222M 3s 35450K .......... .......... .......... .......... .......... 13% 155M 3s 35500K .......... .......... .......... .......... .......... 13% 191M 3s 35550K .......... .......... .......... .......... .......... 13% 95.2M 3s 35600K .......... .......... .......... .......... .......... 13% 75.5M 3s 35650K .......... .......... .......... .......... .......... 13% 91.1M 3s 35700K .......... .......... .......... .......... .......... 13% 65.1M 3s 35750K .......... .......... .......... .......... .......... 13% 75.6M 3s 35800K .......... .......... .......... .......... .......... 13% 119M 3s 35850K .......... .......... .......... .......... .......... 13% 65.2M 3s 35900K .......... .......... .......... .......... .......... 13% 90.8M 3s 35950K .......... .......... .......... .......... .......... 13% 65.3M 3s 36000K .......... .......... .......... .......... .......... 13% 117M 3s 36050K .......... .......... .......... .......... .......... 13% 74.5M 3s 36100K .......... .......... .......... .......... .......... 13% 75.9M 3s 36150K .......... .......... .......... .......... .......... 13% 75.8M 3s 36200K .......... .......... .......... .......... .......... 13% 73.9M 3s 36250K .......... .......... .......... .......... .......... 13% 93.4M 3s 36300K .......... .......... .......... .......... .......... 13% 81.9M 3s 36350K .......... .......... .......... .......... .......... 13% 63.3M 3s 36400K .......... .......... .......... .......... .......... 13% 76.1M 3s 36450K .......... .......... .......... .......... .......... 13% 95.2M 3s 36500K 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.......... .......... .......... 14% 75.6M 3s 37200K .......... .......... .......... .......... .......... 14% 102M 3s 37250K .......... .......... .......... .......... .......... 14% 80.7M 3s 37300K .......... .......... .......... .......... .......... 14% 41.7M 3s 37350K .......... .......... .......... .......... .......... 14% 89.8M 3s 37400K .......... .......... .......... .......... .......... 14% 51.5M 3s 37450K .......... .......... .......... .......... .......... 14% 92.1M 3s 37500K .......... .......... .......... .......... .......... 14% 61.5M 3s 37550K .......... .......... .......... .......... .......... 14% 107M 3s 37600K .......... .......... .......... .......... .......... 14% 61.9M 3s 37650K .......... .......... .......... .......... .......... 14% 119M 3s 37700K .......... .......... .......... .......... .......... 14% 76.9M 3s 37750K .......... .......... .......... .......... .......... 14% 73.2M 3s 37800K .......... .......... .......... .......... .......... 14% 97.3M 3s 37850K .......... .......... .......... .......... .......... 14% 60.8M 3s 37900K .......... .......... .......... .......... .......... 14% 93.5M 3s 37950K .......... .......... .......... .......... .......... 14% 75.2M 3s 38000K .......... .......... .......... .......... .......... 14% 99.2M 3s 38050K .......... .......... .......... .......... .......... 14% 75.5M 3s 38100K .......... .......... .......... .......... .......... 14% 90.1M 3s 38150K .......... .......... .......... .......... .......... 14% 61.8M 3s 38200K .......... .......... .......... .......... .......... 14% 79.3M 3s 38250K .......... .......... .......... .......... .......... 14% 70.5M 3s 38300K .......... .......... .......... .......... .......... 14% 111M 3s 38350K .......... .......... .......... .......... .......... 14% 109M 3s 38400K .......... .......... .......... .......... .......... 14% 96.9M 3s 38450K .......... .......... .......... .......... .......... 14% 61.9M 3s 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.......... 15% 75.6M 3s 39850K .......... .......... .......... .......... .......... 15% 62.8M 3s 39900K .......... .......... .......... .......... .......... 15% 175M 3s 39950K .......... .......... .......... .......... .......... 15% 64.1M 3s 40000K .......... .......... .......... .......... .......... 15% 90.1M 3s 40050K .......... .......... .......... .......... .......... 15% 65.9M 3s 40100K .......... .......... .......... .......... .......... 15% 75.0M 3s 40150K .......... .......... .......... .......... .......... 15% 94.1M 3s 40200K .......... .......... .......... .......... .......... 15% 61.5M 3s 40250K .......... .......... .......... .......... .......... 15% 97.9M 3s 40300K .......... .......... .......... .......... .......... 15% 90.9M 3s 40350K .......... .......... .......... .......... .......... 15% 55.9M 3s 40400K .......... .......... .......... .......... .......... 15% 112M 3s 40450K .......... .......... .......... .......... .......... 15% 56.1M 3s 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.......... .......... .......... .......... 15% 65.4M 3s 41200K .......... .......... .......... .......... .......... 15% 74.9M 3s 41250K .......... .......... .......... .......... .......... 15% 73.0M 3s 41300K .......... .......... .......... .......... .......... 15% 97.9M 3s 41350K .......... .......... .......... .......... .......... 15% 54.3M 3s 41400K .......... .......... .......... .......... .......... 15% 168M 3s 41450K .......... .......... .......... .......... .......... 15% 62.0M 3s 41500K .......... .......... .......... .......... .......... 15% 66.7M 3s 41550K .......... .......... .......... .......... .......... 15% 95.4M 3s 41600K .......... .......... .......... .......... .......... 15% 73.0M 3s 41650K .......... .......... .......... .......... .......... 15% 55.7M 3s 41700K .......... .......... .......... .......... .......... 15% 28.7M 3s 41750K .......... .......... .......... .......... .......... 15% 135M 3s 41800K .......... .......... .......... .......... .......... 15% 40.4M 3s 41850K .......... .......... .......... .......... .......... 15% 97.1M 3s 41900K .......... .......... .......... .......... .......... 15% 46.3M 3s 41950K .......... .......... .......... .......... .......... 16% 99.6M 3s 42000K .......... .......... .......... .......... .......... 16% 98.0M 3s 42050K .......... .......... .......... .......... .......... 16% 117M 3s 42100K .......... .......... .......... .......... .......... 16% 86.6M 3s 42150K .......... .......... .......... .......... .......... 16% 81.1M 3s 42200K .......... .......... .......... .......... .......... 16% 124M 3s 42250K .......... .......... .......... .......... .......... 16% 116M 3s 42300K .......... .......... .......... .......... .......... 16% 80.7M 3s 42350K .......... .......... .......... .......... .......... 16% 96.9M 3s 42400K .......... .......... .......... .......... .......... 16% 103M 3s 42450K .......... .......... .......... .......... .......... 16% 112M 3s 42500K .......... .......... .......... .......... .......... 16% 120M 3s 42550K .......... .......... .......... .......... .......... 16% 123M 3s 42600K .......... .......... .......... .......... .......... 16% 91.4M 3s 42650K .......... .......... .......... .......... .......... 16% 100M 3s 42700K .......... .......... .......... .......... .......... 16% 87.5M 3s 42750K .......... .......... .......... .......... .......... 16% 114M 3s 42800K .......... .......... .......... .......... .......... 16% 138M 3s 42850K .......... .......... .......... .......... .......... 16% 97.1M 3s 42900K .......... .......... .......... .......... .......... 16% 85.1M 3s 42950K .......... .......... .......... .......... .......... 16% 73.9M 3s 43000K .......... .......... .......... .......... .......... 16% 144M 3s 43050K .......... .......... .......... .......... .......... 16% 85.4M 3s 43100K .......... .......... .......... .......... .......... 16% 135M 3s 43150K .......... .......... .......... .......... .......... 16% 105M 3s 43200K .......... .......... .......... .......... .......... 16% 88.1M 3s 43250K .......... .......... .......... .......... .......... 16% 132M 3s 43300K .......... .......... .......... .......... .......... 16% 127M 3s 43350K .......... .......... .......... .......... .......... 16% 92.3M 3s 43400K .......... .......... .......... .......... .......... 16% 106M 3s 43450K .......... .......... .......... .......... .......... 16% 78.5M 3s 43500K .......... .......... .......... .......... .......... 16% 131M 3s 43550K .......... .......... .......... .......... .......... 16% 112M 3s 43600K .......... .......... .......... .......... .......... 16% 120M 3s 43650K .......... .......... .......... .......... .......... 16% 32.9M 3s 43700K .......... .......... .......... .......... .......... 16% 148M 3s 43750K .......... .......... .......... .......... .......... 16% 404M 3s 43800K .......... .......... .......... .......... .......... 16% 364M 3s 43850K .......... .......... .......... .......... .......... 16% 127M 3s 43900K .......... .......... .......... .......... .......... 16% 125M 3s 43950K .......... .......... .......... .......... .......... 16% 70.7M 3s 44000K .......... .......... .......... .......... .......... 16% 150M 3s 44050K .......... .......... .......... .......... .......... 16% 112M 3s 44100K .......... .......... .......... .......... .......... 16% 69.7M 3s 44150K .......... .......... .......... .......... .......... 16% 154M 3s 44200K .......... .......... .......... .......... .......... 16% 49.1M 3s 44250K .......... .......... .......... .......... .......... 16% 117M 3s 44300K .......... .......... .......... .......... .......... 16% 25.0M 3s 44350K .......... .......... .......... .......... .......... 16% 19.3M 3s 44400K .......... .......... .......... .......... .......... 16% 17.6M 3s 44450K .......... .......... .......... .......... .......... 16% 120M 3s 44500K .......... .......... .......... .......... .......... 16% 42.4M 3s 44550K .......... .......... .......... .......... .......... 17% 141M 3s 44600K .......... .......... .......... .......... .......... 17% 87.5M 3s 44650K .......... .......... .......... .......... .......... 17% 57.0M 3s 44700K .......... .......... .......... .......... .......... 17% 131M 3s 44750K .......... .......... .......... .......... .......... 17% 48.0M 3s 44800K .......... .......... .......... .......... .......... 17% 104M 3s 44850K .......... .......... .......... .......... .......... 17% 71.0M 3s 44900K .......... .......... .......... .......... .......... 17% 87.5M 3s 44950K .......... .......... .......... .......... .......... 17% 132M 3s 45000K .......... .......... .......... .......... .......... 17% 43.5M 3s 45050K .......... .......... .......... .......... .......... 17% 35.2M 3s 45100K .......... .......... .......... .......... .......... 17% 351M 3s 45150K .......... .......... .......... .......... .......... 17% 44.0M 3s 45200K .......... .......... .......... .......... .......... 17% 68.8M 3s 45250K .......... .......... .......... .......... .......... 17% 414M 3s 45300K .......... .......... .......... .......... .......... 17% 8.65M 3s 45350K .......... .......... .......... .......... .......... 17% 267M 3s 45400K .......... .......... .......... .......... .......... 17% 45.7M 3s 45450K .......... .......... .......... .......... .......... 17% 68.4M 3s 45500K .......... .......... .......... .......... .......... 17% 128M 3s 45550K .......... .......... .......... .......... .......... 17% 151M 3s 45600K .......... .......... .......... .......... .......... 17% 16.0M 3s 45650K .......... .......... .......... .......... .......... 17% 150M 3s 45700K .......... .......... .......... .......... .......... 17% 37.7M 3s 45750K .......... .......... .......... .......... .......... 17% 88.9M 3s 45800K .......... .......... .......... .......... .......... 17% 150M 3s 45850K .......... .......... .......... .......... .......... 17% 38.5M 3s 45900K .......... .......... .......... .......... .......... 17% 414M 3s 45950K .......... .......... .......... .......... .......... 17% 79.9M 3s 46000K .......... .......... .......... .......... .......... 17% 131M 3s 46050K .......... .......... .......... .......... .......... 17% 143M 3s 46100K .......... .......... .......... .......... .......... 17% 46.9M 3s 46150K .......... .......... .......... .......... .......... 17% 36.4M 3s 46200K .......... .......... .......... .......... .......... 17% 111M 3s 46250K .......... .......... .......... .......... .......... 17% 123M 3s 46300K .......... .......... .......... .......... .......... 17% 21.6M 3s 46350K .......... .......... .......... .......... .......... 17% 122M 3s 46400K .......... .......... .......... .......... .......... 17% 149M 3s 46450K .......... .......... .......... .......... .......... 17% 42.9M 3s 46500K .......... .......... .......... .......... .......... 17% 106M 3s 46550K .......... .......... .......... .......... .......... 17% 122M 3s 46600K .......... .......... .......... .......... .......... 17% 54.6M 3s 46650K .......... .......... .......... .......... .......... 17% 152M 3s 46700K .......... .......... .......... .......... .......... 17% 130M 3s 46750K .......... .......... .......... .......... .......... 17% 43.6M 3s 46800K .......... .......... .......... .......... .......... 17% 106M 3s 46850K .......... .......... .......... .......... .......... 17% 121M 3s 46900K .......... .......... .......... .......... .......... 17% 67.1M 3s 46950K .......... .......... .......... .......... .......... 17% 29.5M 3s 47000K .......... .......... .......... .......... .......... 17% 364M 3s 47050K .......... .......... .......... .......... .......... 17% 31.3M 3s 47100K .......... .......... .......... .......... .......... 17% 341M 3s 47150K .......... .......... .......... .......... .......... 18% 407M 3s 47200K .......... .......... .......... .......... .......... 18% 19.6M 3s 47250K .......... .......... .......... .......... .......... 18% 143M 3s 47300K .......... .......... .......... .......... .......... 18% 154M 3s 47350K .......... .......... .......... .......... .......... 18% 15.9M 3s 47400K .......... .......... .......... .......... .......... 18% 143M 3s 47450K .......... .......... .......... .......... .......... 18% 132M 3s 47500K .......... .......... .......... .......... .......... 18% 36.2M 3s 47550K .......... .......... .......... .......... .......... 18% 149M 3s 47600K .......... .......... .......... .......... .......... 18% 129M 3s 47650K .......... .......... .......... .......... .......... 18% 72.3M 3s 47700K .......... .......... .......... .......... .......... 18% 95.2M 3s 47750K .......... .......... .......... .......... .......... 18% 102M 3s 47800K .......... .......... .......... .......... .......... 18% 78.4M 3s 47850K .......... .......... .......... .......... .......... 18% 111M 3s 47900K .......... .......... .......... .......... .......... 18% 140M 3s 47950K .......... .......... .......... .......... .......... 18% 68.6M 3s 48000K .......... .......... .......... .......... .......... 18% 144M 3s 48050K .......... .......... .......... .......... .......... 18% 95.7M 3s 48100K .......... .......... .......... .......... .......... 18% 79.8M 3s 48150K .......... .......... .......... .......... .......... 18% 128M 3s 48200K .......... .......... .......... .......... .......... 18% 37.0M 3s 48250K .......... .......... .......... .......... .......... 18% 379M 3s 48300K .......... .......... .......... .......... .......... 18% 444M 3s 48350K .......... .......... .......... .......... .......... 18% 47.2M 3s 48400K .......... .......... .......... .......... .......... 18% 138M 3s 48450K .......... .......... .......... .......... .......... 18% 114M 3s 48500K .......... .......... 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18% 51.5M 3s 49200K .......... .......... .......... .......... .......... 18% 23.0M 3s 49250K .......... .......... .......... .......... .......... 18% 121M 3s 49300K .......... .......... .......... .......... .......... 18% 417M 3s 49350K .......... .......... .......... .......... .......... 18% 13.9M 3s 49400K .......... .......... .......... .......... .......... 18% 341M 3s 49450K .......... .......... .......... .......... .......... 18% 321M 3s 49500K .......... .......... .......... .......... .......... 18% 10.3M 3s 49550K .......... .......... .......... .......... .......... 18% 139M 3s 49600K .......... .......... .......... .......... .......... 18% 117M 3s 49650K .......... .......... .......... .......... .......... 18% 45.8M 3s 49700K .......... .......... .......... .......... .......... 18% 69.8M 3s 49750K .......... .......... .......... .......... .......... 18% 133M 3s 49800K .......... .......... .......... .......... .......... 19% 148M 3s 49850K .......... .......... .......... .......... .......... 19% 36.6M 3s 49900K .......... .......... .......... .......... .......... 19% 143M 3s 49950K .......... .......... .......... .......... .......... 19% 102M 3s 50000K .......... .......... .......... .......... .......... 19% 82.3M 3s 50050K .......... .......... .......... .......... .......... 19% 122M 3s 50100K .......... .......... .......... .......... .......... 19% 75.8M 3s 50150K .......... .......... .......... .......... .......... 19% 126M 3s 50200K .......... .......... .......... .......... .......... 19% 26.0M 3s 50250K .......... .......... .......... .......... .......... 19% 137M 3s 50300K .......... .......... .......... .......... .......... 19% 143M 3s 50350K .......... .......... .......... .......... .......... 19% 24.6M 3s 50400K .......... .......... .......... .......... .......... 19% 121M 3s 50450K .......... .......... .......... .......... .......... 19% 131M 3s 50500K .......... .......... .......... .......... .......... 19% 138M 3s 50550K .......... .......... .......... .......... .......... 19% 15.1M 3s 50600K .......... .......... .......... .......... .......... 19% 124M 3s 50650K .......... .......... .......... .......... .......... 19% 148M 3s 50700K .......... .......... .......... .......... .......... 19% 32.7M 3s 50750K .......... .......... .......... .......... .......... 19% 145M 3s 50800K .......... .......... .......... .......... .......... 19% 153M 3s 50850K .......... .......... .......... .......... .......... 19% 24.8M 3s 50900K .......... .......... .......... .......... .......... 19% 132M 3s 50950K .......... .......... .......... .......... .......... 19% 112M 3s 51000K .......... .......... .......... .......... .......... 19% 41.8M 3s 51050K .......... .......... .......... .......... .......... 19% 131M 3s 51100K .......... .......... .......... .......... .......... 19% 76.7M 3s 51150K .......... .......... .......... .......... .......... 19% 151M 3s 51200K .......... .......... .......... .......... .......... 19% 68.1M 3s 51250K .......... .......... .......... .......... .......... 19% 103M 3s 51300K .......... .......... .......... .......... .......... 19% 103M 3s 51350K .......... .......... .......... .......... .......... 19% 47.7M 3s 51400K .......... .......... .......... .......... .......... 19% 394M 3s 51450K .......... .......... .......... .......... .......... 19% 23.4M 3s 51500K .......... .......... .......... .......... .......... 19% 143M 3s 51550K .......... .......... .......... .......... .......... 19% 150M 3s 51600K .......... .......... .......... .......... .......... 19% 32.2M 3s 51650K .......... .......... .......... .......... .......... 19% 379M 3s 51700K .......... .......... .......... .......... .......... 19% 78.6M 3s 51750K .......... .......... .......... .......... .......... 19% 73.3M 3s 51800K .......... .......... .......... .......... .......... 19% 440M 3s 51850K .......... .......... .......... .......... .......... 19% 86.7M 3s 51900K .......... .......... .......... .......... .......... 19% 85.1M 3s 51950K .......... .......... .......... .......... .......... 19% 124M 3s 52000K .......... .......... .......... .......... .......... 19% 108M 3s 52050K .......... .......... .......... .......... .......... 19% 113M 3s 52100K .......... .......... .......... .......... .......... 19% 77.0M 3s 52150K .......... .......... .......... .......... .......... 19% 95.4M 3s 52200K .......... .......... .......... .......... .......... 19% 64.8M 3s 52250K .......... .......... .......... .......... .......... 19% 132M 3s 52300K .......... .......... .......... .......... .......... 19% 147M 3s 52350K .......... .......... .......... .......... .......... 19% 91.8M 3s 52400K .......... .......... .......... .......... .......... 20% 49.7M 3s 52450K .......... .......... .......... .......... .......... 20% 103M 3s 52500K .......... .......... .......... .......... .......... 20% 107M 3s 52550K .......... .......... .......... .......... .......... 20% 132M 3s 52600K .......... .......... .......... .......... .......... 20% 36.7M 3s 52650K .......... .......... .......... .......... .......... 20% 421M 3s 52700K .......... .......... .......... .......... .......... 20% 10.6M 3s 52750K .......... .......... .......... .......... .......... 20% 141M 3s 52800K .......... .......... .......... .......... .......... 20% 152M 3s 52850K .......... .......... .......... .......... .......... 20% 126M 3s 52900K .......... .......... .......... .......... .......... 20% 41.0M 3s 52950K .......... .......... .......... .......... .......... 20% 96.3M 3s 53000K .......... .......... .......... .......... .......... 20% 104M 3s 53050K .......... .......... .......... .......... .......... 20% 96.5M 3s 53100K .......... .......... .......... .......... .......... 20% 102M 3s 53150K .......... .......... .......... .......... .......... 20% 83.2M 3s 53200K .......... .......... 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20% 107M 3s 53900K .......... .......... .......... .......... .......... 20% 10.4M 3s 53950K .......... .......... .......... .......... .......... 20% 126M 3s 54000K .......... .......... .......... .......... .......... 20% 38.3M 3s 54050K .......... .......... .......... .......... .......... 20% 42.3M 3s 54100K .......... .......... .......... .......... .......... 20% 341M 3s 54150K .......... .......... .......... .......... .......... 20% 436M 3s 54200K .......... .......... .......... .......... .......... 20% 41.4M 3s 54250K .......... .......... .......... .......... .......... 20% 126M 3s 54300K .......... .......... .......... .......... .......... 20% 109M 3s 54350K .......... .......... .......... .......... .......... 20% 101M 3s 54400K .......... .......... .......... .......... .......... 20% 133M 3s 54450K .......... .......... .......... .......... .......... 20% 83.3M 3s 54500K .......... .......... .......... .......... .......... 20% 97.9M 3s 54550K .......... 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.......... .......... .......... .......... .......... 21% 138M 3s 55950K .......... .......... .......... .......... .......... 21% 68.2M 3s 56000K .......... .......... .......... .......... .......... 21% 147M 3s 56050K .......... .......... .......... .......... .......... 21% 71.2M 3s 56100K .......... .......... .......... .......... .......... 21% 81.9M 3s 56150K .......... .......... .......... .......... .......... 21% 77.8M 3s 56200K .......... .......... .......... .......... .......... 21% 79.1M 3s 56250K .......... .......... .......... .......... .......... 21% 376M 3s 56300K .......... .......... .......... .......... .......... 21% 9.56M 3s 56350K .......... .......... .......... .......... .......... 21% 121M 3s 56400K .......... .......... .......... .......... .......... 21% 143M 3s 56450K .......... .......... .......... .......... .......... 21% 36.0M 3s 56500K .......... .......... .......... .......... .......... 21% 130M 3s 56550K .......... .......... 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21% 16.3M 3s 57250K .......... .......... .......... .......... .......... 21% 315M 3s 57300K .......... .......... .......... .......... .......... 21% 421M 3s 57350K .......... .......... .......... .......... .......... 21% 99.4M 3s 57400K .......... .......... .......... .......... .......... 21% 27.5M 3s 57450K .......... .......... .......... .......... .......... 21% 127M 3s 57500K .......... .......... .......... .......... .......... 21% 22.2M 3s 57550K .......... .......... .......... .......... .......... 21% 19.0M 3s 57600K .......... .......... .......... .......... .......... 21% 36.9M 3s 57650K .......... .......... .......... .......... .......... 22% 153M 3s 57700K .......... .......... .......... .......... .......... 22% 90.1M 3s 57750K .......... .......... .......... .......... .......... 22% 85.1M 3s 57800K .......... .......... .......... .......... .......... 22% 131M 3s 57850K .......... .......... .......... .......... .......... 22% 116M 3s 57900K .......... 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61250K .......... .......... .......... .......... .......... 23% 68.0M 3s 61300K .......... .......... .......... .......... .......... 23% 82.5M 3s 61350K .......... .......... .......... .......... .......... 23% 88.1M 3s 61400K .......... .......... .......... .......... .......... 23% 59.3M 3s 61450K .......... .......... .......... .......... .......... 23% 132M 3s 61500K .......... .......... .......... .......... .......... 23% 123M 3s 61550K .......... .......... .......... .......... .......... 23% 104M 3s 61600K .......... .......... .......... .......... .......... 23% 77.6M 3s 61650K .......... .......... .......... .......... .......... 23% 107M 3s 61700K .......... .......... .......... .......... .......... 23% 95.0M 3s 61750K .......... .......... .......... .......... .......... 23% 120M 3s 61800K .......... .......... .......... .......... .......... 23% 94.8M 3s 61850K .......... .......... .......... .......... .......... 23% 91.8M 3s 61900K .......... .......... 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3s 69250K .......... .......... .......... .......... .......... 26% 265M 3s 69300K .......... .......... .......... .......... .......... 26% 294M 3s 69350K .......... .......... .......... .......... .......... 26% 79.7M 3s 69400K .......... .......... .......... .......... .......... 26% 384M 3s 69450K .......... .......... .......... .......... .......... 26% 121M 3s 69500K .......... .......... .......... .......... .......... 26% 92.1M 3s 69550K .......... .......... .......... .......... .......... 26% 142M 3s 69600K .......... .......... .......... .......... .......... 26% 328M 3s 69650K .......... .......... .......... .......... .......... 26% 334M 3s 69700K .......... .......... .......... .......... .......... 26% 65.0M 3s 69750K .......... .......... .......... .......... .......... 26% 63.7M 3s 69800K .......... .......... .......... .......... .......... 26% 90.4M 3s 69850K .......... .......... .......... .......... .......... 26% 65.5M 3s 69900K .......... .......... .......... .......... .......... 26% 73.1M 3s 69950K .......... .......... .......... .......... .......... 26% 78.4M 3s 70000K .......... .......... .......... .......... .......... 26% 73.6M 3s 70050K .......... .......... .......... .......... .......... 26% 78.8M 3s 70100K .......... .......... .......... .......... .......... 26% 61.2M 3s 70150K .......... .......... .......... .......... .......... 26% 65.7M 3s 70200K .......... .......... .......... .......... .......... 26% 75.1M 3s 70250K .......... .......... .......... .......... .......... 26% 76.5M 3s 70300K .......... .......... .......... .......... .......... 26% 90.9M 3s 70350K .......... .......... .......... .......... .......... 26% 55.2M 3s 70400K .......... .......... .......... .......... .......... 26% 75.5M 3s 70450K .......... .......... .......... .......... .......... 26% 122M 3s 70500K .......... .......... .......... .......... .......... 26% 61.9M 3s 70550K .......... .......... .......... .......... .......... 26% 76.2M 3s 70600K .......... .......... .......... .......... .......... 26% 64.2M 3s 70650K .......... .......... .......... .......... .......... 26% 120M 3s 70700K .......... .......... .......... .......... .......... 26% 63.3M 3s 70750K .......... .......... .......... .......... .......... 27% 75.6M 3s 70800K .......... .......... .......... .......... .......... 27% 74.7M 3s 70850K .......... .......... .......... .......... .......... 27% 55.9M 3s 70900K .......... .......... .......... .......... .......... 27% 127M 3s 70950K .......... .......... .......... .......... .......... 27% 63.4M 3s 71000K .......... .......... .......... .......... .......... 27% 72.9M 3s 71050K .......... .......... .......... .......... .......... 27% 78.8M 3s 71100K .......... .......... .......... .......... .......... 27% 63.5M 3s 71150K .......... .......... .......... .......... .......... 27% 120M 3s 71200K .......... .......... .......... .......... .......... 27% 76.4M 3s 71250K .......... .......... .......... .......... .......... 27% 54.1M 3s 71300K .......... .......... .......... .......... .......... 27% 94.1M 3s 71350K .......... .......... .......... .......... .......... 27% 47.9M 3s 71400K .......... .......... .......... .......... .......... 27% 94.6M 3s 71450K .......... .......... .......... .......... .......... 27% 62.2M 3s 71500K .......... .......... .......... .......... .......... 27% 73.4M 3s 71550K .......... .......... .......... .......... .......... 27% 56.1M 3s 71600K .......... .......... .......... .......... .......... 27% 117M 3s 71650K .......... .......... .......... .......... .......... 27% 76.5M 3s 71700K .......... .......... .......... .......... .......... 27% 62.4M 3s 71750K .......... .......... .......... .......... .......... 27% 96.1M 3s 71800K .......... .......... .......... .......... .......... 27% 65.1M 3s 71850K .......... .......... .......... .......... .......... 27% 88.9M 3s 71900K .......... .......... .......... .......... .......... 27% 65.5M 3s 71950K .......... .......... .......... .......... .......... 27% 72.8M 3s 72000K .......... .......... .......... .......... .......... 27% 77.8M 3s 72050K .......... .......... .......... .......... .......... 27% 85.4M 3s 72100K .......... .......... .......... .......... .......... 27% 54.4M 3s 72150K .......... .......... .......... .......... .......... 27% 98.6M 3s 72200K .......... .......... .......... .......... .......... 27% 58.3M 3s 72250K .......... .......... .......... .......... .......... 27% 86.4M 3s 72300K .......... .......... .......... .......... .......... 27% 62.7M 3s 72350K .......... .......... .......... .......... .......... 27% 118M 3s 72400K .......... .......... .......... .......... .......... 27% 42.7M 3s 72450K .......... .......... .......... .......... .......... 27% 118M 3s 72500K .......... .......... .......... .......... .......... 27% 79.4M 3s 72550K .......... .......... .......... .......... .......... 27% 156M 3s 72600K .......... .......... .......... .......... .......... 27% 96.5M 3s 72650K .......... .......... .......... .......... .......... 27% 97.3M 3s 72700K .......... .......... .......... .......... .......... 27% 92.5M 3s 72750K .......... .......... .......... .......... .......... 27% 101M 3s 72800K .......... .......... .......... .......... .......... 27% 27.7M 3s 72850K .......... .......... .......... .......... .......... 27% 131M 3s 72900K .......... .......... .......... .......... .......... 27% 291M 3s 72950K .......... .......... .......... .......... .......... 27% 273M 3s 73000K .......... .......... .......... .......... .......... 27% 229M 3s 73050K .......... .......... .......... .......... .......... 27% 54.6M 3s 73100K .......... .......... .......... .......... .......... 27% 174M 3s 73150K .......... .......... .......... .......... .......... 27% 391M 3s 73200K .......... .......... .......... .......... .......... 27% 134M 3s 73250K .......... .......... .......... .......... .......... 27% 78.5M 3s 73300K .......... .......... .......... .......... .......... 27% 74.9M 3s 73350K .......... .......... .......... .......... .......... 27% 63.8M 3s 73400K .......... .......... .......... .......... .......... 28% 124M 3s 73450K .......... .......... .......... .......... .......... 28% 61.1M 3s 73500K .......... .......... .......... .......... .......... 28% 98.6M 3s 73550K .......... .......... .......... .......... .......... 28% 88.5M 3s 73600K .......... .......... .......... .......... .......... 28% 65.5M 3s 73650K .......... .......... .......... .......... .......... 28% 94.3M 3s 73700K .......... .......... .......... .......... .......... 28% 48.8M 3s 73750K .......... .......... .......... .......... .......... 28% 59.9M 3s 73800K .......... .......... .......... .......... .......... 28% 119M 3s 73850K .......... .......... .......... .......... .......... 28% 63.6M 3s 73900K .......... .......... .......... .......... .......... 28% 95.4M 3s 73950K .......... .......... .......... .......... .......... 28% 62.2M 3s 74000K .......... .......... .......... .......... .......... 28% 91.8M 3s 74050K .......... .......... .......... .......... .......... 28% 98.6M 3s 74100K .......... .......... .......... .......... .......... 28% 61.7M 3s 74150K .......... .......... .......... .......... .......... 28% 76.3M 3s 74200K .......... .......... .......... .......... .......... 28% 93.7M 3s 74250K .......... .......... .......... .......... .......... 28% 64.8M 3s 74300K .......... .......... .......... .......... .......... 28% 119M 3s 74350K .......... .......... .......... .......... .......... 28% 63.4M 3s 74400K .......... .......... .......... .......... .......... 28% 96.9M 3s 74450K .......... .......... .......... .......... .......... 28% 63.4M 3s 74500K .......... .......... .......... .......... .......... 28% 75.2M 3s 74550K .......... .......... .......... 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57.0M 3s 75250K .......... .......... .......... .......... .......... 28% 96.3M 3s 75300K .......... .......... .......... .......... .......... 28% 68.2M 3s 75350K .......... .......... .......... .......... .......... 28% 75.7M 3s 75400K .......... .......... .......... .......... .......... 28% 93.2M 3s 75450K .......... .......... .......... .......... .......... 28% 62.0M 3s 75500K .......... .......... .......... .......... .......... 28% 75.2M 3s 75550K .......... .......... .......... .......... .......... 28% 101M 3s 75600K .......... .......... .......... .......... .......... 28% 61.3M 3s 75650K .......... .......... .......... .......... .......... 28% 77.9M 3s 75700K .......... .......... .......... .......... .......... 28% 73.2M 3s 75750K .......... .......... .......... .......... .......... 28% 97.7M 3s 75800K .......... .......... .......... .......... .......... 28% 75.0M 3s 75850K .......... .......... .......... .......... .......... 28% 73.3M 3s 75900K .......... 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.......... 29% 24.3M 3s 76600K .......... .......... .......... .......... .......... 29% 381M 3s 76650K .......... .......... .......... .......... .......... 29% 444M 3s 76700K .......... .......... .......... .......... .......... 29% 452M 3s 76750K .......... .......... .......... .......... .......... 29% 543M 3s 76800K .......... .......... .......... .......... .......... 29% 125M 3s 76850K .......... .......... .......... .......... .......... 29% 407M 3s 76900K .......... .......... .......... .......... .......... 29% 59.3M 3s 76950K .......... .......... .......... .......... .......... 29% 173M 3s 77000K .......... .......... .......... .......... .......... 29% 97.3M 3s 77050K .......... .......... .......... .......... .......... 29% 479M 3s 77100K .......... .......... .......... .......... .......... 29% 330M 2s 77150K .......... .......... .......... .......... .......... 29% 102M 2s 77200K .......... .......... .......... .......... .......... 29% 63.7M 2s 77250K .......... .......... .......... .......... .......... 29% 73.1M 2s 77300K .......... .......... .......... .......... .......... 29% 30.9M 2s 77350K .......... .......... .......... .......... .......... 29% 68.6M 2s 77400K .......... .......... .......... .......... .......... 29% 121M 2s 77450K .......... .......... .......... .......... .......... 29% 63.7M 2s 77500K .......... .......... .......... .......... .......... 29% 94.4M 2s 77550K .......... .......... .......... .......... .......... 29% 73.5M 2s 77600K .......... .......... .......... .......... .......... 29% 63.5M 2s 77650K .......... .......... .......... .......... .......... 29% 129M 2s 77700K .......... .......... .......... .......... .......... 29% 61.7M 2s 77750K .......... .......... .......... .......... .......... 29% 78.1M 2s 77800K .......... .......... .......... .......... .......... 29% 75.2M 2s 77850K .......... .......... .......... .......... .......... 29% 63.7M 2s 77900K .......... .......... 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.......... 29% 9.76M 2s 78600K .......... .......... .......... .......... .......... 29% 47.1M 2s 78650K .......... .......... .......... .......... .......... 30% 130M 2s 78700K .......... .......... .......... .......... .......... 30% 57.5M 2s 78750K .......... .......... .......... .......... .......... 30% 27.1M 2s 78800K .......... .......... .......... .......... .......... 30% 190M 2s 78850K .......... .......... .......... .......... .......... 30% 38.1M 2s 78900K .......... .......... .......... .......... .......... 30% 32.8M 2s 78950K .......... .......... .......... .......... .......... 30% 191M 2s 79000K .......... .......... .......... .......... .......... 30% 28.9M 2s 79050K .......... .......... .......... .......... .......... 30% 23.9M 2s 79100K .......... .......... .......... .......... .......... 30% 425M 2s 79150K .......... .......... .......... .......... .......... 30% 14.1M 3s 79200K .......... .......... .......... .......... .......... 30% 93.9M 2s 79250K .......... .......... .......... .......... .......... 30% 30.7M 3s 79300K .......... .......... .......... .......... .......... 30% 519M 2s 79350K .......... .......... .......... .......... .......... 30% 39.4M 2s 79400K .......... .......... .......... .......... .......... 30% 103M 2s 79450K .......... .......... .......... .......... .......... 30% 98.2M 2s 79500K .......... .......... .......... .......... .......... 30% 49.2M 2s 79550K .......... .......... .......... .......... .......... 30% 90.9M 2s 79600K .......... .......... .......... .......... .......... 30% 66.0M 2s 79650K .......... .......... .......... .......... .......... 30% 154M 2s 79700K .......... .......... .......... .......... .......... 30% 49.3M 2s 79750K .......... .......... .......... .......... .......... 30% 71.5M 2s 79800K .......... .......... .......... .......... .......... 30% 136M 2s 79850K .......... .......... .......... .......... .......... 30% 51.0M 2s 79900K .......... .......... 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.......... 30% 123M 2s 80600K .......... .......... .......... .......... .......... 30% 57.2M 2s 80650K .......... .......... .......... .......... .......... 30% 67.3M 2s 80700K .......... .......... .......... .......... .......... 30% 79.4M 2s 80750K .......... .......... .......... .......... .......... 30% 110M 2s 80800K .......... .......... .......... .......... .......... 30% 87.0M 2s 80850K .......... .......... .......... .......... .......... 30% 74.0M 2s 80900K .......... .......... .......... .......... .......... 30% 79.3M 2s 80950K .......... .......... .......... .......... .......... 30% 87.2M 2s 81000K .......... .......... .......... .......... .......... 30% 52.0M 2s 81050K .......... .......... .......... .......... .......... 30% 21.0M 2s 81100K .......... .......... .......... .......... .......... 30% 234M 2s 81150K .......... .......... .......... .......... .......... 30% 18.5M 2s 81200K .......... .......... .......... .......... .......... 30% 328M 2s 81250K .......... .......... .......... .......... .......... 31% 47.5M 2s 81300K .......... .......... .......... .......... .......... 31% 62.1M 2s 81350K .......... .......... .......... .......... .......... 31% 440M 2s 81400K .......... .......... .......... .......... .......... 31% 49.2M 2s 81450K .......... .......... .......... .......... .......... 31% 97.9M 2s 81500K .......... .......... .......... .......... .......... 31% 170M 2s 81550K .......... .......... .......... .......... .......... 31% 50.8M 2s 81600K .......... .......... .......... .......... .......... 31% 97.5M 2s 81650K .......... .......... .......... .......... .......... 31% 64.8M 2s 81700K .......... .......... .......... .......... .......... 31% 112M 2s 81750K .......... .......... .......... .......... .......... 31% 120M 2s 81800K .......... .......... .......... .......... .......... 31% 111M 2s 81850K .......... .......... .......... .......... .......... 31% 85.7M 2s 81900K .......... .......... 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.......... 31% 183M 2s 82600K .......... .......... .......... .......... .......... 31% 31.9M 2s 82650K .......... .......... .......... .......... .......... 31% 182M 2s 82700K .......... .......... .......... .......... .......... 31% 135M 2s 82750K .......... .......... .......... .......... .......... 31% 43.4M 2s 82800K .......... .......... .......... .......... .......... 31% 16.2M 2s 82850K .......... .......... .......... .......... .......... 31% 159M 2s 82900K .......... .......... .......... .......... .......... 31% 31.8M 2s 82950K .......... .......... .......... .......... .......... 31% 452M 2s 83000K .......... .......... .......... .......... .......... 31% 183M 2s 83050K .......... .......... .......... .......... .......... 31% 31.7M 2s 83100K .......... .......... .......... .......... .......... 31% 440M 2s 83150K .......... .......... .......... .......... .......... 31% 18.6M 2s 83200K .......... .......... .......... .......... .......... 31% 156M 2s 83250K 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.......... .......... .......... 32% 96.5M 2s 83950K .......... .......... .......... .......... .......... 32% 84.8M 2s 84000K .......... .......... .......... .......... .......... 32% 93.2M 2s 84050K .......... .......... .......... .......... .......... 32% 130M 2s 84100K .......... .......... .......... .......... .......... 32% 90.3M 2s 84150K .......... .......... .......... .......... .......... 32% 127M 2s 84200K .......... .......... .......... .......... .......... 32% 21.3M 2s 84250K .......... .......... .......... .......... .......... 32% 332M 2s 84300K .......... .......... .......... .......... .......... 32% 19.8M 2s 84350K .......... .......... .......... .......... .......... 32% 354M 2s 84400K .......... .......... .......... .......... .......... 32% 537M 2s 84450K .......... .......... .......... .......... .......... 32% 22.5M 2s 84500K .......... .......... .......... .......... .......... 32% 493M 2s 84550K .......... .......... .......... .......... .......... 32% 531M 2s 84600K .......... .......... .......... .......... .......... 32% 39.6M 2s 84650K .......... .......... .......... .......... .......... 32% 108M 2s 84700K .......... .......... .......... .......... .......... 32% 89.8M 2s 84750K .......... .......... .......... .......... .......... 32% 108M 2s 84800K .......... .......... .......... .......... .......... 32% 106M 2s 84850K .......... .......... .......... .......... .......... 32% 108M 2s 84900K .......... .......... .......... .......... .......... 32% 108M 2s 84950K .......... .......... .......... .......... .......... 32% 93.7M 2s 85000K .......... .......... .......... .......... .......... 32% 98.8M 2s 85050K .......... .......... .......... .......... .......... 32% 104M 2s 85100K .......... .......... .......... .......... .......... 32% 62.9M 2s 85150K .......... .......... .......... .......... .......... 32% 136M 2s 85200K .......... .......... .......... .......... .......... 32% 108M 2s 85250K .......... .......... .......... .......... .......... 32% 124M 2s 85300K .......... .......... .......... .......... .......... 32% 95.9M 2s 85350K .......... .......... .......... .......... .......... 32% 110M 2s 85400K .......... .......... .......... .......... .......... 32% 87.8M 2s 85450K .......... .......... .......... .......... .......... 32% 101M 2s 85500K .......... .......... .......... .......... .......... 32% 36.3M 2s 85550K .......... .......... .......... .......... .......... 32% 189M 2s 85600K .......... .......... .......... .......... .......... 32% 168M 2s 85650K .......... .......... .......... .......... .......... 32% 40.3M 2s 85700K .......... .......... .......... .......... .......... 32% 13.0M 2s 85750K .......... .......... .......... .......... .......... 32% 164M 2s 85800K .......... .......... .......... .......... .......... 32% 185M 2s 85850K .......... .......... .......... .......... .......... 32% 37.7M 2s 85900K .......... .......... .......... .......... .......... 32% 178M 2s 85950K .......... .......... .......... .......... .......... 32% 68.8M 2s 86000K .......... .......... .......... .......... .......... 32% 138M 2s 86050K .......... .......... .......... .......... .......... 32% 98.2M 2s 86100K .......... .......... .......... .......... .......... 32% 93.2M 2s 86150K .......... .......... .......... .......... .......... 32% 120M 2s 86200K .......... .......... .......... .......... .......... 32% 93.5M 2s 86250K .......... .......... .......... .......... .......... 32% 124M 2s 86300K .......... .......... .......... .......... .......... 32% 91.8M 2s 86350K .......... .......... .......... .......... .......... 32% 95.9M 2s 86400K .......... .......... .......... .......... .......... 32% 120M 2s 86450K .......... .......... .......... .......... .......... 32% 75.4M 2s 86500K .......... .......... .......... .......... .......... 33% 131M 2s 86550K .......... .......... .......... .......... .......... 33% 120M 2s 86600K .......... .......... .......... .......... .......... 33% 91.8M 2s 86650K .......... .......... .......... .......... .......... 33% 28.4M 2s 86700K .......... .......... .......... .......... .......... 33% 191M 2s 86750K .......... .......... .......... .......... .......... 33% 271M 2s 86800K .......... .......... .......... .......... .......... 33% 154M 2s 86850K .......... .......... .......... .......... .......... 33% 156M 2s 86900K .......... .......... .......... .......... .......... 33% 174M 2s 86950K .......... .......... .......... .......... .......... 33% 113M 2s 87000K .......... .......... .......... .......... .......... 33% 97.1M 2s 87050K .......... .......... .......... .......... .......... 33% 119M 2s 87100K .......... .......... .......... .......... .......... 33% 64.6M 2s 87150K .......... .......... .......... .......... .......... 33% 149M 2s 87200K .......... .......... .......... .......... .......... 33% 67.5M 2s 87250K .......... .......... 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88600K .......... .......... .......... .......... .......... 33% 95.4M 2s 88650K .......... .......... .......... .......... .......... 33% 125M 2s 88700K .......... .......... .......... .......... .......... 33% 76.7M 2s 88750K .......... .......... .......... .......... .......... 33% 120M 2s 88800K .......... .......... .......... .......... .......... 33% 77.1M 2s 88850K .......... .......... .......... .......... .......... 33% 120M 2s 88900K .......... .......... .......... .......... .......... 33% 76.5M 2s 88950K .......... .......... .......... .......... .......... 33% 93.4M 2s 89000K .......... .......... .......... .......... .......... 33% 90.9M 2s 89050K .......... .......... .......... .......... .......... 33% 97.5M 2s 89100K .......... .......... .......... .......... .......... 33% 92.3M 2s 89150K .......... .......... .......... .......... .......... 34% 94.1M 2s 89200K .......... .......... .......... .......... .......... 34% 89.6M 2s 89250K .......... .......... 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91950K .......... .......... .......... .......... .......... 35% 428M 2s 92000K .......... .......... .......... .......... .......... 35% 555M 2s 92050K .......... .......... .......... .......... .......... 35% 86.6M 2s 92100K .......... .......... .......... .......... .......... 35% 94.3M 2s 92150K .......... .......... .......... .......... .......... 35% 121M 2s 92200K .......... .......... .......... .......... .......... 35% 65.2M 2s 92250K .......... .......... .......... .......... .......... 35% 69.2M 2s 92300K .......... .......... .......... .......... .......... 35% 188M 2s 92350K .......... .......... .......... .......... .......... 35% 79.4M 2s 92400K .......... .......... .......... .......... .......... 35% 97.9M 2s 92450K .......... .......... .......... .......... .......... 35% 94.4M 2s 92500K .......... .......... .......... .......... .......... 35% 117M 2s 92550K .......... .......... .......... .......... .......... 35% 102M 2s 92600K .......... .......... 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93950K .......... .......... .......... .......... .......... 35% 90.8M 2s 94000K .......... .......... .......... .......... .......... 35% 77.8M 2s 94050K .......... .......... .......... .......... .......... 35% 127M 2s 94100K .......... .......... .......... .......... .......... 35% 74.0M 2s 94150K .......... .......... .......... .......... .......... 35% 98.6M 2s 94200K .......... .......... .......... .......... .......... 35% 86.7M 2s 94250K .......... .......... .......... .......... .......... 35% 80.8M 2s 94300K .......... .......... .......... .......... .......... 35% 121M 2s 94350K .......... .......... .......... .......... .......... 36% 94.3M 2s 94400K .......... .......... .......... .......... .......... 36% 77.6M 2s 94450K .......... .......... .......... .......... .......... 36% 74.3M 2s 94500K .......... .......... .......... .......... .......... 36% 119M 2s 94550K .......... .......... .......... .......... .......... 36% 96.9M 2s 94600K .......... .......... 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.......... 36% 121M 2s 95300K .......... .......... .......... .......... .......... 36% 98.8M 2s 95350K .......... .......... .......... .......... .......... 36% 94.3M 2s 95400K .......... .......... .......... .......... .......... 36% 124M 2s 95450K .......... .......... .......... .......... .......... 36% 94.8M 2s 95500K .......... .......... .......... .......... .......... 36% 19.2M 2s 95550K .......... .......... .......... .......... .......... 36% 362M 2s 95600K .......... .......... .......... .......... .......... 36% 407M 2s 95650K .......... .......... .......... .......... .......... 36% 514M 2s 95700K .......... .......... .......... .......... .......... 36% 384M 2s 95750K .......... .......... .......... .......... .......... 36% 71.0M 2s 95800K .......... .......... .......... .......... .......... 36% 448M 2s 95850K .......... .......... .......... .......... .......... 36% 89.3M 2s 95900K .......... .......... .......... .......... .......... 36% 170M 2s 95950K 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97950K .......... .......... .......... .......... .......... 37% 52.3M 2s 98000K .......... .......... .......... .......... .......... 37% 64.1M 2s 98050K .......... .......... .......... .......... .......... 37% 78.0M 2s 98100K .......... .......... .......... .......... .......... 37% 69.3M 2s 98150K .......... .......... .......... .......... .......... 37% 101M 2s 98200K .......... .......... .......... .......... .......... 37% 94.3M 2s 98250K .......... .......... .......... .......... .......... 37% 97.5M 2s 98300K .......... .......... .......... .......... .......... 37% 97.5M 2s 98350K .......... .......... .......... .......... .......... 37% 119M 2s 98400K .......... .......... .......... .......... .......... 37% 120M 2s 98450K .......... .......... .......... .......... .......... 37% 94.3M 2s 98500K .......... .......... .......... .......... .......... 37% 126M 2s 98550K .......... .......... .......... .......... .......... 37% 95.9M 2s 98600K .......... .......... .......... .......... .......... 37% 23.0M 2s 98650K .......... .......... .......... .......... .......... 37% 330M 2s 98700K .......... .......... .......... .......... .......... 37% 351M 2s 98750K .......... .......... .......... .......... .......... 37% 379M 2s 98800K .......... .......... .......... .......... .......... 37% 436M 2s 98850K .......... .......... .......... .......... .......... 37% 45.5M 2s 98900K .......... .......... .......... .......... .......... 37% 119M 2s 98950K .......... .......... .......... .......... .......... 37% 263M 2s 99000K .......... .......... .......... .......... .......... 37% 404M 2s 99050K .......... .......... .......... .......... .......... 37% 234M 2s 99100K .......... .......... .......... .......... .......... 37% 95.0M 2s 99150K .......... .......... .......... .......... .......... 37% 91.6M 2s 99200K .......... .......... .......... .......... .......... 37% 93.7M 2s 99250K .......... .......... .......... .......... .......... 37% 99.9M 2s 99300K .......... .......... .......... .......... .......... 37% 94.6M 2s 99350K .......... .......... .......... .......... .......... 37% 93.9M 2s 99400K .......... .......... .......... .......... .......... 37% 75.6M 2s 99450K .......... .......... .......... .......... .......... 37% 94.4M 2s 99500K .......... .......... .......... .......... .......... 37% 94.6M 2s 99550K .......... .......... .......... .......... .......... 37% 121M 2s 99600K .......... .......... .......... .......... .......... 38% 77.3M 2s 99650K .......... .......... .......... .......... .......... 38% 120M 2s 99700K .......... .......... .......... .......... .......... 38% 93.4M 2s 99750K .......... .......... .......... .......... .......... 38% 95.7M 2s 99800K .......... .......... .......... .......... .......... 38% 97.5M 2s 99850K .......... .......... .......... .......... .......... 38% 91.6M 2s 99900K .......... .......... .......... .......... .......... 38% 97.3M 2s 99950K .......... .......... .......... .......... .......... 38% 92.1M 2s 100000K .......... .......... .......... .......... .......... 38% 97.7M 2s 100050K .......... .......... .......... .......... .......... 38% 94.4M 2s 100100K .......... .......... .......... .......... .......... 38% 93.9M 2s 100150K .......... .......... .......... .......... .......... 38% 93.4M 2s 100200K .......... .......... .......... .......... .......... 38% 95.0M 2s 100250K .......... .......... .......... .......... .......... 38% 92.5M 2s 100300K .......... .......... .......... .......... .......... 38% 95.2M 2s 100350K .......... .......... .......... .......... .......... 38% 91.6M 2s 100400K .......... .......... .......... .......... .......... 38% 127M 2s 100450K .......... .......... .......... .......... .......... 38% 76.2M 2s 100500K .......... .......... .......... .......... .......... 38% 120M 2s 100550K .......... .......... .......... .......... .......... 38% 97.7M 2s 100600K .......... .......... .......... .......... .......... 38% 90.3M 2s 100650K .......... .......... .......... .......... .......... 38% 95.4M 2s 100700K .......... .......... .......... .......... .......... 38% 91.1M 2s 100750K .......... .......... .......... .......... .......... 38% 99.2M 2s 100800K .......... .......... .......... .......... .......... 38% 97.9M 2s 100850K .......... .......... .......... .......... .......... 38% 91.1M 2s 100900K .......... .......... .......... .......... .......... 38% 97.7M 2s 100950K .......... .......... .......... .......... .......... 38% 94.8M 2s 101000K .......... .......... .......... .......... .......... 38% 94.6M 2s 101050K .......... .......... .......... .......... .......... 38% 120M 2s 101100K .......... .......... .......... .......... .......... 38% 76.5M 2s 101150K .......... .......... .......... .......... .......... 38% 119M 2s 101200K .......... .......... .......... .......... .......... 38% 78.3M 2s 101250K .......... .......... .......... .......... .......... 38% 91.1M 2s 101300K .......... .......... .......... .......... .......... 38% 123M 2s 101350K .......... .......... .......... .......... .......... 38% 98.4M 2s 101400K .......... .......... .......... .......... .......... 38% 92.8M 2s 101450K .......... .......... .......... .......... .......... 38% 82.5M 2s 101500K .......... .......... .......... .......... .......... 38% 101M 2s 101550K .......... .......... .......... .......... .......... 38% 85.4M 2s 101600K .......... .......... .......... .......... .......... 38% 103M 2s 101650K .......... .......... .......... .......... .......... 38% 79.9M 2s 101700K .......... .......... .......... .......... .......... 38% 94.6M 2s 101750K .......... .......... .......... .......... .......... 38% 94.3M 2s 101800K .......... .......... .......... .......... .......... 38% 119M 2s 101850K .......... .......... .......... .......... .......... 38% 77.3M 2s 101900K .......... .......... .......... .......... .......... 38% 94.3M 2s 101950K .......... .......... .......... .......... .......... 38% 95.2M 2s 102000K .......... .......... .......... .......... .......... 38% 95.0M 2s 102050K .......... .......... .......... .......... .......... 38% 119M 2s 102100K .......... .......... .......... .......... .......... 38% 94.8M 2s 102150K .......... .......... .......... .......... .......... 38% 95.2M 2s 102200K .......... .......... .......... .......... .......... 38% 77.3M 2s 102250K .......... .......... .......... .......... .......... 39% 123M 2s 102300K .......... .......... .......... .......... .......... 39% 94.3M 2s 102350K .......... .......... .......... .......... .......... 39% 92.7M 2s 102400K .......... .......... .......... .......... .......... 39% 96.7M 2s 102450K .......... .......... .......... .......... .......... 39% 91.4M 2s 102500K .......... .......... .......... .......... .......... 39% 125M 2s 102550K .......... .......... .......... .......... .......... 39% 98.8M 2s 102600K .......... .......... .......... .......... .......... 39% 94.1M 2s 102650K .......... .......... .......... .......... .......... 39% 120M 2s 102700K .......... .......... .......... .......... .......... 39% 93.4M 2s 102750K .......... .......... .......... .......... .......... 39% 19.9M 2s 102800K .......... .......... .......... .......... .......... 39% 474M 2s 102850K .......... .......... .......... .......... .......... 39% 400M 2s 102900K .......... .......... .......... .......... .......... 39% 483M 2s 102950K .......... .......... .......... .......... .......... 39% 113M 2s 103000K .......... .......... .......... .......... .......... 39% 519M 2s 103050K .......... .......... .......... .......... .......... 39% 41.0M 2s 103100K .......... .......... .......... .......... .......... 39% 131M 2s 103150K .......... .......... .......... .......... .......... 39% 174M 2s 103200K .......... .......... .......... .......... .......... 39% 151M 2s 103250K .......... .......... .......... .......... .......... 39% 183M 2s 103300K .......... .......... .......... .......... .......... 39% 175M 2s 103350K .......... .......... .......... .......... .......... 39% 148M 2s 103400K .......... .......... .......... .......... .......... 39% 124M 2s 103450K .......... .......... .......... .......... .......... 39% 92.7M 2s 103500K .......... .......... .......... .......... .......... 39% 76.8M 2s 103550K .......... .......... .......... .......... .......... 39% 126M 2s 103600K .......... .......... .......... .......... .......... 39% 75.2M 2s 103650K .......... .......... .......... .......... .......... 39% 120M 2s 103700K .......... .......... .......... .......... .......... 39% 77.4M 2s 103750K .......... .......... .......... .......... .......... 39% 120M 2s 103800K .......... .......... .......... .......... .......... 39% 94.8M 2s 103850K .......... .......... .......... .......... .......... 39% 93.4M 2s 103900K .......... .......... .......... .......... .......... 39% 96.1M 2s 103950K .......... .......... .......... .......... .......... 39% 92.8M 2s 104000K .......... .......... .......... .......... .......... 39% 95.0M 2s 104050K .......... .......... .......... .......... .......... 39% 95.0M 2s 104100K .......... .......... .......... .......... .......... 39% 98.0M 2s 104150K .......... .......... .......... .......... .......... 39% 92.8M 2s 104200K .......... .......... .......... .......... .......... 39% 93.5M 2s 104250K .......... .......... .......... .......... .......... 39% 96.3M 2s 104300K .......... .......... .......... .......... .......... 39% 94.4M 2s 104350K .......... .......... .......... .......... .......... 39% 94.6M 2s 104400K .......... .......... .......... .......... .......... 39% 119M 2s 104450K .......... .......... .......... .......... .......... 39% 77.8M 2s 104500K .......... .......... .......... .......... .......... 39% 95.4M 2s 104550K .......... .......... .......... .......... .......... 39% 120M 2s 104600K .......... .......... .......... .......... .......... 39% 77.9M 2s 104650K .......... .......... .......... .......... .......... 39% 120M 2s 104700K .......... .......... .......... .......... .......... 39% 77.0M 2s 104750K .......... .......... .......... .......... .......... 39% 94.8M 2s 104800K .......... .......... .......... .......... .......... 39% 125M 2s 104850K .......... .......... .......... .......... .......... 40% 90.1M 2s 104900K .......... .......... .......... .......... .......... 40% 99.6M 2s 104950K .......... .......... .......... .......... .......... 40% 91.3M 2s 105000K .......... .......... .......... .......... .......... 40% 95.0M 2s 105050K .......... .......... .......... .......... .......... 40% 97.5M 2s 105100K .......... .......... .......... .......... .......... 40% 94.8M 2s 105150K .......... .......... .......... .......... .......... 40% 79.4M 2s 105200K .......... .......... .......... .......... .......... 40% 124M 2s 105250K .......... .......... .......... .......... .......... 40% 79.5M 2s 105300K .......... .......... .......... .......... .......... 40% 123M 2s 105350K .......... .......... .......... .......... .......... 40% 77.5M 2s 105400K .......... .......... .......... .......... .......... 40% 119M 2s 105450K .......... .......... .......... .......... .......... 40% 77.3M 2s 105500K .......... .......... .......... .......... .......... 40% 95.4M 2s 105550K .......... .......... .......... .......... .......... 40% 126M 2s 105600K .......... .......... .......... .......... .......... 40% 91.4M 2s 105650K .......... .......... .......... .......... .......... 40% 96.7M 2s 105700K .......... .......... .......... .......... .......... 40% 75.1M 2s 105750K .......... .......... .......... .......... .......... 40% 127M 2s 105800K .......... .......... .......... .......... .......... 40% 94.3M 2s 105850K .......... .......... .......... .......... .......... 40% 93.9M 2s 105900K .......... .......... .......... .......... .......... 40% 95.0M 2s 105950K .......... .......... .......... .......... .......... 40% 92.7M 2s 106000K .......... .......... .......... .......... .......... 40% 97.5M 2s 106050K .......... .......... .......... .......... .......... 40% 119M 2s 106100K .......... .......... .......... .......... .......... 40% 78.5M 2s 106150K .......... .......... .......... .......... .......... 40% 119M 2s 106200K .......... .......... .......... .......... .......... 40% 77.8M 2s 106250K .......... .......... .......... .......... .......... 40% 120M 2s 106300K .......... .......... .......... .......... .......... 40% 98.4M 2s 106350K .......... .......... .......... .......... .......... 40% 91.4M 2s 106400K .......... .......... .......... .......... .......... 40% 94.8M 2s 106450K .......... .......... .......... .......... .......... 40% 47.9M 2s 106500K .......... .......... .......... .......... .......... 40% 488M 2s 106550K .......... .......... .......... .......... .......... 40% 61.3M 2s 106600K .......... .......... .......... .......... .......... 40% 120M 2s 106650K .......... .......... .......... .......... .......... 40% 97.3M 2s 106700K .......... .......... .......... .......... .......... 40% 93.4M 2s 106750K .......... .......... .......... .......... .......... 40% 92.3M 2s 106800K .......... .......... .......... .......... .......... 40% 122M 2s 106850K .......... .......... .......... .......... .......... 40% 71.6M 2s 106900K .......... .......... .......... .......... .......... 40% 168M 2s 106950K .......... .......... .......... .......... .......... 40% 69.1M 2s 107000K .......... .......... .......... .......... .......... 40% 121M 2s 107050K .......... .......... .......... .......... .......... 40% 126M 2s 107100K .......... .......... .......... .......... .......... 40% 95.2M 2s 107150K .......... .......... .......... .......... .......... 40% 97.7M 2s 107200K .......... .......... .......... .......... .......... 40% 119M 2s 107250K .......... .......... .......... .......... .......... 40% 96.7M 2s 107300K .......... .......... .......... .......... .......... 40% 122M 2s 107350K .......... .......... .......... .......... .......... 40% 17.3M 2s 107400K .......... .......... .......... .......... .......... 40% 461M 2s 107450K .......... .......... .......... .......... .......... 40% 440M 2s 107500K .......... .......... .......... .......... .......... 41% 180M 2s 107550K .......... .......... .......... .......... .......... 41% 514M 2s 107600K .......... .......... .......... .......... .......... 41% 456M 2s 107650K .......... .......... .......... .......... .......... 41% 67.3M 2s 107700K .......... .......... .......... .......... .......... 41% 84.3M 2s 107750K .......... .......... .......... .......... .......... 41% 243M 2s 107800K .......... .......... .......... .......... .......... 41% 452M 2s 107850K .......... .......... .......... .......... .......... 41% 241M 2s 107900K .......... .......... .......... .......... .......... 41% 119M 2s 107950K .......... .......... .......... .......... .......... 41% 75.5M 2s 108000K .......... .......... .......... .......... .......... 41% 78.0M 2s 108050K .......... .......... .......... .......... .......... 41% 125M 2s 108100K .......... .......... .......... .......... .......... 41% 90.8M 2s 108150K .......... .......... .......... .......... .......... 41% 94.3M 2s 108200K .......... .......... .......... .......... .......... 41% 76.9M 2s 108250K .......... .......... .......... .......... .......... 41% 102M 2s 108300K .......... .......... .......... .......... .......... 41% 87.2M 2s 108350K .......... .......... .......... .......... .......... 41% 75.9M 2s 108400K .......... .......... .......... .......... .......... 41% 92.7M 2s 108450K .......... .......... .......... .......... .......... 41% 75.5M 2s 108500K .......... .......... .......... .......... .......... 41% 126M 2s 108550K .......... .......... .......... .......... .......... 41% 92.0M 2s 108600K .......... .......... .......... .......... .......... 41% 78.1M 2s 108650K .......... .......... .......... .......... .......... 41% 120M 2s 108700K .......... .......... .......... .......... .......... 41% 77.4M 2s 108750K .......... .......... .......... .......... .......... 41% 123M 2s 108800K .......... .......... .......... .......... .......... 41% 92.0M 2s 108850K .......... .......... .......... .......... .......... 41% 78.6M 2s 108900K .......... .......... .......... .......... .......... 41% 90.9M 2s 108950K .......... .......... .......... .......... .......... 41% 91.8M 2s 109000K .......... .......... .......... .......... .......... 41% 98.0M 2s 109050K .......... .......... .......... .......... .......... 41% 93.9M 2s 109100K .......... .......... .......... .......... .......... 41% 91.4M 2s 109150K .......... .......... .......... .......... .......... 41% 98.0M 2s 109200K .......... .......... .......... .......... .......... 41% 81.5M 2s 109250K .......... .......... .......... .......... .......... 41% 107M 2s 109300K .......... .......... .......... .......... .......... 41% 93.0M 2s 109350K .......... .......... .......... .......... .......... 41% 86.9M 2s 109400K .......... .......... .......... .......... .......... 41% 103M 2s 109450K .......... .......... .......... .......... .......... 41% 93.4M 2s 109500K .......... .......... .......... .......... .......... 41% 75.4M 2s 109550K .......... .......... .......... .......... .......... 41% 127M 2s 109600K .......... .......... .......... .......... .......... 41% 69.7M 2s 109650K .......... .......... .......... .......... .......... 41% 137M 2s 109700K .......... .......... .......... .......... .......... 41% 63.9M 2s 109750K .......... .......... .......... .......... .......... 41% 121M 2s 109800K .......... .......... .......... .......... .......... 41% 93.7M 2s 109850K .......... .......... .......... .......... .......... 41% 75.8M 2s 109900K .......... .......... .......... .......... .......... 41% 122M 2s 109950K .......... .......... .......... .......... .......... 41% 76.2M 2s 110000K .......... .......... .......... .......... .......... 41% 96.9M 2s 110050K .......... .......... .......... .......... .......... 41% 94.6M 2s 110100K .......... .......... .......... .......... .......... 42% 94.4M 2s 110150K .......... .......... .......... .......... .......... 42% 73.3M 2s 110200K .......... .......... .......... .......... .......... 42% 96.9M 2s 110250K .......... .......... .......... .......... .......... 42% 94.8M 2s 110300K .......... .......... .......... .......... .......... 42% 94.1M 2s 110350K .......... .......... .......... .......... .......... 42% 95.2M 2s 110400K .......... .......... .......... .......... .......... 42% 121M 2s 110450K .......... .......... .......... .......... .......... 42% 63.1M 2s 110500K .......... .......... .......... .......... .......... 42% 121M 2s 110550K .......... .......... .......... .......... .......... 42% 104M 2s 110600K .......... .......... .......... .......... .......... 42% 88.0M 2s 110650K .......... .......... .......... .......... .......... 42% 73.0M 2s 110700K .......... .......... .......... .......... .......... 42% 99.9M 2s 110750K .......... .......... .......... .......... .......... 42% 119M 2s 110800K .......... .......... .......... .......... .......... 42% 79.5M 2s 110850K .......... .......... .......... .......... .......... 42% 93.2M 2s 110900K .......... .......... .......... .......... .......... 42% 77.8M 2s 110950K .......... .......... .......... .......... .......... 42% 119M 2s 111000K .......... .......... .......... .......... .......... 42% 121M 2s 111050K .......... .......... .......... .......... .......... 42% 88.0M 2s 111100K .......... .......... .......... .......... .......... 42% 105M 2s 111150K .......... .......... .......... .......... .......... 42% 93.9M 2s 111200K .......... .......... .......... .......... .......... 42% 95.2M 2s 111250K .......... .......... .......... .......... .......... 42% 102M 2s 111300K .......... .......... .......... .......... .......... 42% 114M 2s 111350K .......... .......... .......... .......... .......... 42% 79.4M 2s 111400K .......... .......... .......... .......... .......... 42% 128M 2s 111450K .......... .......... .......... .......... .......... 42% 110M 2s 111500K .......... .......... .......... .......... .......... 42% 95.0M 2s 111550K .......... .......... .......... .......... .......... 42% 19.9M 2s 111600K .......... .......... .......... .......... .......... 42% 421M 2s 111650K .......... .......... .......... .......... .......... 42% 479M 2s 111700K .......... .......... .......... .......... .......... 42% 43.4M 2s 111750K .......... .......... .......... .......... .......... 42% 165M 2s 111800K .......... .......... .......... .......... .......... 42% 174M 2s 111850K .......... .......... .......... .......... .......... 42% 151M 2s 111900K .......... .......... .......... .......... .......... 42% 176M 2s 111950K .......... .......... .......... .......... .......... 42% 156M 2s 112000K .......... .......... .......... .......... .......... 42% 289M 2s 112050K .......... .......... .......... .......... .......... 42% 397M 2s 112100K .......... .......... .......... .......... .......... 42% 286M 2s 112150K .......... .......... .......... .......... .......... 42% 93.7M 2s 112200K .......... .......... .......... .......... .......... 42% 122M 2s 112250K .......... .......... .......... .......... .......... 42% 77.4M 2s 112300K .......... .......... .......... .......... .......... 42% 94.4M 2s 112350K .......... .......... .......... .......... .......... 42% 39.4M 2s 112400K .......... .......... .......... .......... .......... 42% 456M 2s 112450K .......... .......... .......... .......... .......... 42% 55.4M 2s 112500K .......... .......... .......... .......... .......... 42% 134M 2s 112550K .......... .......... .......... .......... .......... 42% 93.9M 2s 112600K .......... .......... .......... .......... .......... 42% 93.0M 2s 112650K .......... .......... .......... .......... .......... 42% 118M 2s 112700K .......... .......... .......... .......... .......... 43% 77.9M 2s 112750K .......... .......... .......... .......... .......... 43% 72.1M 2s 112800K .......... .......... .......... .......... .......... 43% 124M 2s 112850K .......... .......... .......... .......... .......... 43% 71.0M 2s 112900K .......... .......... .......... .......... .......... 43% 138M 2s 112950K .......... .......... .......... .......... .......... 43% 54.6M 2s 113000K .......... .......... .......... .......... .......... 43% 55.2M 2s 113050K .......... .......... .......... .......... .......... 43% 52.8M 2s 113100K .......... .......... .......... .......... .......... 43% 126M 2s 113150K .......... .......... .......... .......... .......... 43% 94.8M 2s 113200K .......... .......... .......... .......... .......... 43% 90.8M 2s 113250K .......... .......... .......... .......... .......... 43% 98.6M 2s 113300K .......... .......... .......... .......... .......... 43% 125M 2s 113350K .......... .......... .......... .......... .......... 43% 91.8M 2s 113400K .......... .......... .......... .......... .......... 43% 126M 2s 113450K .......... .......... .......... .......... .......... 43% 95.2M 2s 113500K .......... .......... .......... .......... .......... 43% 77.3M 2s 113550K .......... .......... .......... .......... .......... 43% 120M 2s 113600K .......... .......... .......... .......... .......... 43% 94.3M 2s 113650K .......... .......... .......... .......... .......... 43% 91.4M 2s 113700K .......... .......... .......... .......... .......... 43% 94.6M 2s 113750K .......... .......... .......... .......... .......... 43% 77.3M 2s 113800K .......... .......... .......... .......... .......... 43% 116M 2s 113850K .......... .......... .......... .......... .......... 43% 73.5M 2s 113900K .......... .......... .......... .......... .......... 43% 134M 2s 113950K .......... .......... .......... .......... .......... 43% 71.8M 2s 114000K .......... .......... .......... .......... .......... 43% 104M 2s 114050K .......... .......... .......... .......... .......... 43% 87.0M 2s 114100K .......... .......... .......... .......... .......... 43% 85.2M 2s 114150K .......... .......... .......... .......... .......... 43% 85.8M 2s 114200K .......... .......... .......... .......... .......... 43% 94.8M 2s 114250K .......... .......... .......... .......... .......... 43% 96.5M 2s 114300K .......... .......... .......... .......... .......... 43% 94.3M 2s 114350K .......... .......... .......... .......... .......... 43% 94.6M 2s 114400K .......... .......... .......... .......... .......... 43% 75.5M 2s 114450K .......... .......... .......... .......... .......... 43% 119M 2s 114500K .......... .......... .......... .......... .......... 43% 77.1M 2s 114550K .......... .......... .......... .......... .......... 43% 125M 2s 114600K .......... .......... .......... .......... .......... 43% 75.7M 2s 114650K .......... .......... .......... .......... .......... 43% 71.9M 2s 114700K .......... .......... .......... .......... .......... 43% 192M 2s 114750K .......... .......... .......... .......... .......... 43% 74.2M 2s 114800K .......... .......... .......... .......... .......... 43% 124M 2s 114850K .......... .......... .......... .......... .......... 43% 94.4M 2s 114900K .......... .......... .......... .......... .......... 43% 96.9M 2s 114950K .......... .......... .......... .......... .......... 43% 91.3M 2s 115000K .......... .......... .......... .......... .......... 43% 96.5M 2s 115050K .......... .......... .......... .......... .......... 43% 92.7M 2s 115100K .......... .......... .......... .......... .......... 43% 94.3M 2s 115150K .......... .......... .......... .......... .......... 43% 95.0M 2s 115200K .......... .......... .......... .......... .......... 43% 91.3M 2s 115250K .......... .......... .......... .......... .......... 43% 99.2M 2s 115300K .......... .......... .......... .......... .......... 43% 94.6M 2s 115350K .......... .......... .......... .......... .......... 44% 120M 2s 115400K .......... .......... .......... .......... .......... 44% 97.5M 2s 115450K .......... .......... .......... .......... .......... 44% 93.4M 2s 115500K .......... .......... .......... .......... .......... 44% 21.4M 2s 115550K .......... .......... .......... .......... .......... 44% 268M 2s 115600K .......... .......... .......... .......... .......... 44% 440M 2s 115650K .......... .......... .......... .......... .......... 44% 503M 2s 115700K .......... .......... .......... .......... .......... 44% 97.9M 2s 115750K .......... .......... .......... .......... .......... 44% 525M 2s 115800K .......... .......... .......... .......... .......... 44% 52.3M 2s 115850K .......... .......... .......... .......... .......... 44% 117M 2s 115900K .......... .......... .......... .......... .......... 44% 106M 2s 115950K .......... .......... .......... .......... .......... 44% 303M 2s 116000K .......... .......... .......... .......... .......... 44% 75.9M 2s 116050K .......... .......... .......... .......... .......... 44% 421M 2s 116100K .......... .......... .......... .......... .......... 44% 400M 2s 116150K .......... .......... .......... .......... .......... 44% 97.1M 2s 116200K .......... .......... .......... .......... .......... 44% 61.9M 2s 116250K .......... .......... .......... .......... .......... 44% 65.5M 2s 116300K .......... .......... .......... .......... .......... 44% 63.2M 2s 116350K .......... .......... .......... .......... .......... 44% 61.8M 2s 116400K .......... .......... .......... .......... .......... 44% 126M 2s 116450K .......... .......... .......... .......... .......... 44% 54.7M 2s 116500K .......... .......... .......... .......... .......... 44% 61.7M 2s 116550K .......... .......... .......... .......... .......... 44% 64.4M 2s 116600K .......... .......... .......... .......... .......... 44% 95.2M 2s 116650K .......... .......... .......... .......... .......... 44% 94.3M 2s 116700K .......... .......... .......... .......... .......... 44% 61.2M 2s 116750K .......... .......... .......... .......... .......... 44% 73.8M 2s 116800K .......... .......... .......... .......... .......... 44% 54.6M 2s 116850K .......... .......... .......... .......... .......... 44% 89.4M 2s 116900K .......... .......... .......... .......... .......... 44% 65.3M 2s 116950K .......... .......... .......... .......... .......... 44% 48.6M 2s 117000K .......... .......... .......... .......... .......... 44% 54.1M 2s 117050K .......... .......... .......... .......... .......... 44% 124M 2s 117100K .......... .......... .......... .......... .......... 44% 55.1M 2s 117150K .......... .......... .......... .......... .......... 44% 69.7M 2s 117200K .......... .......... .......... .......... .......... 44% 79.5M 2s 117250K .......... .......... .......... .......... .......... 44% 90.3M 2s 117300K .......... .......... .......... .......... .......... 44% 63.4M 2s 117350K .......... .......... .......... .......... .......... 44% 77.1M 2s 117400K .......... .......... .......... .......... .......... 44% 75.2M 2s 117450K .......... .......... .......... .......... .......... 44% 54.3M 2s 117500K .......... .......... .......... .......... .......... 44% 63.2M 2s 117550K .......... .......... .......... .......... .......... 44% 122M 2s 117600K .......... .......... .......... .......... .......... 44% 63.0M 2s 117650K .......... .......... .......... .......... .......... 44% 76.3M 2s 117700K .......... .......... .......... .......... .......... 44% 55.0M 2s 117750K .......... .......... .......... .......... .......... 44% 128M 2s 117800K .......... .......... .......... .......... .......... 44% 74.8M 2s 117850K .......... .......... .......... .......... .......... 44% 92.1M 2s 117900K .......... .......... .......... .......... .......... 44% 76.2M 2s 117950K .......... .......... .......... .......... .......... 45% 75.6M 2s 118000K .......... .......... .......... .......... .......... 45% 64.7M 2s 118050K .......... .......... .......... .......... .......... 45% 50.4M 2s 118100K .......... .......... .......... .......... .......... 45% 72.7M 2s 118150K .......... .......... .......... .......... .......... 45% 64.7M 2s 118200K .......... .......... .......... .......... .......... 45% 61.4M 2s 118250K .......... .......... .......... .......... .......... 45% 65.5M 2s 118300K .......... .......... .......... .......... .......... 45% 72.6M 2s 118350K .......... .......... .......... .......... .......... 45% 54.9M 2s 118400K .......... .......... .......... .......... .......... 45% 93.2M 2s 118450K .......... .......... .......... .......... .......... 45% 63.5M 2s 118500K .......... .......... .......... .......... .......... 45% 53.6M 2s 118550K .......... .......... .......... .......... .......... 45% 92.7M 2s 118600K .......... .......... .......... .......... .......... 45% 61.0M 2s 118650K .......... .......... .......... .......... .......... 45% 79.3M 2s 118700K .......... .......... .......... .......... .......... 45% 90.9M 2s 118750K .......... .......... .......... .......... .......... 45% 135M 2s 118800K .......... .......... .......... .......... .......... 45% 96.9M 2s 118850K .......... .......... .......... .......... .......... 45% 94.8M 2s 118900K .......... .......... .......... .......... .......... 45% 123M 2s 118950K .......... .......... .......... .......... .......... 45% 64.0M 2s 119000K .......... .......... .......... .......... .......... 45% 28.2M 2s 119050K .......... .......... .......... .......... .......... 45% 394M 2s 119100K .......... .......... .......... .......... .......... 45% 440M 2s 119150K .......... .......... .......... .......... .......... 45% 421M 2s 119200K .......... .......... .......... .......... .......... 45% 119M 2s 119250K .......... .......... .......... .......... .......... 45% 57.6M 2s 119300K .......... .......... .......... .......... .......... 45% 514M 2s 119350K .......... .......... .......... .......... .......... 45% 140M 2s 119400K .......... .......... .......... .......... .......... 45% 92.5M 2s 119450K .......... .......... .......... .......... .......... 45% 121M 2s 119500K .......... .......... .......... .......... .......... 45% 99.2M 2s 119550K .......... .......... .......... .......... .......... 45% 120M 2s 119600K .......... .......... .......... .......... .......... 45% 93.7M 2s 119650K .......... .......... .......... .......... .......... 45% 126M 2s 119700K .......... .......... .......... .......... .......... 45% 94.6M 2s 119750K .......... .......... .......... .......... .......... 45% 21.1M 2s 119800K .......... .......... .......... .......... .......... 45% 309M 2s 119850K .......... .......... .......... .......... .......... 45% 268M 2s 119900K .......... .......... .......... .......... .......... 45% 519M 2s 119950K .......... .......... .......... .......... .......... 45% 56.4M 2s 120000K .......... .......... .......... .......... .......... 45% 509M 2s 120050K .......... .......... .......... .......... .......... 45% 53.1M 2s 120100K .......... .......... .......... .......... .......... 45% 45.8M 2s 120150K .......... .......... .......... .......... .......... 45% 249M 2s 120200K .......... .......... .......... .......... .......... 45% 349M 2s 120250K .......... .......... .......... .......... .......... 45% 381M 2s 120300K .......... .......... .......... .......... .......... 45% 124M 2s 120350K .......... .......... .......... .......... .......... 45% 136M 2s 120400K .......... .......... .......... .......... .......... 45% 148M 2s 120450K .......... .......... .......... .......... .......... 45% 75.9M 2s 120500K .......... .......... .......... .......... .......... 45% 514M 2s 120550K .......... .......... .......... .......... .......... 45% 305M 2s 120600K .......... .......... .......... .......... .......... 46% 91.1M 2s 120650K .......... .......... .......... .......... .......... 46% 55.3M 2s 120700K .......... .......... .......... .......... .......... 46% 54.2M 2s 120750K .......... .......... .......... .......... .......... 46% 63.3M 2s 120800K .......... .......... .......... .......... .......... 46% 75.4M 2s 120850K .......... .......... .......... .......... .......... 46% 63.3M 2s 120900K .......... .......... .......... .......... .......... 46% 93.7M 2s 120950K .......... .......... .......... .......... .......... 46% 63.7M 2s 121000K .......... .......... .......... .......... .......... 46% 77.8M 2s 121050K .......... .......... .......... .......... .......... 46% 73.8M 2s 121100K .......... .......... .......... .......... .......... 46% 65.0M 2s 121150K .......... .......... .......... .......... .......... 46% 90.1M 2s 121200K .......... .......... .......... .......... .......... 46% 55.6M 2s 121250K .......... .......... .......... .......... .......... 46% 90.3M 2s 121300K .......... .......... .......... .......... .......... 46% 65.5M 2s 121350K .......... .......... .......... .......... .......... 46% 75.9M 2s 121400K .......... .......... .......... .......... .......... 46% 74.3M 2s 121450K .......... .......... .......... .......... .......... 46% 55.0M 2s 121500K .......... .......... .......... .......... .......... 46% 88.1M 2s 121550K .......... .......... .......... .......... .......... 46% 67.2M 2s 121600K .......... .......... .......... .......... .......... 46% 76.2M 2s 121650K .......... .......... .......... .......... .......... 46% 94.4M 2s 121700K .......... .......... .......... .......... .......... 46% 46.8M 2s 121750K .......... .......... .......... .......... .......... 46% 64.9M 2s 121800K .......... .......... .......... .......... .......... 46% 95.4M 2s 121850K .......... .......... .......... .......... .......... 46% 63.2M 2s 121900K .......... .......... .......... .......... .......... 46% 73.1M 2s 121950K .......... .......... .......... .......... .......... 46% 55.3M 2s 122000K .......... .......... .......... .......... .......... 46% 61.5M 2s 122050K .......... .......... .......... .......... .......... 46% 97.5M 2s 122100K .......... .......... .......... .......... .......... 46% 59.4M 2s 122150K .......... .......... .......... .......... .......... 46% 78.0M 2s 122200K .......... .......... .......... .......... .......... 46% 62.4M 2s 122250K .......... .......... .......... .......... .......... 46% 54.4M 2s 122300K .......... .......... .......... .......... .......... 46% 126M 2s 122350K .......... .......... .......... .......... .......... 46% 62.9M 2s 122400K .......... .......... .......... .......... .......... 46% 63.0M 2s 122450K .......... .......... .......... .......... .......... 46% 62.9M 2s 122500K .......... .......... .......... .......... .......... 46% 64.4M 2s 122550K .......... .......... .......... .......... .......... 46% 73.9M 2s 122600K .......... .......... .......... .......... .......... 46% 58.6M 2s 122650K .......... .......... .......... .......... .......... 46% 101M 2s 122700K .......... .......... .......... .......... .......... 46% 63.2M 2s 122750K .......... .......... .......... .......... .......... 46% 63.2M 2s 122800K .......... .......... .......... .......... .......... 46% 96.1M 2s 122850K .......... .......... .......... .......... .......... 46% 24.5M 2s 122900K .......... .......... .......... .......... .......... 46% 58.4M 2s 122950K .......... .......... .......... .......... .......... 46% 122M 2s 123000K .......... .......... .......... .......... .......... 46% 66.3M 2s 123050K .......... .......... .......... .......... .......... 46% 63.2M 2s 123100K .......... .......... .......... .......... .......... 46% 123M 2s 123150K .......... .......... .......... .......... .......... 46% 77.1M 2s 123200K .......... .......... .......... .......... .......... 47% 94.1M 2s 123250K .......... .......... .......... .......... .......... 47% 122M 2s 123300K .......... .......... .......... .......... .......... 47% 95.2M 2s 123350K .......... .......... .......... .......... .......... 47% 92.7M 2s 123400K .......... .......... .......... .......... .......... 47% 125M 2s 123450K .......... .......... .......... .......... .......... 47% 93.7M 2s 123500K .......... .......... .......... .......... .......... 47% 21.1M 2s 123550K .......... .......... .......... .......... .......... 47% 493M 2s 123600K .......... .......... .......... .......... .......... 47% 351M 2s 123650K .......... .......... .......... .......... .......... 47% 514M 2s 123700K .......... .......... .......... .......... .......... 47% 391M 2s 123750K .......... .......... .......... .......... .......... 47% 38.2M 2s 123800K .......... .......... .......... .......... .......... 47% 498M 2s 123850K .......... .......... .......... .......... .......... 47% 116M 2s 123900K .......... .......... .......... .......... .......... 47% 267M 2s 123950K .......... .......... .......... .......... .......... 47% 444M 2s 124000K .......... .......... .......... .......... .......... 47% 40.1M 2s 124050K .......... .......... .......... .......... .......... 47% 161M 2s 124100K .......... .......... .......... .......... .......... 47% 142M 2s 124150K .......... .......... .......... .......... .......... 47% 173M 2s 124200K .......... .......... .......... .......... .......... 47% 174M 2s 124250K .......... .......... .......... .......... .......... 47% 93.5M 2s 124300K .......... .......... .......... .......... .......... 47% 96.7M 2s 124350K .......... .......... .......... .......... .......... 47% 64.2M 2s 124400K .......... .......... .......... .......... .......... 47% 93.2M 2s 124450K .......... .......... .......... .......... .......... 47% 72.2M 2s 124500K .......... .......... .......... .......... .......... 47% 96.3M 2s 124550K .......... .......... .......... .......... .......... 47% 76.7M 2s 124600K .......... .......... .......... .......... .......... 47% 64.2M 2s 124650K .......... .......... .......... .......... .......... 47% 91.1M 2s 124700K .......... .......... .......... .......... .......... 47% 63.8M 2s 124750K .......... .......... .......... .......... .......... 47% 126M 2s 124800K .......... .......... .......... .......... .......... 47% 72.0M 2s 124850K .......... .......... .......... .......... .......... 47% 64.7M 2s 124900K .......... .......... .......... .......... .......... 47% 117M 2s 124950K .......... .......... .......... .......... .......... 47% 70.6M 2s 125000K .......... .......... .......... .......... .......... 47% 98.2M 2s 125050K .......... .......... .......... .......... .......... 47% 77.8M 2s 125100K .......... .......... .......... .......... .......... 47% 40.9M 2s 125150K .......... .......... .......... .......... .......... 47% 126M 2s 125200K .......... .......... .......... .......... .......... 47% 62.9M 2s 125250K .......... .......... .......... .......... .......... 47% 91.8M 2s 125300K .......... .......... .......... .......... .......... 47% 93.2M 2s 125350K .......... .......... .......... .......... .......... 47% 75.1M 2s 125400K .......... .......... .......... .......... .......... 47% 75.6M 2s 125450K .......... .......... .......... .......... .......... 47% 78.8M 2s 125500K .......... .......... .......... .......... .......... 47% 98.0M 2s 125550K .......... .......... .......... .......... .......... 47% 77.0M 2s 125600K .......... .......... .......... .......... .......... 47% 93.7M 2s 125650K .......... .......... .......... .......... .......... 47% 75.9M 2s 125700K .......... .......... .......... .......... .......... 47% 72.9M 2s 125750K .......... .......... .......... .......... .......... 47% 78.3M 2s 125800K .......... .......... .......... .......... .......... 47% 74.8M 2s 125850K .......... .......... .......... .......... .......... 48% 94.6M 2s 125900K .......... .......... .......... .......... .......... 48% 76.3M 2s 125950K .......... .......... .......... .......... .......... 48% 75.1M 2s 126000K .......... .......... .......... .......... .......... 48% 74.1M 2s 126050K .......... .......... .......... .......... .......... 48% 97.3M 2s 126100K .......... .......... .......... .......... .......... 48% 75.2M 2s 126150K .......... .......... .......... .......... .......... 48% 75.1M 2s 126200K .......... .......... .......... .......... .......... 48% 74.5M 2s 126250K .......... .......... .......... .......... .......... 48% 90.8M 2s 126300K .......... .......... .......... .......... .......... 48% 76.1M 2s 126350K .......... .......... .......... .......... .......... 48% 64.9M 2s 126400K .......... .......... .......... .......... .......... 48% 117M 2s 126450K .......... .......... .......... .......... .......... 48% 75.6M 2s 126500K .......... .......... .......... .......... .......... 48% 76.8M 2s 126550K .......... .......... .......... .......... .......... 48% 94.3M 2s 126600K .......... .......... .......... .......... .......... 48% 73.6M 2s 126650K .......... .......... .......... .......... .......... 48% 77.1M 2s 126700K .......... .......... .......... .......... .......... 48% 71.6M 2s 126750K .......... .......... .......... .......... .......... 48% 79.4M 2s 126800K .......... .......... .......... .......... .......... 48% 92.3M 2s 126850K .......... .......... .......... .......... .......... 48% 76.1M 2s 126900K .......... .......... .......... .......... .......... 48% 75.1M 2s 126950K .......... .......... .......... .......... .......... 48% 121M 2s 127000K .......... .......... .......... .......... .......... 48% 98.4M 2s 127050K .......... .......... .......... .......... .......... 48% 121M 2s 127100K .......... .......... .......... .......... .......... 48% 98.4M 2s 127150K .......... .......... .......... .......... .......... 48% 115M 2s 127200K .......... .......... .......... .......... .......... 48% 96.3M 2s 127250K .......... .......... .......... .......... .......... 48% 98.2M 2s 127300K .......... .......... .......... .......... .......... 48% 122M 2s 127350K .......... .......... .......... .......... .......... 48% 24.1M 2s 127400K .......... .......... .......... .......... .......... 48% 465M 2s 127450K .......... .......... .......... .......... .......... 48% 425M 2s 127500K .......... .......... .......... .......... .......... 48% 514M 2s 127550K .......... .......... .......... .......... .......... 48% 525M 2s 127600K .......... .......... .......... .......... .......... 48% 33.6M 2s 127650K .......... .......... .......... .......... .......... 48% 239M 2s 127700K .......... .......... .......... .......... .......... 48% 461M 2s 127750K .......... .......... .......... .......... .......... 48% 561M 2s 127800K .......... .......... .......... .......... .......... 48% 118M 2s 127850K .......... .......... .......... .......... .......... 48% 77.8M 2s 127900K .......... .......... .......... .......... .......... 48% 71.2M 2s 127950K .......... .......... .......... .......... .......... 48% 102M 2s 128000K .......... .......... .......... .......... .......... 48% 93.2M 2s 128050K .......... .......... .......... .......... .......... 48% 119M 2s 128100K .......... .......... .......... .......... .......... 48% 61.1M 2s 128150K .......... .......... .......... .......... .......... 48% 78.9M 2s 128200K .......... .......... .......... .......... .......... 48% 92.8M 2s 128250K .......... .......... .......... .......... .......... 48% 91.6M 2s 128300K .......... .......... .......... .......... .......... 48% 94.6M 2s 128350K .......... .......... .......... .......... .......... 48% 61.2M 2s 128400K .......... .......... .......... .......... .......... 48% 94.1M 2s 128450K .......... .......... .......... .......... .......... 49% 82.6M 2s 128500K .......... .......... .......... .......... .......... 49% 94.8M 2s 128550K .......... .......... .......... .......... .......... 49% 92.3M 2s 128600K .......... .......... .......... .......... .......... 49% 76.9M 2s 128650K .......... .......... .......... .......... .......... 49% 125M 2s 128700K .......... .......... .......... .......... .......... 49% 63.2M 2s 128750K .......... .......... .......... .......... .......... 49% 91.1M 2s 128800K .......... .......... .......... .......... .......... 49% 77.5M 2s 128850K .......... .......... .......... .......... .......... 49% 73.4M 2s 128900K .......... .......... .......... .......... .......... 49% 97.9M 2s 128950K .......... .......... .......... .......... .......... 49% 73.6M 2s 129000K .......... .......... .......... .......... .......... 49% 77.5M 2s 129050K .......... .......... .......... .......... .......... 49% 76.1M 2s 129100K .......... .......... .......... .......... .......... 49% 75.6M 2s 129150K .......... .......... .......... .......... .......... 49% 119M 2s 129200K .......... .......... .......... .......... .......... 49% 64.2M 2s 129250K .......... .......... .......... .......... .......... 49% 75.5M 2s 129300K .......... .......... .......... .......... .......... 49% 91.3M 2s 129350K .......... .......... .......... .......... .......... 49% 64.4M 2s 129400K .......... .......... .......... .......... .......... 49% 126M 2s 129450K .......... .......... .......... .......... .......... 49% 73.5M 2s 129500K .......... .......... .......... .......... .......... 49% 88.1M 2s 129550K .......... .......... .......... .......... .......... 49% 80.7M 2s 129600K .......... .......... .......... .......... .......... 49% 88.0M 2s 129650K .......... .......... .......... .......... .......... 49% 78.5M 2s 129700K .......... .......... .......... .......... .......... 49% 75.7M 2s 129750K .......... .......... .......... .......... .......... 49% 90.4M 2s 129800K .......... .......... .......... .......... .......... 49% 77.8M 2s 129850K .......... .......... .......... .......... .......... 49% 93.9M 2s 129900K .......... .......... .......... .......... .......... 49% 75.9M 2s 129950K .......... .......... .......... .......... .......... 49% 75.9M 2s 130000K .......... .......... .......... .......... .......... 49% 74.1M 2s 130050K .......... .......... .......... .......... .......... 49% 120M 2s 130100K .......... .......... .......... .......... .......... 49% 64.9M 2s 130150K .......... .......... .......... .......... .......... 49% 92.1M 2s 130200K .......... .......... .......... .......... .......... 49% 63.8M 2s 130250K .......... .......... .......... .......... .......... 49% 76.5M 2s 130300K .......... .......... .......... .......... .......... 49% 124M 2s 130350K .......... .......... .......... .......... .......... 49% 74.4M 2s 130400K .......... .......... .......... .......... .......... 49% 75.7M 2s 130450K .......... .......... .......... .......... .......... 49% 63.6M 2s 130500K .......... .......... .......... .......... .......... 49% 96.9M 2s 130550K .......... .......... .......... .......... .......... 49% 92.0M 2s 130600K .......... .......... .......... .......... .......... 49% 59.3M 2s 130650K .......... .......... .......... .......... .......... 49% 112M 2s 130700K .......... .......... .......... .......... .......... 49% 46.9M 2s 130750K .......... .......... .......... .......... .......... 49% 159M 2s 130800K .......... .......... .......... .......... .......... 49% 63.2M 2s 130850K .......... .......... .......... .......... .......... 49% 90.6M 2s 130900K .......... .......... .......... .......... .......... 49% 128M 2s 130950K .......... .......... .......... .......... .......... 49% 97.1M 2s 131000K .......... .......... .......... .......... .......... 49% 117M 2s 131050K .......... .......... .......... .......... .......... 49% 55.5M 2s 131100K .......... .......... .......... .......... .......... 50% 163M 2s 131150K .......... .......... .......... .......... .......... 50% 35.7M 2s 131200K .......... .......... .......... .......... .......... 50% 148M 2s 131250K .......... .......... .......... .......... .......... 50% 19.6M 2s 131300K .......... .......... .......... .......... .......... 50% 184M 2s 131350K .......... .......... .......... .......... .......... 50% 161M 2s 131400K .......... .......... .......... .......... .......... 50% 189M 2s 131450K .......... .......... .......... .......... .......... 50% 31.4M 2s 131500K .......... .......... .......... .......... .......... 50% 187M 2s 131550K .......... .......... .......... .......... .......... 50% 57.0M 2s 131600K .......... .......... .......... .......... .......... 50% 47.5M 2s 131650K .......... .......... .......... .......... .......... 50% 470M 2s 131700K .......... .......... .......... .......... .......... 50% 474M 2s 131750K .......... .......... .......... .......... .......... 50% 102M 2s 131800K .......... .......... .......... .......... .......... 50% 69.8M 2s 131850K .......... .......... .......... .......... .......... 50% 151M 2s 131900K .......... .......... .......... .......... .......... 50% 136M 2s 131950K .......... .......... .......... .......... .......... 50% 79.8M 2s 132000K .......... .......... .......... .......... .......... 50% 86.6M 2s 132050K .......... .......... .......... .......... .......... 50% 109M 2s 132100K .......... .......... .......... .......... .......... 50% 80.7M 2s 132150K .......... .......... .......... .......... .......... 50% 194M 2s 132200K .......... .......... .......... .......... .......... 50% 103M 2s 132250K .......... .......... .......... .......... .......... 50% 80.2M 2s 132300K .......... .......... .......... .......... .......... 50% 108M 2s 132350K .......... .......... .......... .......... .......... 50% 119M 2s 132400K .......... .......... .......... .......... .......... 50% 82.5M 2s 132450K .......... .......... .......... .......... .......... 50% 86.3M 2s 132500K .......... .......... .......... .......... .......... 50% 138M 2s 132550K .......... .......... .......... .......... .......... 50% 126M 2s 132600K .......... .......... .......... .......... .......... 50% 97.7M 2s 132650K .......... .......... .......... .......... .......... 50% 116M 2s 132700K .......... .......... .......... .......... .......... 50% 116M 2s 132750K .......... .......... .......... .......... .......... 50% 22.9M 2s 132800K .......... .......... .......... .......... .......... 50% 452M 2s 132850K .......... .......... .......... .......... .......... 50% 417M 2s 132900K .......... .......... .......... .......... .......... 50% 28.2M 2s 132950K .......... .......... .......... .......... .......... 50% 124M 2s 133000K .......... .......... .......... .......... .......... 50% 180M 2s 133050K .......... .......... .......... .......... .......... 50% 196M 2s 133100K .......... .......... .......... .......... .......... 50% 16.5M 2s 133150K .......... .......... .......... .......... .......... 50% 474M 2s 133200K .......... .......... .......... .......... .......... 50% 421M 2s 133250K .......... .......... .......... .......... .......... 50% 525M 2s 133300K .......... .......... .......... .......... .......... 50% 38.1M 2s 133350K .......... .......... .......... .......... .......... 50% 140M 2s 133400K .......... .......... .......... .......... .......... 50% 141M 2s 133450K .......... .......... .......... .......... .......... 50% 64.7M 2s 133500K .......... .......... .......... .......... .......... 50% 191M 2s 133550K .......... .......... .......... .......... .......... 50% 101M 2s 133600K .......... .......... .......... .......... .......... 50% 78.3M 2s 133650K .......... .......... .......... .......... .......... 50% 176M 2s 133700K .......... .......... .......... .......... .......... 51% 109M 2s 133750K .......... .......... .......... .......... .......... 51% 88.1M 2s 133800K .......... .......... .......... .......... .......... 51% 182M 2s 133850K .......... .......... .......... .......... .......... 51% 107M 2s 133900K .......... .......... .......... .......... .......... 51% 104M 2s 133950K .......... .......... .......... .......... .......... 51% 97.1M 2s 134000K .......... .......... .......... .......... .......... 51% 105M 2s 134050K .......... .......... .......... .......... .......... 51% 84.3M 2s 134100K .......... .......... .......... .......... .......... 51% 164M 2s 134150K .......... .......... .......... .......... .......... 51% 19.5M 2s 134200K .......... .......... .......... .......... .......... 51% 388M 2s 134250K .......... .......... .......... .......... .......... 51% 525M 2s 134300K .......... .......... .......... .......... .......... 51% 519M 2s 134350K .......... .......... .......... .......... .......... 51% 41.6M 2s 134400K .......... .......... .......... .......... .......... 51% 18.5M 2s 134450K .......... .......... .......... .......... .......... 51% 46.2M 2s 134500K .......... .......... .......... .......... .......... 51% 341M 2s 134550K .......... .......... .......... .......... .......... 51% 483M 2s 134600K .......... .......... .......... .......... .......... 51% 39.2M 2s 134650K .......... .......... .......... .......... .......... 51% 128M 2s 134700K .......... .......... .......... .......... .......... 51% 101M 2s 134750K .......... .......... .......... .......... .......... 51% 103M 2s 134800K .......... .......... .......... .......... .......... 51% 132M 2s 134850K .......... .......... 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.......... 51% 549M 2s 136200K .......... .......... .......... .......... .......... 51% 493M 2s 136250K .......... .......... .......... .......... .......... 51% 46.9M 2s 136300K .......... .......... .......... .......... .......... 52% 162M 2s 136350K .......... .......... .......... .......... .......... 52% 82.1M 2s 136400K .......... .......... .......... .......... .......... 52% 184M 2s 136450K .......... .......... .......... .......... .......... 52% 86.9M 2s 136500K .......... .......... .......... .......... .......... 52% 25.8M 2s 136550K .......... .......... .......... .......... .......... 52% 509M 2s 136600K .......... .......... .......... .......... .......... 52% 38.9M 2s 136650K .......... .......... .......... .......... .......... 52% 189M 2s 136700K .......... .......... .......... .......... .......... 52% 41.6M 2s 136750K .......... .......... .......... .......... .......... 52% 184M 2s 136800K .......... .......... .......... .......... .......... 52% 191M 2s 136850K .......... .......... .......... .......... .......... 52% 27.8M 2s 136900K .......... .......... .......... .......... .......... 52% 498M 2s 136950K .......... .......... .......... .......... .......... 52% 483M 2s 137000K .......... .......... .......... .......... .......... 52% 201M 2s 137050K .......... .......... .......... .......... .......... 52% 70.6M 2s 137100K .......... .......... .......... .......... .......... 52% 80.0M 2s 137150K .......... .......... .......... .......... .......... 52% 116M 2s 137200K .......... .......... .......... .......... .......... 52% 115M 2s 137250K .......... .......... .......... .......... .......... 52% 113M 2s 137300K .......... .......... .......... .......... .......... 52% 113M 2s 137350K .......... .......... .......... .......... .......... 52% 16.7M 2s 137400K .......... .......... .......... .......... .......... 52% 388M 2s 137450K .......... .......... .......... .......... .......... 52% 432M 2s 137500K .......... 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.......... 52% 139M 2s 138850K .......... .......... .......... .......... .......... 52% 92.1M 2s 138900K .......... .......... .......... .......... .......... 52% 81.2M 2s 138950K .......... .......... .......... .......... .......... 53% 101M 2s 139000K .......... .......... .......... .......... .......... 53% 189M 2s 139050K .......... .......... .......... .......... .......... 53% 137M 2s 139100K .......... .......... .......... .......... .......... 53% 17.8M 2s 139150K .......... .......... .......... .......... .......... 53% 202M 2s 139200K .......... .......... .......... .......... .......... 53% 184M 2s 139250K .......... .......... .......... .......... .......... 53% 14.9M 2s 139300K .......... .......... .......... .......... .......... 53% 440M 2s 139350K .......... .......... .......... .......... .......... 53% 452M 2s 139400K .......... .......... .......... .......... .......... 53% 29.8M 2s 139450K .......... .......... .......... .......... .......... 53% 117M 2s 139500K .......... .......... .......... .......... .......... 53% 199M 2s 139550K .......... .......... .......... .......... .......... 53% 417M 2s 139600K .......... .......... .......... .......... .......... 53% 32.0M 2s 139650K .......... .......... .......... .......... .......... 53% 190M 2s 139700K .......... .......... .......... .......... .......... 53% 164M 2s 139750K .......... .......... .......... .......... .......... 53% 46.3M 2s 139800K .......... .......... .......... .......... .......... 53% 167M 2s 139850K .......... .......... .......... .......... .......... 53% 108M 2s 139900K .......... .......... .......... .......... .......... 53% 192M 2s 139950K .......... .......... .......... .......... .......... 53% 69.5M 2s 140000K .......... .......... .......... .......... .......... 53% 184M 2s 140050K .......... .......... .......... .......... .......... 53% 147M 2s 140100K .......... .......... .......... .......... .......... 53% 86.7M 2s 140150K .......... 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.......... .......... 53% 63.7M 2s 141500K .......... .......... .......... .......... .......... 53% 95.0M 2s 141550K .......... .......... .......... .......... .......... 54% 75.0M 2s 141600K .......... .......... .......... .......... .......... 54% 76.1M 2s 141650K .......... .......... .......... .......... .......... 54% 122M 2s 141700K .......... .......... .......... .......... .......... 54% 64.2M 2s 141750K .......... .......... .......... .......... .......... 54% 92.7M 2s 141800K .......... .......... .......... .......... .......... 54% 95.2M 2s 141850K .......... .......... .......... .......... .......... 54% 55.4M 2s 141900K .......... .......... .......... .......... .......... 54% 126M 2s 141950K .......... .......... .......... .......... .......... 54% 75.2M 2s 142000K .......... .......... .......... .......... .......... 54% 54.2M 2s 142050K .......... .......... .......... .......... .......... 54% 130M 2s 142100K .......... .......... .......... .......... .......... 54% 75.8M 2s 142150K .......... .......... .......... .......... .......... 54% 94.1M 2s 142200K .......... .......... .......... .......... .......... 54% 75.9M 2s 142250K .......... .......... .......... .......... .......... 54% 121M 2s 142300K .......... .......... .......... .......... .......... 54% 77.6M 2s 142350K .......... .......... .......... .......... .......... 54% 92.3M 2s 142400K .......... .......... .......... .......... .......... 54% 77.8M 2s 142450K .......... .......... .......... .......... .......... 54% 31.8M 2s 142500K .......... .......... .......... .......... .......... 54% 465M 2s 142550K .......... .......... .......... .......... .......... 54% 41.7M 2s 142600K .......... .......... .......... .......... .......... 54% 133M 2s 142650K .......... .......... .......... .......... .......... 54% 45.0M 2s 142700K .......... .......... .......... .......... .......... 54% 93.0M 2s 142750K .......... .......... .......... .......... .......... 54% 70.7M 2s 142800K .......... .......... .......... .......... .......... 54% 127M 2s 142850K .......... .......... .......... .......... .......... 54% 74.5M 2s 142900K .......... .......... .......... .......... .......... 54% 102M 2s 142950K .......... .......... .......... .......... .......... 54% 75.2M 2s 143000K .......... .......... .......... .......... .......... 54% 75.5M 2s 143050K .......... .......... .......... .......... .......... 54% 110M 2s 143100K .......... .......... .......... .......... .......... 54% 57.2M 2s 143150K .......... .......... .......... .......... .......... 54% 121M 2s 143200K .......... .......... .......... .......... .......... 54% 64.5M 2s 143250K .......... .......... .......... .......... .......... 54% 94.3M 2s 143300K .......... .......... .......... .......... .......... 54% 90.4M 2s 143350K .......... .......... .......... .......... .......... 54% 77.6M 2s 143400K .......... .......... .......... .......... .......... 54% 92.0M 2s 143450K .......... .......... .......... .......... .......... 54% 78.3M 2s 143500K .......... .......... .......... .......... .......... 54% 89.9M 2s 143550K .......... .......... .......... .......... .......... 54% 135M 2s 143600K .......... .......... .......... .......... .......... 54% 73.4M 2s 143650K .......... .......... .......... .......... .......... 54% 95.2M 2s 143700K .......... .......... .......... .......... .......... 54% 64.8M 2s 143750K .......... .......... .......... .......... .......... 54% 121M 2s 143800K .......... .......... .......... .......... .......... 54% 94.4M 2s 143850K .......... .......... .......... .......... .......... 54% 63.1M 2s 143900K .......... .......... .......... .......... .......... 54% 95.2M 2s 143950K .......... .......... .......... .......... .......... 54% 76.1M 2s 144000K .......... .......... .......... .......... .......... 54% 125M 2s 144050K .......... .......... .......... .......... .......... 54% 91.8M 2s 144100K .......... .......... .......... .......... .......... 54% 78.5M 2s 144150K .......... .......... .......... .......... .......... 54% 76.5M 2s 144200K .......... .......... .......... .......... .......... 55% 91.3M 2s 144250K .......... .......... .......... .......... .......... 55% 126M 2s 144300K .......... .......... .......... .......... .......... 55% 71.4M 2s 144350K .......... .......... .......... .......... .......... 55% 101M 2s 144400K .......... .......... .......... .......... .......... 55% 122M 2s 144450K .......... .......... .......... .......... .......... 55% 78.1M 2s 144500K .......... .......... .......... .......... .......... 55% 121M 2s 144550K .......... .......... .......... .......... .......... 55% 98.0M 2s 144600K .......... .......... .......... .......... .......... 55% 30.6M 2s 144650K .......... .......... .......... .......... .......... 55% 188M 2s 144700K .......... .......... .......... .......... .......... 55% 364M 2s 144750K .......... .......... .......... .......... .......... 55% 47.8M 2s 144800K .......... .......... .......... .......... .......... 55% 185M 2s 144850K .......... .......... .......... .......... .......... 55% 170M 2s 144900K .......... .......... .......... .......... .......... 55% 493M 2s 144950K .......... .......... .......... .......... .......... 55% 206M 2s 145000K .......... .......... .......... .......... .......... 55% 120M 2s 145050K .......... .......... .......... .......... .......... 55% 94.6M 2s 145100K .......... .......... .......... .......... .......... 55% 64.5M 2s 145150K .......... .......... .......... .......... .......... 55% 121M 2s 145200K .......... .......... .......... .......... .......... 55% 75.4M 2s 145250K .......... .......... .......... .......... .......... 55% 75.4M 2s 145300K .......... .......... .......... .......... .......... 55% 76.3M 2s 145350K .......... .......... .......... .......... .......... 55% 75.8M 1s 145400K .......... .......... .......... .......... .......... 55% 95.9M 1s 145450K .......... .......... .......... .......... .......... 55% 74.7M 1s 145500K .......... .......... .......... .......... .......... 55% 75.6M 1s 145550K .......... .......... .......... .......... .......... 55% 76.5M 1s 145600K .......... .......... .......... .......... .......... 55% 72.6M 1s 145650K .......... .......... .......... .......... .......... 55% 101M 1s 145700K .......... .......... .......... .......... .......... 55% 60.4M 1s 145750K .......... .......... .......... .......... .......... 55% 119M 1s 145800K .......... .......... .......... .......... .......... 55% 93.7M 1s 145850K .......... .......... .......... .......... .......... 55% 64.2M 1s 145900K .......... .......... .......... .......... .......... 55% 92.5M 1s 145950K .......... .......... .......... .......... .......... 55% 73.3M 1s 146000K .......... .......... .......... .......... .......... 55% 93.5M 1s 146050K .......... .......... .......... .......... .......... 55% 76.8M 1s 146100K .......... .......... .......... .......... .......... 55% 73.1M 1s 146150K .......... .......... .......... .......... .......... 55% 98.6M 1s 146200K .......... .......... .......... .......... .......... 55% 95.2M 1s 146250K .......... .......... .......... .......... .......... 55% 87.7M 1s 146300K .......... .......... .......... .......... .......... 55% 66.0M 1s 146350K .......... .......... .......... .......... .......... 55% 87.3M 1s 146400K .......... .......... .......... .......... .......... 55% 104M 1s 146450K .......... .......... .......... .......... .......... 55% 75.9M 1s 146500K .......... .......... .......... .......... .......... 55% 93.4M 1s 146550K .......... .......... .......... .......... .......... 55% 121M 1s 146600K .......... .......... .......... .......... .......... 55% 55.0M 1s 146650K .......... .......... .......... .......... .......... 55% 174M 1s 146700K .......... .......... .......... .......... .......... 55% 64.8M 1s 146750K .......... .......... .......... .......... .......... 55% 93.5M 1s 146800K .......... .......... .......... .......... .......... 56% 124M 1s 146850K .......... .......... .......... .......... .......... 56% 73.9M 1s 146900K .......... .......... .......... .......... .......... 56% 94.8M 1s 146950K .......... .......... .......... .......... .......... 56% 77.8M 1s 147000K .......... .......... .......... .......... .......... 56% 75.0M 1s 147050K .......... .......... .......... .......... .......... 56% 105M 1s 147100K .......... .......... .......... .......... .......... 56% 105M 1s 147150K .......... .......... .......... .......... .......... 56% 72.0M 1s 147200K .......... .......... .......... .......... .......... 56% 78.8M 1s 147250K .......... .......... .......... .......... .......... 56% 92.3M 1s 147300K .......... .......... .......... .......... .......... 56% 100M 1s 147350K .......... .......... .......... .......... .......... 56% 73.2M 1s 147400K .......... .......... .......... .......... .......... 56% 80.4M 1s 147450K .......... .......... .......... .......... .......... 56% 61.2M 1s 147500K .......... .......... .......... .......... .......... 56% 60.2M 1s 147550K .......... .......... .......... .......... .......... 56% 135M 1s 147600K .......... .......... .......... .......... .......... 56% 54.0M 1s 147650K .......... .......... .......... .......... .......... 56% 125M 1s 147700K .......... .......... .......... .......... .......... 56% 92.8M 1s 147750K .......... .......... .......... .......... .......... 56% 94.4M 1s 147800K .......... .......... .......... .......... .......... 56% 121M 1s 147850K .......... .......... .......... .......... .......... 56% 78.3M 1s 147900K .......... .......... .......... .......... .......... 56% 126M 1s 147950K .......... .......... .......... .......... .......... 56% 94.6M 1s 148000K .......... .......... .......... .......... .......... 56% 121M 1s 148050K .......... 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73.8M 1s 150700K .......... .......... .......... .......... .......... 57% 97.3M 1s 150750K .......... .......... .......... .......... .......... 57% 77.5M 1s 150800K .......... .......... .......... .......... .......... 57% 120M 1s 150850K .......... .......... .......... .......... .......... 57% 75.4M 1s 150900K .......... .......... .......... .......... .......... 57% 123M 1s 150950K .......... .......... .......... .......... .......... 57% 65.5M 1s 151000K .......... .......... .......... .......... .......... 57% 121M 1s 151050K .......... .......... .......... .......... .......... 57% 76.9M 1s 151100K .......... .......... .......... .......... .......... 57% 123M 1s 151150K .......... .......... .......... .......... .......... 57% 77.0M 1s 151200K .......... .......... .......... .......... .......... 57% 93.2M 1s 151250K .......... .......... .......... .......... .......... 57% 94.4M 1s 151300K .......... .......... .......... .......... .......... 57% 126M 1s 151350K 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1s 157950K .......... .......... .......... .......... .......... 60% 132M 1s 158000K .......... .......... .......... .......... .......... 60% 186M 1s 158050K .......... .......... .......... .......... .......... 60% 191M 1s 158100K .......... .......... .......... .......... .......... 60% 36.6M 1s 158150K .......... .......... .......... .......... .......... 60% 183M 1s 158200K .......... .......... .......... .......... .......... 60% 128M 1s 158250K .......... .......... .......... .......... .......... 60% 93.2M 1s 158300K .......... .......... .......... .......... .......... 60% 126M 1s 158350K .......... .......... .......... .......... .......... 60% 95.2M 1s 158400K .......... .......... .......... .......... .......... 60% 129M 1s 158450K .......... .......... .......... .......... .......... 60% 80.7M 1s 158500K .......... .......... .......... .......... .......... 60% 107M 1s 158550K .......... .......... .......... .......... .......... 60% 109M 1s 158600K .......... 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.......... .......... 65% 92.8M 1s 171150K .......... .......... .......... .......... .......... 65% 86.7M 1s 171200K .......... .......... .......... .......... .......... 65% 44.3M 1s 171250K .......... .......... .......... .......... .......... 65% 46.0M 1s 171300K .......... .......... .......... .......... .......... 65% 125M 1s 171350K .......... .......... .......... .......... .......... 65% 95.7M 1s 171400K .......... .......... .......... .......... .......... 65% 93.5M 1s 171450K .......... .......... .......... .......... .......... 65% 95.9M 1s 171500K .......... .......... .......... .......... .......... 65% 18.9M 1s 171550K .......... .......... .......... .......... .......... 65% 301M 1s 171600K .......... .......... .......... .......... .......... 65% 364M 1s 171650K .......... .......... .......... .......... .......... 65% 407M 1s 171700K .......... .......... .......... .......... .......... 65% 407M 1s 171750K .......... .......... .......... .......... .......... 65% 94.3M 1s 171800K .......... .......... .......... .......... .......... 65% 150M 1s 171850K .......... .......... .......... .......... .......... 65% 84.0M 1s 171900K .......... .......... .......... .......... .......... 65% 531M 1s 171950K .......... .......... .......... .......... .......... 65% 78.5M 1s 172000K .......... .......... .......... .......... .......... 65% 28.7M 1s 172050K .......... .......... .......... .......... .......... 65% 428M 1s 172100K .......... .......... .......... .......... .......... 65% 55.1M 1s 172150K .......... .......... .......... .......... .......... 65% 63.3M 1s 172200K .......... .......... .......... .......... .......... 65% 47.5M 1s 172250K .......... .......... .......... .......... .......... 65% 176M 1s 172300K .......... .......... .......... .......... .......... 65% 53.9M 1s 172350K .......... .......... .......... .......... .......... 65% 56.1M 1s 172400K .......... .......... .......... .......... .......... 65% 62.2M 1s 172450K .......... .......... .......... .......... .......... 65% 63.4M 1s 172500K .......... .......... .......... .......... .......... 65% 77.6M 1s 172550K .......... .......... .......... .......... .......... 65% 63.0M 1s 172600K .......... .......... .......... .......... .......... 65% 62.3M 1s 172650K .......... .......... .......... .......... .......... 65% 25.2M 1s 172700K .......... .......... .......... .......... .......... 65% 42.6M 1s 172750K .......... .......... .......... .......... .......... 65% 60.4M 1s 172800K .......... .......... .......... .......... .......... 65% 65.5M 1s 172850K .......... .......... .......... .......... .......... 65% 36.8M 1s 172900K .......... .......... .......... .......... .......... 65% 214M 1s 172950K .......... .......... .......... .......... .......... 65% 54.9M 1s 173000K .......... .......... .......... .......... .......... 65% 53.8M 1s 173050K .......... .......... .......... .......... .......... 66% 63.7M 1s 173100K .......... .......... .......... .......... .......... 66% 54.3M 1s 173150K .......... .......... .......... .......... .......... 66% 75.0M 1s 173200K .......... .......... .......... .......... .......... 66% 47.0M 1s 173250K .......... .......... .......... .......... .......... 66% 52.8M 1s 173300K .......... .......... .......... .......... .......... 66% 64.7M 1s 173350K .......... .......... .......... .......... .......... 66% 74.4M 1s 173400K .......... .......... .......... .......... .......... 66% 61.4M 1s 173450K .......... .......... .......... .......... .......... 66% 64.6M 1s 173500K .......... .......... .......... .......... .......... 66% 54.5M 1s 173550K .......... .......... .......... .......... .......... 66% 75.6M 1s 173600K .......... .......... .......... .......... .......... 66% 61.5M 1s 173650K .......... .......... .......... .......... .......... 66% 55.3M 1s 173700K .......... .......... .......... .......... .......... 66% 63.7M 1s 173750K 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67% 56.4M 1s 176400K .......... .......... .......... .......... .......... 67% 63.2M 1s 176450K .......... .......... .......... .......... .......... 67% 48.0M 1s 176500K .......... .......... .......... .......... .......... 67% 121M 1s 176550K .......... .......... .......... .......... .......... 67% 62.8M 1s 176600K .......... .......... .......... .......... .......... 67% 55.8M 1s 176650K .......... .......... .......... .......... .......... 67% 62.0M 1s 176700K .......... .......... .......... .......... .......... 67% 62.8M 1s 176750K .......... .......... .......... .......... .......... 67% 54.7M 1s 176800K .......... .......... .......... .......... .......... 67% 65.4M 1s 176850K .......... .......... .......... .......... .......... 67% 46.3M 1s 176900K .......... .......... .......... .......... .......... 67% 62.8M 1s 176950K .......... .......... .......... .......... .......... 67% 62.4M 1s 177000K .......... .......... .......... .......... .......... 67% 82.6M 1s 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1s 183650K .......... .......... .......... .......... .......... 70% 189M 1s 183700K .......... .......... .......... .......... .......... 70% 15.5M 1s 183750K .......... .......... .......... .......... .......... 70% 175M 1s 183800K .......... .......... .......... .......... .......... 70% 186M 1s 183850K .......... .......... .......... .......... .......... 70% 161M 1s 183900K .......... .......... .......... .......... .......... 70% 36.4M 1s 183950K .......... .......... .......... .......... .......... 70% 133M 1s 184000K .......... .......... .......... .......... .......... 70% 116M 1s 184050K .......... .......... .......... .......... .......... 70% 124M 1s 184100K .......... .......... .......... .......... .......... 70% 102M 1s 184150K .......... .......... .......... .......... .......... 70% 91.4M 1s 184200K .......... .......... .......... .......... .......... 70% 128M 1s 184250K .......... .......... .......... .......... .......... 70% 96.3M 1s 184300K .......... 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.......... .......... 70% 164M 1s 185000K .......... .......... .......... .......... .......... 70% 195M 1s 185050K .......... .......... .......... .......... .......... 70% 194M 1s 185100K .......... .......... .......... .......... .......... 70% 76.8M 1s 185150K .......... .......... .......... .......... .......... 70% 88.6M 1s 185200K .......... .......... .......... .......... .......... 70% 54.5M 1s 185250K .......... .......... .......... .......... .......... 70% 531M 1s 185300K .......... .......... .......... .......... .......... 70% 18.8M 1s 185350K .......... .......... .......... .......... .......... 70% 159M 1s 185400K .......... .......... .......... .......... .......... 70% 36.1M 1s 185450K .......... .......... .......... .......... .......... 70% 130M 1s 185500K .......... .......... .......... .......... .......... 70% 104M 1s 185550K .......... .......... .......... .......... .......... 70% 142M 1s 185600K .......... .......... .......... .......... .......... 70% 71.6M 1s 185650K .......... .......... .......... .......... .......... 70% 100M 1s 185700K .......... .......... .......... .......... .......... 70% 139M 1s 185750K .......... .......... .......... .......... .......... 70% 102M 1s 185800K .......... .......... .......... .......... .......... 70% 100M 1s 185850K .......... .......... .......... .......... .......... 70% 92.3M 1s 185900K .......... .......... .......... .......... .......... 70% 108M 1s 185950K .......... .......... .......... .......... .......... 70% 89.3M 1s 186000K .......... .......... .......... .......... .......... 70% 141M 1s 186050K .......... .......... .......... .......... .......... 70% 104M 1s 186100K .......... .......... .......... .......... .......... 70% 84.0M 1s 186150K .......... .......... .......... .......... .......... 71% 175M 1s 186200K .......... .......... .......... .......... .......... 71% 21.1M 1s 186250K .......... .......... .......... .......... .......... 71% 186M 1s 186300K .......... .......... .......... .......... .......... 71% 12.1M 1s 186350K .......... .......... .......... .......... .......... 71% 153M 1s 186400K .......... .......... .......... .......... .......... 71% 43.7M 1s 186450K .......... .......... .......... .......... .......... 71% 108M 1s 186500K .......... .......... .......... .......... .......... 71% 108M 1s 186550K .......... .......... .......... .......... .......... 71% 64.9M 1s 186600K .......... .......... .......... .......... .......... 71% 92.3M 1s 186650K .......... .......... .......... .......... .......... 71% 126M 1s 186700K .......... .......... .......... .......... .......... 71% 75.6M 1s 186750K .......... .......... .......... .......... .......... 71% 137M 1s 186800K .......... .......... .......... .......... .......... 71% 85.4M 1s 186850K .......... .......... .......... .......... .......... 71% 94.3M 1s 186900K .......... .......... .......... .......... .......... 71% 99.4M 1s 186950K .......... .......... .......... .......... .......... 71% 66.0M 1s 187000K .......... .......... .......... .......... .......... 71% 178M 1s 187050K .......... .......... .......... .......... .......... 71% 79.4M 1s 187100K .......... .......... .......... .......... .......... 71% 20.2M 1s 187150K .......... .......... .......... .......... .......... 71% 503M 1s 187200K .......... .......... .......... .......... .......... 71% 31.8M 1s 187250K .......... .......... .......... .......... .......... 71% 525M 1s 187300K .......... .......... .......... .......... .......... 71% 10.9M 1s 187350K .......... .......... .......... .......... .......... 71% 332M 1s 187400K .......... .......... .......... .......... .......... 71% 514M 1s 187450K .......... .......... .......... .......... .......... 71% 32.4M 1s 187500K .......... .......... .......... .......... .......... 71% 537M 1s 187550K .......... .......... .......... .......... .......... 71% 156M 1s 187600K .......... 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.......... .......... .......... 71% 126M 1s 188300K .......... .......... .......... .......... .......... 71% 135M 1s 188350K .......... .......... .......... .......... .......... 71% 35.7M 1s 188400K .......... .......... .......... .......... .......... 71% 11.2M 1s 188450K .......... .......... .......... .......... .......... 71% 35.4M 1s 188500K .......... .......... .......... .......... .......... 71% 164M 1s 188550K .......... .......... .......... .......... .......... 71% 169M 1s 188600K .......... .......... .......... .......... .......... 71% 74.3M 1s 188650K .......... .......... .......... .......... .......... 71% 51.5M 1s 188700K .......... .......... .......... .......... .......... 71% 151M 1s 188750K .......... .......... .......... .......... .......... 72% 196M 1s 188800K .......... .......... .......... .......... .......... 72% 44.9M 1s 188850K .......... .......... .......... .......... .......... 72% 85.4M 1s 188900K .......... .......... .......... .......... .......... 72% 176M 1s 188950K .......... .......... .......... .......... .......... 72% 58.5M 1s 189000K .......... .......... .......... .......... .......... 72% 175M 1s 189050K .......... .......... .......... .......... .......... 72% 97.3M 1s 189100K .......... .......... .......... .......... .......... 72% 75.6M 1s 189150K .......... .......... .......... .......... .......... 72% 113M 1s 189200K .......... .......... .......... .......... .......... 72% 87.5M 1s 189250K .......... .......... .......... .......... .......... 72% 129M 1s 189300K .......... .......... .......... .......... .......... 72% 70.7M 1s 189350K .......... .......... .......... .......... .......... 72% 81.8M 1s 189400K .......... .......... .......... .......... .......... 72% 32.6M 1s 189450K .......... .......... .......... .......... .......... 72% 159M 1s 189500K .......... .......... .......... .......... .......... 72% 191M 1s 189550K .......... .......... .......... .......... 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93.9M 1s 190250K .......... .......... .......... .......... .......... 72% 108M 1s 190300K .......... .......... .......... .......... .......... 72% 73.8M 1s 190350K .......... .......... .......... .......... .......... 72% 162M 1s 190400K .......... .......... .......... .......... .......... 72% 85.7M 1s 190450K .......... .......... .......... .......... .......... 72% 100M 1s 190500K .......... .......... .......... .......... .......... 72% 120M 1s 190550K .......... .......... .......... .......... .......... 72% 10.9M 1s 190600K .......... .......... .......... .......... .......... 72% 153M 1s 190650K .......... .......... .......... .......... .......... 72% 184M 1s 190700K .......... .......... .......... .......... .......... 72% 15.8M 1s 190750K .......... .......... .......... .......... .......... 72% 432M 1s 190800K .......... .......... .......... .......... .......... 72% 514M 1s 190850K .......... .......... .......... .......... .......... 72% 48.8M 1s 190900K 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1s 194200K .......... .......... .......... .......... .......... 74% 151M 1s 194250K .......... .......... .......... .......... .......... 74% 178M 1s 194300K .......... .......... .......... .......... .......... 74% 187M 1s 194350K .......... .......... .......... .......... .......... 74% 26.3M 1s 194400K .......... .......... .......... .......... .......... 74% 488M 1s 194450K .......... .......... .......... .......... .......... 74% 187M 1s 194500K .......... .......... .......... .......... .......... 74% 113M 1s 194550K .......... .......... .......... .......... .......... 74% 115M 1s 194600K .......... .......... .......... .......... .......... 74% 92.3M 1s 194650K .......... .......... .......... .......... .......... 74% 110M 1s 194700K .......... .......... .......... .......... .......... 74% 94.8M 1s 194750K .......... .......... .......... .......... .......... 74% 99.0M 1s 194800K .......... .......... .......... .......... .......... 74% 187M 1s 194850K .......... .......... .......... .......... .......... 74% 90.6M 1s 194900K .......... .......... .......... .......... .......... 74% 143M 1s 194950K .......... .......... .......... .......... .......... 74% 68.2M 1s 195000K .......... .......... .......... .......... .......... 74% 27.9M 1s 195050K .......... .......... .......... .......... .......... 74% 498M 1s 195100K .......... .......... .......... .......... .......... 74% 376M 1s 195150K .......... .......... .......... .......... .......... 74% 525M 1s 195200K .......... .......... .......... .......... .......... 74% 39.4M 1s 195250K .......... .......... .......... .......... .......... 74% 27.0M 1s 195300K .......... .......... .......... .......... .......... 74% 188M 1s 195350K .......... .......... .......... .......... .......... 74% 162M 1s 195400K .......... .......... .......... .......... .......... 74% 15.3M 1s 195450K .......... .......... .......... .......... .......... 74% 126M 1s 195500K .......... .......... 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.......... 75% 93.2M 1s 196850K .......... .......... .......... .......... .......... 75% 94.6M 1s 196900K .......... .......... .......... .......... .......... 75% 120M 1s 196950K .......... .......... .......... .......... .......... 75% 30.0M 1s 197000K .......... .......... .......... .......... .......... 75% 346M 1s 197050K .......... .......... .......... .......... .......... 75% 78.3M 1s 197100K .......... .......... .......... .......... .......... 75% 250M 1s 197150K .......... .......... .......... .......... .......... 75% 59.5M 1s 197200K .......... .......... .......... .......... .......... 75% 239M 1s 197250K .......... .......... .......... .......... .......... 75% 156M 1s 197300K .......... .......... .......... .......... .......... 75% 88.9M 1s 197350K .......... .......... .......... .......... .......... 75% 328M 1s 197400K .......... .......... .......... .......... .......... 75% 163M 1s 197450K .......... .......... .......... .......... .......... 75% 48.8M 1s 197500K .......... .......... .......... .......... .......... 75% 74.5M 1s 197550K .......... .......... .......... .......... .......... 75% 75.2M 1s 197600K .......... .......... .......... .......... .......... 75% 54.7M 1s 197650K .......... .......... .......... .......... .......... 75% 63.2M 1s 197700K .......... .......... .......... .......... .......... 75% 62.0M 1s 197750K .......... .......... .......... .......... .......... 75% 57.6M 1s 197800K .......... .......... .......... .......... .......... 75% 36.5M 1s 197850K .......... .......... .......... .......... .......... 75% 52.1M 1s 197900K .......... .......... .......... .......... .......... 75% 104M 1s 197950K .......... .......... .......... .......... .......... 75% 45.2M 1s 198000K .......... .......... .......... .......... .......... 75% 31.7M 1s 198050K .......... .......... .......... .......... .......... 75% 40.9M 1s 198100K .......... .......... .......... .......... .......... 75% 50.9M 1s 198150K .......... .......... .......... .......... .......... 75% 92.8M 1s 198200K .......... .......... .......... .......... .......... 75% 52.6M 1s 198250K .......... .......... .......... .......... .......... 75% 65.2M 1s 198300K .......... .......... .......... .......... .......... 75% 69.0M 1s 198350K .......... .......... .......... .......... .......... 75% 50.4M 1s 198400K .......... .......... .......... .......... .......... 75% 64.3M 1s 198450K .......... .......... .......... .......... .......... 75% 61.9M 1s 198500K .......... .......... .......... .......... .......... 75% 47.0M 1s 198550K .......... .......... .......... .......... .......... 75% 56.3M 1s 198600K .......... .......... .......... .......... .......... 75% 45.5M 1s 198650K .......... .......... .......... .......... .......... 75% 63.0M 1s 198700K .......... .......... .......... .......... .......... 75% 55.5M 1s 198750K .......... .......... .......... .......... .......... 75% 63.4M 1s 198800K 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93.0M 1s 201450K .......... .......... .......... .......... .......... 76% 64.5M 1s 201500K .......... .......... .......... .......... .......... 76% 90.9M 1s 201550K .......... .......... .......... .......... .......... 76% 95.2M 1s 201600K .......... .......... .......... .......... .......... 76% 75.9M 1s 201650K .......... .......... .......... .......... .......... 76% 78.6M 1s 201700K .......... .......... .......... .......... .......... 76% 73.3M 1s 201750K .......... .......... .......... .......... .......... 76% 77.5M 1s 201800K .......... .......... .......... .......... .......... 76% 95.2M 1s 201850K .......... .......... .......... .......... .......... 76% 74.7M 1s 201900K .......... .......... .......... .......... .......... 77% 73.2M 1s 201950K .......... .......... .......... .......... .......... 77% 75.5M 1s 202000K .......... .......... .......... .......... .......... 77% 75.0M 1s 202050K .......... .......... .......... .......... .......... 77% 94.8M 1s 202100K .......... .......... .......... .......... .......... 77% 62.9M 1s 202150K .......... .......... .......... .......... .......... 77% 76.7M 1s 202200K .......... .......... .......... .......... .......... 77% 74.5M 1s 202250K .......... .......... .......... .......... .......... 77% 94.6M 1s 202300K .......... .......... .......... .......... .......... 77% 116M 1s 202350K .......... .......... .......... .......... .......... 77% 79.0M 1s 202400K .......... .......... .......... .......... .......... 77% 79.0M 1s 202450K .......... .......... .......... .......... .......... 77% 93.9M 1s 202500K .......... .......... .......... .......... .......... 77% 92.7M 1s 202550K .......... .......... .......... .......... .......... 77% 97.1M 1s 202600K .......... .......... .......... .......... .......... 77% 73.4M 1s 202650K .......... .......... .......... .......... .......... 77% 93.7M 1s 202700K .......... .......... .......... .......... .......... 77% 77.0M 1s 202750K 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44.2M 1s 210000K .......... .......... .......... .......... .......... 80% 298M 1s 210050K .......... .......... .......... .......... .......... 80% 144M 1s 210100K .......... .......... .......... .......... .......... 80% 73.4M 1s 210150K .......... .......... .......... .......... .......... 80% 120M 1s 210200K .......... .......... .......... .......... .......... 80% 102M 1s 210250K .......... .......... .......... .......... .......... 80% 97.9M 1s 210300K .......... .......... .......... .......... .......... 80% 73.5M 1s 210350K .......... .......... .......... .......... .......... 80% 154M 1s 210400K .......... .......... .......... .......... .......... 80% 54.6M 1s 210450K .......... .......... .......... .......... .......... 80% 83.5M 1s 210500K .......... .......... .......... .......... .......... 80% 118M 1s 210550K .......... .......... .......... .......... .......... 80% 63.6M 1s 210600K .......... .......... .......... .......... .......... 80% 77.4M 1s 210650K 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.......... .......... 81% 32.8M 1s 212650K .......... .......... .......... .......... .......... 81% 509M 1s 212700K .......... .......... .......... .......... .......... 81% 436M 1s 212750K .......... .......... .......... .......... .......... 81% 46.9M 1s 212800K .......... .......... .......... .......... .......... 81% 133M 1s 212850K .......... .......... .......... .......... .......... 81% 80.6M 1s 212900K .......... .......... .......... .......... .......... 81% 157M 1s 212950K .......... .......... .......... .......... .......... 81% 49.8M 1s 213000K .......... .......... .......... .......... .......... 81% 184M 1s 213050K .......... .......... .......... .......... .......... 81% 189M 1s 213100K .......... .......... .......... .......... .......... 81% 59.6M 1s 213150K .......... .......... .......... .......... .......... 81% 121M 1s 213200K .......... .......... .......... .......... .......... 81% 93.4M 1s 213250K .......... .......... .......... .......... .......... 81% 98.8M 1s 213300K .......... .......... .......... .......... .......... 81% 115M 1s 213350K .......... .......... .......... .......... .......... 81% 95.7M 1s 213400K .......... .......... .......... .......... .......... 81% 109M 1s 213450K .......... .......... .......... .......... .......... 81% 100M 1s 213500K .......... .......... .......... .......... .......... 81% 92.8M 1s 213550K .......... .......... .......... .......... .......... 81% 129M 1s 213600K .......... .......... .......... .......... .......... 81% 126M 1s 213650K .......... .......... .......... .......... .......... 81% 78.1M 1s 213700K .......... .......... .......... .......... .......... 81% 115M 1s 213750K .......... .......... .......... .......... .......... 81% 82.1M 1s 213800K .......... .......... .......... .......... .......... 81% 160M 1s 213850K .......... .......... .......... .......... .......... 81% 91.6M 1s 213900K .......... .......... .......... .......... .......... 81% 133M 1s 213950K .......... .......... .......... .......... .......... 81% 67.3M 1s 214000K .......... .......... .......... .......... .......... 81% 181M 1s 214050K .......... .......... .......... .......... .......... 81% 110M 1s 214100K .......... .......... .......... .......... .......... 81% 92.3M 1s 214150K .......... .......... .......... .......... .......... 81% 91.4M 1s 214200K .......... .......... .......... .......... .......... 81% 88.8M 1s 214250K .......... .......... .......... .......... .......... 81% 121M 1s 214300K .......... .......... .......... .......... .......... 81% 88.3M 1s 214350K .......... .......... .......... .......... .......... 81% 88.9M 1s 214400K .......... .......... .......... .......... .......... 81% 95.0M 1s 214450K .......... .......... .......... .......... .......... 81% 86.1M 1s 214500K .......... .......... .......... .......... .......... 81% 134M 1s 214550K .......... .......... .......... .......... .......... 81% 126M 1s 214600K .......... .......... .......... .......... .......... 81% 97.7M 1s 214650K .......... .......... .......... .......... .......... 81% 131M 1s 214700K .......... .......... .......... .......... .......... 81% 89.1M 1s 214750K .......... .......... .......... .......... .......... 81% 120M 1s 214800K .......... .......... .......... .......... .......... 81% 62.7M 1s 214850K .......... .......... .......... .......... .......... 81% 148M 1s 214900K .......... .......... .......... .......... .......... 81% 68.9M 1s 214950K .......... .......... .......... .......... .......... 81% 40.0M 1s 215000K .......... .......... .......... .......... .......... 82% 456M 1s 215050K .......... .......... .......... .......... .......... 82% 239M 1s 215100K .......... .......... .......... .......... .......... 82% 69.9M 1s 215150K .......... .......... .......... .......... .......... 82% 139M 1s 215200K .......... .......... .......... .......... .......... 82% 90.6M 1s 215250K .......... .......... .......... .......... .......... 82% 65.7M 1s 215300K .......... .......... .......... .......... .......... 82% 161M 1s 215350K .......... .......... .......... .......... .......... 82% 118M 1s 215400K .......... .......... .......... .......... .......... 82% 73.9M 1s 215450K .......... .......... .......... .......... .......... 82% 126M 1s 215500K .......... .......... .......... .......... .......... 82% 134M 1s 215550K .......... .......... .......... .......... .......... 82% 86.9M 1s 215600K .......... .......... .......... .......... .......... 82% 99.0M 1s 215650K .......... .......... .......... .......... .......... 82% 121M 1s 215700K .......... .......... .......... .......... .......... 82% 76.9M 1s 215750K .......... .......... .......... .......... .......... 82% 133M 1s 215800K .......... .......... .......... .......... .......... 82% 107M 1s 215850K .......... .......... .......... .......... .......... 82% 105M 1s 215900K .......... .......... .......... .......... .......... 82% 116M 1s 215950K .......... .......... .......... .......... .......... 82% 70.2M 1s 216000K .......... .......... .......... .......... .......... 82% 125M 1s 216050K .......... .......... .......... .......... .......... 82% 76.9M 1s 216100K .......... .......... .......... .......... .......... 82% 84.3M 1s 216150K .......... .......... .......... .......... .......... 82% 86.0M 1s 216200K .......... .......... .......... .......... .......... 82% 296M 1s 216250K .......... .......... .......... .......... .......... 82% 66.2M 1s 216300K .......... .......... .......... .......... .......... 82% 126M 1s 216350K .......... .......... .......... .......... .......... 82% 94.1M 1s 216400K .......... .......... .......... .......... .......... 82% 77.0M 1s 216450K .......... .......... .......... .......... .......... 82% 110M 1s 216500K .......... .......... .......... .......... .......... 82% 147M 1s 216550K .......... .......... .......... .......... .......... 82% 118M 1s 216600K .......... .......... .......... .......... .......... 82% 52.1M 1s 216650K .......... .......... .......... .......... .......... 82% 436M 1s 216700K .......... .......... .......... .......... .......... 82% 72.3M 1s 216750K .......... .......... .......... .......... .......... 82% 184M 1s 216800K .......... .......... .......... .......... .......... 82% 63.0M 1s 216850K .......... .......... .......... .......... .......... 82% 67.8M 1s 216900K .......... .......... .......... .......... .......... 82% 178M 1s 216950K .......... .......... .......... .......... .......... 82% 83.9M 1s 217000K .......... .......... .......... .......... .......... 82% 134M 1s 217050K .......... .......... .......... .......... .......... 82% 93.0M 1s 217100K .......... .......... .......... .......... .......... 82% 93.7M 1s 217150K .......... .......... .......... .......... .......... 82% 115M 1s 217200K .......... .......... .......... .......... .......... 82% 105M 1s 217250K .......... .......... .......... .......... .......... 82% 118M 1s 217300K .......... .......... .......... .......... .......... 82% 83.5M 1s 217350K .......... .......... .......... .......... .......... 82% 55.2M 1s 217400K .......... .......... .......... .......... .......... 82% 465M 1s 217450K .......... .......... .......... .......... .......... 82% 34.1M 1s 217500K .......... .......... .......... .......... .......... 82% 158M 1s 217550K .......... .......... .......... .......... .......... 82% 180M 1s 217600K .......... .......... .......... .......... .......... 83% 43.5M 1s 217650K .......... .......... .......... .......... .......... 83% 146M 1s 217700K .......... .......... .......... .......... .......... 83% 96.7M 1s 217750K .......... .......... .......... .......... .......... 83% 119M 1s 217800K .......... .......... .......... .......... .......... 83% 127M 1s 217850K .......... .......... .......... .......... .......... 83% 93.9M 1s 217900K .......... .......... .......... .......... .......... 83% 99.4M 1s 217950K .......... .......... .......... .......... .......... 83% 93.2M 1s 218000K .......... .......... .......... .......... .......... 83% 113M 1s 218050K .......... .......... .......... .......... .......... 83% 17.4M 1s 218100K .......... .......... .......... .......... .......... 83% 139M 1s 218150K .......... .......... .......... .......... .......... 83% 146M 1s 218200K .......... .......... .......... .......... .......... 83% 171M 1s 218250K .......... .......... .......... .......... .......... 83% 397M 1s 218300K .......... .......... .......... .......... .......... 83% 452M 1s 218350K .......... .......... .......... .......... .......... 83% 261M 1s 218400K .......... .......... .......... .......... .......... 83% 440M 1s 218450K .......... .......... .......... .......... .......... 83% 432M 1s 218500K .......... .......... .......... .......... .......... 83% 133M 1s 218550K .......... .......... .......... .......... .......... 83% 75.8M 1s 218600K .......... .......... .......... .......... .......... 83% 75.7M 1s 218650K .......... .......... .......... .......... .......... 83% 62.9M 1s 218700K .......... .......... .......... .......... .......... 83% 75.1M 1s 218750K .......... .......... .......... .......... .......... 83% 120M 1s 218800K .......... .......... .......... .......... .......... 83% 64.8M 1s 218850K .......... .......... .......... .......... .......... 83% 90.9M 1s 218900K .......... .......... .......... .......... .......... 83% 75.1M 1s 218950K .......... .......... .......... .......... .......... 83% 77.8M 1s 219000K .......... .......... .......... .......... .......... 83% 75.5M 1s 219050K .......... .......... .......... .......... .......... 83% 64.2M 1s 219100K .......... .......... .......... .......... .......... 83% 93.5M 1s 219150K .......... .......... .......... .......... .......... 83% 79.8M 1s 219200K .......... .......... 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84% 6.14M 1s 221200K .......... .......... .......... .......... .......... 84% 388M 1s 221250K .......... .......... .......... .......... .......... 84% 43.2M 1s 221300K .......... .......... .......... .......... .......... 84% 135M 1s 221350K .......... .......... .......... .......... .......... 84% 93.5M 1s 221400K .......... .......... .......... .......... .......... 84% 98.4M 1s 221450K .......... .......... .......... .......... .......... 84% 61.6M 1s 221500K .......... .......... .......... .......... .......... 84% 112M 1s 221550K .......... .......... .......... .......... .......... 84% 474M 1s 221600K .......... .......... .......... .......... .......... 84% 76.3M 1s 221650K .......... .......... .......... .......... .......... 84% 98.6M 1s 221700K .......... .......... .......... .......... .......... 84% 121M 1s 221750K .......... .......... .......... .......... .......... 84% 117M 1s 221800K .......... .......... .......... .......... .......... 84% 134M 1s 221850K .......... .......... .......... .......... .......... 84% 71.5M 1s 221900K .......... .......... .......... .......... .......... 84% 135M 1s 221950K .......... .......... .......... .......... .......... 84% 87.2M 1s 222000K .......... .......... .......... .......... .......... 84% 96.1M 1s 222050K .......... .......... .......... .......... .......... 84% 115M 1s 222100K .......... .......... .......... .......... .......... 84% 105M 1s 222150K .......... .......... .......... .......... .......... 84% 74.4M 1s 222200K .......... .......... .......... .......... .......... 84% 119M 1s 222250K .......... .......... .......... .......... .......... 84% 96.3M 1s 222300K .......... .......... .......... .......... .......... 84% 119M 1s 222350K .......... .......... .......... .......... .......... 84% 93.9M 1s 222400K .......... .......... .......... .......... .......... 84% 113M 1s 222450K .......... .......... .......... .......... .......... 84% 82.2M 1s 222500K .......... 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.......... 85% 93.2M 0s 224500K .......... .......... .......... .......... .......... 85% 123M 0s 224550K .......... .......... .......... .......... .......... 85% 97.9M 0s 224600K .......... .......... .......... .......... .......... 85% 109M 0s 224650K .......... .......... .......... .......... .......... 85% 101M 0s 224700K .......... .......... .......... .......... .......... 85% 65.2M 0s 224750K .......... .......... .......... .......... .......... 85% 121M 0s 224800K .......... .......... .......... .......... .......... 85% 131M 0s 224850K .......... .......... .......... .......... .......... 85% 93.9M 0s 224900K .......... .......... .......... .......... .......... 85% 75.1M 0s 224950K .......... .......... .......... .......... .......... 85% 115M 0s 225000K .......... .......... .......... .......... .......... 85% 80.3M 0s 225050K .......... .......... .......... .......... .......... 85% 119M 0s 225100K .......... .......... .......... .......... .......... 85% 93.7M 0s 225150K .......... .......... .......... .......... .......... 85% 101M 0s 225200K .......... .......... .......... .......... .......... 85% 93.7M 0s 225250K .......... .......... .......... .......... .......... 85% 118M 0s 225300K .......... .......... .......... .......... .......... 85% 128M 0s 225350K .......... .......... .......... .......... .......... 85% 27.8M 0s 225400K .......... .......... .......... .......... .......... 85% 163M 0s 225450K .......... .......... .......... .......... .......... 86% 32.1M 0s 225500K .......... .......... .......... .......... .......... 86% 444M 0s 225550K .......... .......... .......... .......... .......... 86% 483M 0s 225600K .......... .......... .......... .......... .......... 86% 440M 0s 225650K .......... .......... .......... .......... .......... 86% 80.6M 0s 225700K .......... .......... .......... .......... .......... 86% 74.9M 0s 225750K .......... .......... .......... .......... .......... 86% 95.0M 0s 225800K 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.......... .......... .......... 86% 68.8M 0s 227150K .......... .......... .......... .......... .......... 86% 102M 0s 227200K .......... .......... .......... .......... .......... 86% 74.9M 0s 227250K .......... .......... .......... .......... .......... 86% 97.9M 0s 227300K .......... .......... .......... .......... .......... 86% 90.3M 0s 227350K .......... .......... .......... .......... .......... 86% 63.6M 0s 227400K .......... .......... .......... .......... .......... 86% 93.9M 0s 227450K .......... .......... .......... .......... .......... 86% 93.4M 0s 227500K .......... .......... .......... .......... .......... 86% 94.6M 0s 227550K .......... .......... .......... .......... .......... 86% 71.7M 0s 227600K .......... .......... .......... .......... .......... 86% 80.6M 0s 227650K .......... .......... .......... .......... .......... 86% 89.1M 0s 227700K .......... .......... .......... .......... .......... 86% 79.1M 0s 227750K .......... .......... .......... .......... .......... 86% 120M 0s 227800K .......... .......... .......... .......... .......... 86% 95.9M 0s 227850K .......... .......... .......... .......... .......... 86% 94.8M 0s 227900K .......... .......... .......... .......... .......... 86% 74.5M 0s 227950K .......... .......... .......... .......... .......... 86% 127M 0s 228000K .......... .......... .......... .......... .......... 86% 76.1M 0s 228050K .......... .......... .......... .......... .......... 86% 95.2M 0s 228100K .......... .......... .......... .......... .......... 87% 68.6M 0s 228150K .......... .......... .......... .......... .......... 87% 72.0M 0s 228200K .......... .......... .......... .......... .......... 87% 75.4M 0s 228250K .......... .......... .......... .......... .......... 87% 108M 0s 228300K .......... .......... .......... .......... .......... 87% 57.3M 0s 228350K .......... .......... .......... .......... .......... 87% 97.7M 0s 228400K .......... .......... .......... .......... .......... 87% 83.8M 0s 228450K .......... .......... .......... .......... .......... 87% 82.6M 0s 228500K .......... .......... .......... .......... .......... 87% 81.1M 0s 228550K .......... .......... .......... .......... .......... 87% 57.6M 0s 228600K .......... .......... .......... .......... .......... 87% 57.7M 0s 228650K .......... .......... .......... .......... .......... 87% 112M 0s 228700K .......... .......... .......... .......... .......... 87% 29.5M 0s 228750K .......... .......... .......... .......... .......... 87% 174M 0s 228800K .......... .......... .......... .......... .......... 87% 12.5M 0s 228850K .......... .......... .......... .......... .......... 87% 222M 0s 228900K .......... .......... .......... .......... .......... 87% 158M 0s 228950K .......... .......... .......... .......... .......... 87% 13.2M 0s 229000K .......... .......... .......... .......... .......... 87% 509M 0s 229050K .......... .......... .......... .......... .......... 87% 531M 0s 229100K .......... .......... .......... .......... .......... 87% 39.4M 0s 229150K .......... .......... .......... .......... .......... 87% 122M 0s 229200K .......... .......... .......... .......... .......... 87% 85.7M 0s 229250K .......... .......... .......... .......... .......... 87% 100M 0s 229300K .......... .......... .......... .......... .......... 87% 101M 0s 229350K .......... .......... .......... .......... .......... 87% 95.6M 0s 229400K .......... .......... .......... .......... .......... 87% 79.9M 0s 229450K .......... .......... .......... .......... .......... 87% 98.0M 0s 229500K .......... .......... .......... .......... .......... 87% 24.2M 0s 229550K .......... .......... .......... .......... .......... 87% 189M 0s 229600K .......... .......... .......... .......... .......... 87% 167M 0s 229650K .......... .......... .......... .......... .......... 87% 11.9M 0s 229700K .......... .......... .......... .......... .......... 87% 29.6M 0s 229750K .......... .......... .......... .......... .......... 87% 36.8M 0s 229800K .......... .......... .......... .......... .......... 87% 309M 0s 229850K .......... .......... .......... .......... .......... 87% 74.3M 0s 229900K .......... .......... .......... .......... .......... 87% 118M 0s 229950K .......... .......... .......... .......... .......... 87% 112M 0s 230000K .......... .......... .......... .......... .......... 87% 123M 0s 230050K .......... .......... .......... .......... .......... 87% 105M 0s 230100K .......... .......... .......... .......... .......... 87% 104M 0s 230150K .......... .......... .......... .......... .......... 87% 81.4M 0s 230200K .......... .......... .......... .......... .......... 87% 88.3M 0s 230250K .......... .......... .......... .......... .......... 87% 107M 0s 230300K .......... .......... .......... .......... .......... 87% 117M 0s 230350K .......... .......... .......... .......... .......... 87% 99.4M 0s 230400K .......... .......... .......... .......... .......... 87% 138M 0s 230450K .......... .......... .......... .......... .......... 87% 60.9M 0s 230500K .......... .......... .......... .......... .......... 87% 133M 0s 230550K .......... .......... .......... .......... .......... 87% 126M 0s 230600K .......... .......... .......... .......... .......... 87% 79.0M 0s 230650K .......... .......... .......... .......... .......... 87% 124M 0s 230700K .......... .......... .......... .......... .......... 88% 91.4M 0s 230750K .......... .......... .......... .......... .......... 88% 120M 0s 230800K .......... .......... .......... .......... .......... 88% 93.0M 0s 230850K .......... .......... .......... .......... .......... 88% 45.0M 0s 230900K .......... .......... .......... .......... .......... 88% 182M 0s 230950K .......... .......... .......... .......... .......... 88% 14.7M 0s 231000K .......... .......... .......... .......... .......... 88% 341M 0s 231050K .......... .......... .......... .......... .......... 88% 514M 0s 231100K .......... .......... .......... .......... .......... 88% 34.9M 0s 231150K .......... .......... .......... .......... .......... 88% 493M 0s 231200K .......... .......... .......... .......... .......... 88% 77.5M 0s 231250K .......... .......... .......... .......... .......... 88% 98.0M 0s 231300K .......... .......... .......... .......... .......... 88% 104M 0s 231350K .......... .......... .......... .......... .......... 88% 93.7M 0s 231400K .......... .......... .......... .......... .......... 88% 57.4M 0s 231450K .......... .......... .......... .......... .......... 88% 72.1M 0s 231500K .......... .......... .......... .......... .......... 88% 173M 0s 231550K .......... .......... .......... .......... .......... 88% 66.4M 0s 231600K .......... .......... .......... .......... .......... 88% 102M 0s 231650K .......... .......... .......... .......... .......... 88% 87.2M 0s 231700K .......... .......... .......... .......... .......... 88% 137M 0s 231750K .......... .......... .......... .......... .......... 88% 97.5M 0s 231800K .......... .......... .......... .......... .......... 88% 103M 0s 231850K .......... .......... .......... .......... .......... 88% 84.2M 0s 231900K .......... .......... .......... .......... .......... 88% 108M 0s 231950K .......... .......... .......... .......... .......... 88% 102M 0s 232000K .......... .......... .......... .......... .......... 88% 113M 0s 232050K .......... .......... .......... .......... .......... 88% 51.8M 0s 232100K .......... .......... .......... .......... .......... 88% 163M 0s 232150K .......... .......... .......... .......... .......... 88% 195M 0s 232200K .......... .......... .......... .......... .......... 88% 23.1M 0s 232250K .......... .......... .......... .......... .......... 88% 189M 0s 232300K .......... .......... .......... .......... .......... 88% 31.1M 0s 232350K .......... .......... .......... .......... .......... 88% 210M 0s 232400K .......... .......... .......... .......... .......... 88% 56.7M 0s 232450K .......... .......... .......... .......... .......... 88% 40.0M 0s 232500K .......... .......... .......... .......... .......... 88% 114M 0s 232550K .......... .......... .......... .......... .......... 88% 208M 0s 232600K .......... .......... .......... .......... .......... 88% 59.1M 0s 232650K .......... .......... .......... .......... .......... 88% 31.8M 0s 232700K .......... .......... .......... .......... .......... 88% 407M 0s 232750K .......... .......... .......... .......... .......... 88% 261M 0s 232800K .......... .......... .......... .......... .......... 88% 44.9M 0s 232850K .......... .......... .......... .......... .......... 88% 70.3M 0s 232900K .......... .......... .......... .......... .......... 88% 428M 0s 232950K .......... .......... .......... .......... .......... 88% 75.4M 0s 233000K .......... .......... .......... .......... .......... 88% 128M 0s 233050K .......... .......... .......... .......... .......... 88% 79.0M 0s 233100K .......... .......... .......... .......... .......... 88% 102M 0s 233150K .......... .......... .......... .......... .......... 88% 132M 0s 233200K .......... .......... .......... .......... .......... 88% 103M 0s 233250K .......... .......... .......... .......... .......... 88% 82.1M 0s 233300K .......... .......... .......... .......... .......... 88% 146M 0s 233350K .......... .......... .......... .......... .......... 89% 26.2M 0s 233400K .......... .......... .......... .......... .......... 89% 187M 0s 233450K .......... .......... .......... .......... .......... 89% 18.1M 0s 233500K .......... .......... .......... .......... .......... 89% 330M 0s 233550K .......... .......... .......... .......... .......... 89% 474M 0s 233600K .......... .......... .......... .......... .......... 89% 22.5M 0s 233650K .......... .......... .......... .......... .......... 89% 36.9M 0s 233700K .......... .......... .......... .......... .......... 89% 432M 0s 233750K .......... .......... .......... .......... .......... 89% 42.6M 0s 233800K .......... .......... .......... .......... .......... 89% 186M 0s 233850K .......... .......... .......... .......... .......... 89% 108M 0s 233900K .......... .......... .......... .......... .......... 89% 74.1M 0s 233950K .......... .......... .......... .......... .......... 89% 100M 0s 234000K .......... .......... .......... .......... .......... 89% 136M 0s 234050K .......... .......... .......... .......... .......... 89% 83.8M 0s 234100K .......... .......... .......... .......... .......... 89% 122M 0s 234150K .......... .......... .......... .......... .......... 89% 71.1M 0s 234200K .......... .......... .......... .......... .......... 89% 103M 0s 234250K .......... .......... .......... .......... .......... 89% 91.6M 0s 234300K .......... .......... .......... .......... .......... 89% 120M 0s 234350K .......... .......... .......... .......... .......... 89% 95.7M 0s 234400K .......... .......... .......... .......... .......... 89% 103M 0s 234450K .......... .......... .......... .......... .......... 89% 96.5M 0s 234500K .......... .......... .......... .......... .......... 89% 32.6M 0s 234550K .......... .......... .......... .......... .......... 89% 166M 0s 234600K .......... .......... .......... .......... .......... 89% 156M 0s 234650K .......... .......... .......... .......... .......... 89% 18.5M 0s 234700K .......... .......... .......... .......... .......... 89% 417M 0s 234750K .......... .......... .......... .......... .......... 89% 514M 0s 234800K .......... .......... .......... .......... .......... 89% 25.2M 0s 234850K .......... .......... .......... .......... .......... 89% 156M 0s 234900K .......... .......... .......... .......... .......... 89% 29.3M 0s 234950K .......... .......... .......... .......... .......... 89% 319M 0s 235000K .......... .......... .......... .......... .......... 89% 531M 0s 235050K .......... .......... .......... .......... .......... 89% 54.1M 0s 235100K .......... .......... .......... .......... .......... 89% 97.9M 0s 235150K .......... .......... .......... .......... .......... 89% 98.8M 0s 235200K .......... .......... .......... .......... .......... 89% 106M 0s 235250K .......... .......... .......... .......... .......... 89% 138M 0s 235300K .......... .......... .......... .......... .......... 89% 119M 0s 235350K .......... .......... .......... .......... .......... 89% 95.2M 0s 235400K .......... .......... .......... .......... .......... 89% 93.0M 0s 235450K .......... .......... .......... .......... .......... 89% 71.0M 0s 235500K .......... .......... .......... .......... .......... 89% 110M 0s 235550K .......... .......... .......... .......... .......... 89% 101M 0s 235600K .......... .......... .......... .......... .......... 89% 100M 0s 235650K .......... .......... .......... .......... .......... 89% 105M 0s 235700K .......... .......... .......... .......... .......... 89% 105M 0s 235750K .......... .......... .......... .......... .......... 89% 66.3M 0s 235800K .......... .......... .......... .......... .......... 89% 36.9M 0s 235850K .......... .......... .......... .......... .......... 89% 461M 0s 235900K .......... .......... .......... .......... .......... 89% 17.9M 0s 235950K .......... .......... .......... .......... .......... 90% 129M 0s 236000K .......... .......... .......... .......... .......... 90% 187M 0s 236050K .......... .......... .......... .......... .......... 90% 40.9M 0s 236100K .......... .......... .......... .......... .......... 90% 63.8M 0s 236150K .......... .......... .......... .......... .......... 90% 178M 0s 236200K .......... .......... .......... .......... .......... 90% 134M 0s 236250K .......... .......... .......... .......... .......... 90% 42.5M 0s 236300K .......... .......... .......... .......... .......... 90% 142M 0s 236350K .......... .......... .......... .......... .......... 90% 95.2M 0s 236400K .......... .......... .......... .......... .......... 90% 110M 0s 236450K .......... .......... .......... .......... .......... 90% 89.6M 0s 236500K .......... .......... .......... .......... .......... 90% 175M 0s 236550K .......... .......... .......... .......... .......... 90% 103M 0s 236600K .......... .......... .......... .......... .......... 90% 85.2M 0s 236650K .......... .......... .......... .......... .......... 90% 112M 0s 236700K .......... .......... .......... .......... .......... 90% 65.7M 0s 236750K .......... .......... .......... .......... .......... 90% 125M 0s 236800K .......... .......... .......... .......... .......... 90% 114M 0s 236850K .......... .......... .......... .......... .......... 90% 92.1M 0s 236900K .......... .......... .......... .......... .......... 90% 93.0M 0s 236950K .......... .......... .......... .......... .......... 90% 152M 0s 237000K .......... .......... .......... .......... .......... 90% 63.0M 0s 237050K .......... .......... .......... .......... .......... 90% 150M 0s 237100K .......... .......... .......... .......... .......... 90% 65.7M 0s 237150K .......... .......... .......... .......... .......... 90% 68.8M 0s 237200K .......... .......... .......... .......... .......... 90% 135M 0s 237250K .......... .......... .......... .......... .......... 90% 89.8M 0s 237300K .......... .......... .......... .......... .......... 90% 57.4M 0s 237350K .......... .......... .......... .......... .......... 90% 95.6M 0s 237400K .......... .......... .......... .......... .......... 90% 125M 0s 237450K .......... .......... .......... .......... .......... 90% 92.0M 0s 237500K .......... .......... .......... .......... .......... 90% 97.5M 0s 237550K .......... .......... .......... .......... .......... 90% 52.3M 0s 237600K .......... .......... .......... .......... .......... 90% 332M 0s 237650K .......... .......... .......... .......... .......... 90% 140M 0s 237700K .......... .......... .......... .......... .......... 90% 73.4M 0s 237750K .......... .......... .......... .......... .......... 90% 97.7M 0s 237800K .......... .......... .......... .......... .......... 90% 123M 0s 237850K .......... .......... .......... .......... .......... 90% 92.0M 0s 237900K .......... .......... .......... .......... .......... 90% 124M 0s 237950K .......... .......... .......... .......... .......... 90% 74.3M 0s 238000K .......... .......... .......... .......... .......... 90% 32.1M 0s 238050K .......... .......... .......... .......... .......... 90% 152M 0s 238100K .......... .......... .......... .......... .......... 90% 397M 0s 238150K .......... .......... .......... .......... .......... 90% 89.8M 0s 238200K .......... .......... .......... .......... .......... 90% 92.8M 0s 238250K .......... .......... .......... .......... .......... 90% 493M 0s 238300K .......... .......... .......... .......... .......... 90% 448M 0s 238350K .......... .......... .......... .......... .......... 90% 63.0M 0s 238400K .......... .......... .......... .......... .......... 90% 73.6M 0s 238450K .......... .......... .......... .......... .......... 90% 79.0M 0s 238500K .......... .......... .......... .......... .......... 90% 94.4M 0s 238550K .......... .......... .......... .......... .......... 90% 92.5M 0s 238600K .......... .......... .......... .......... .......... 91% 74.0M 0s 238650K .......... .......... .......... .......... .......... 91% 76.8M 0s 238700K .......... .......... .......... .......... .......... 91% 53.7M 0s 238750K .......... .......... .......... .......... .......... 91% 134M 0s 238800K .......... .......... .......... .......... .......... 91% 63.1M 0s 238850K .......... .......... .......... .......... .......... 91% 75.7M 0s 238900K .......... .......... .......... .......... .......... 91% 88.5M 0s 238950K .......... .......... .......... .......... .......... 91% 56.3M 0s 239000K .......... .......... .......... .......... .......... 91% 114M 0s 239050K .......... .......... .......... .......... .......... 91% 66.4M 0s 239100K .......... .......... .......... .......... .......... 91% 63.0M 0s 239150K .......... .......... .......... .......... .......... 91% 120M 0s 239200K .......... .......... .......... .......... .......... 91% 61.6M 0s 239250K .......... .......... .......... .......... .......... 91% 78.0M 0s 239300K .......... .......... .......... .......... .......... 91% 94.4M 0s 239350K .......... .......... .......... .......... .......... 91% 74.0M 0s 239400K .......... .......... .......... .......... .......... 91% 72.3M 0s 239450K .......... .......... .......... .......... .......... 91% 57.0M 0s 239500K .......... .......... .......... .......... .......... 91% 93.2M 0s 239550K .......... .......... .......... .......... .......... 91% 71.7M 0s 239600K .......... .......... .......... .......... .......... 91% 76.8M 0s 239650K .......... .......... .......... .......... .......... 91% 76.8M 0s 239700K .......... .......... .......... .......... .......... 91% 77.0M 0s 239750K .......... .......... .......... .......... .......... 91% 92.5M 0s 239800K .......... .......... .......... .......... .......... 91% 64.8M 0s 239850K .......... .......... .......... .......... .......... 91% 94.3M 0s 239900K .......... .......... .......... .......... .......... 91% 63.6M 0s 239950K .......... .......... .......... .......... .......... 91% 75.7M 0s 240000K .......... .......... .......... .......... .......... 91% 75.5M 0s 240050K .......... .......... .......... .......... .......... 91% 74.8M 0s 240100K .......... .......... .......... .......... .......... 91% 62.7M 0s 240150K .......... .......... .......... .......... .......... 91% 118M 0s 240200K .......... .......... .......... .......... .......... 91% 55.6M 0s 240250K .......... .......... .......... .......... .......... 91% 63.1M 0s 240300K .......... .......... .......... .......... .......... 91% 76.7M 0s 240350K .......... .......... .......... .......... .......... 91% 62.8M 0s 240400K .......... .......... .......... .......... .......... 91% 92.3M 0s 240450K .......... .......... .......... .......... .......... 91% 62.8M 0s 240500K .......... .......... .......... .......... .......... 91% 76.4M 0s 240550K .......... .......... .......... .......... .......... 91% 76.4M 0s 240600K .......... .......... .......... .......... .......... 91% 73.9M 0s 240650K .......... .......... .......... .......... .......... 91% 82.9M 0s 240700K .......... .......... .......... .......... .......... 91% 57.6M 0s 240750K .......... .......... .......... .......... .......... 91% 64.8M 0s 240800K .......... .......... .......... .......... .......... 91% 125M 0s 240850K .......... .......... .......... .......... .......... 91% 62.8M 0s 240900K .......... .......... .......... .......... .......... 91% 76.2M 0s 240950K .......... .......... .......... .......... .......... 91% 73.0M 0s 241000K .......... .......... .......... .......... .......... 91% 93.5M 0s 241050K .......... .......... .......... .......... .......... 91% 93.2M 0s 241100K .......... .......... .......... .......... .......... 91% 98.0M 0s 241150K .......... .......... .......... .......... .......... 91% 94.4M 0s 241200K .......... .......... .......... .......... .......... 92% 95.7M 0s 241250K .......... .......... .......... .......... .......... 92% 119M 0s 241300K .......... .......... .......... .......... .......... 92% 22.1M 0s 241350K .......... .......... .......... .......... .......... 92% 113M 0s 241400K .......... .......... .......... .......... .......... 92% 160M 0s 241450K .......... .......... .......... .......... .......... 92% 139M 0s 241500K .......... .......... .......... .......... .......... 92% 274M 0s 241550K .......... .......... .......... .......... .......... 92% 456M 0s 241600K .......... .......... .......... .......... .......... 92% 31.4M 0s 241650K .......... .......... .......... .......... .......... 92% 448M 0s 241700K .......... .......... .......... .......... .......... 92% 356M 0s 241750K .......... .......... .......... .......... .......... 92% 444M 0s 241800K .......... .......... .......... .......... .......... 92% 452M 0s 241850K .......... .......... .......... .......... .......... 92% 224M 0s 241900K .......... .......... .......... .......... .......... 92% 94.3M 0s 241950K .......... .......... .......... .......... .......... 92% 53.4M 0s 242000K .......... .......... .......... .......... .......... 92% 64.2M 0s 242050K .......... .......... .......... .......... .......... 92% 93.5M 0s 242100K .......... .......... .......... .......... .......... 92% 63.4M 0s 242150K .......... .......... .......... .......... .......... 92% 74.7M 0s 242200K .......... .......... .......... .......... .......... 92% 54.6M 0s 242250K .......... .......... .......... .......... .......... 92% 120M 0s 242300K .......... .......... .......... .......... .......... 92% 53.2M 0s 242350K .......... .......... .......... .......... .......... 92% 78.8M 0s 242400K .......... .......... .......... .......... .......... 92% 66.6M 0s 242450K .......... .......... .......... .......... .......... 92% 70.2M 0s 242500K .......... .......... .......... .......... .......... 92% 27.2M 0s 242550K .......... .......... .......... .......... .......... 92% 47.3M 0s 242600K .......... .......... .......... .......... .......... 92% 94.3M 0s 242650K .......... .......... .......... .......... .......... 92% 73.0M 0s 242700K .......... .......... .......... .......... .......... 92% 64.5M 0s 242750K .......... .......... .......... .......... .......... 92% 92.8M 0s 242800K .......... .......... .......... .......... .......... 92% 64.5M 0s 242850K .......... .......... .......... .......... .......... 92% 62.4M 0s 242900K .......... .......... .......... .......... .......... 92% 65.0M 0s 242950K .......... .......... .......... .......... .......... 92% 94.3M 0s 243000K .......... .......... .......... .......... .......... 92% 71.3M 0s 243050K .......... .......... .......... .......... .......... 92% 63.8M 0s 243100K .......... .......... .......... .......... .......... 92% 41.3M 0s 243150K .......... .......... .......... .......... .......... 92% 44.5M 0s 243200K .......... .......... .......... .......... .......... 92% 54.1M 0s 243250K .......... .......... .......... .......... .......... 92% 126M 0s 243300K .......... .......... .......... .......... .......... 92% 61.0M 0s 243350K .......... .......... .......... .......... .......... 92% 61.0M 0s 243400K .......... .......... .......... .......... .......... 92% 59.3M 0s 243450K .......... .......... .......... .......... .......... 92% 40.2M 0s 243500K .......... .......... .......... .......... .......... 92% 157M 0s 243550K .......... .......... .......... .......... .......... 92% 66.0M 0s 243600K .......... .......... .......... .......... .......... 92% 63.3M 0s 243650K .......... .......... .......... .......... .......... 92% 72.2M 0s 243700K .......... .......... .......... .......... .......... 92% 78.3M 0s 243750K .......... .......... .......... .......... .......... 92% 74.5M 0s 243800K .......... .......... .......... .......... .......... 92% 65.3M 0s 243850K .......... .......... .......... .......... .......... 93% 70.7M 0s 243900K .......... .......... .......... .......... .......... 93% 57.0M 0s 243950K .......... .......... .......... .......... .......... 93% 113M 0s 244000K .......... .......... .......... .......... .......... 93% 55.6M 0s 244050K .......... .......... .......... .......... .......... 93% 78.0M 0s 244100K .......... .......... .......... .......... .......... 93% 62.2M 0s 244150K .......... .......... .......... .......... .......... 93% 63.5M 0s 244200K .......... .......... .......... .......... .......... 93% 85.2M 0s 244250K .......... .......... .......... .......... .......... 93% 66.4M 0s 244300K .......... .......... .......... .......... .......... 93% 128M 0s 244350K .......... .......... .......... .......... .......... 93% 94.3M 0s 244400K .......... .......... .......... .......... .......... 93% 110M 0s 244450K .......... .......... .......... .......... .......... 93% 81.4M 0s 244500K .......... .......... .......... .......... .......... 93% 98.4M 0s 244550K .......... .......... .......... .......... .......... 93% 156M 0s 244600K .......... .......... .......... .......... .......... 93% 77.4M 0s 244650K .......... .......... .......... .......... .......... 93% 28.5M 0s 244700K .......... .......... .......... .......... .......... 93% 313M 0s 244750K .......... .......... .......... .......... .......... 93% 119M 0s 244800K .......... .......... .......... .......... .......... 93% 367M 0s 244850K .......... .......... .......... .......... .......... 93% 421M 0s 244900K .......... .......... .......... .......... .......... 93% 33.7M 0s 244950K .......... .......... .......... .......... .......... 93% 229M 0s 245000K .......... .......... .......... .......... .......... 93% 124M 0s 245050K .......... .......... .......... .......... .......... 93% 165M 0s 245100K .......... .......... .......... .......... .......... 93% 140M 0s 245150K .......... .......... .......... .......... .......... 93% 167M 0s 245200K .......... .......... .......... .......... .......... 93% 111M 0s 245250K .......... .......... .......... .......... .......... 93% 90.3M 0s 245300K .......... .......... .......... .......... .......... 93% 95.9M 0s 245350K .......... .......... .......... .......... .......... 93% 78.0M 0s 245400K .......... .......... .......... .......... .......... 93% 91.1M 0s 245450K .......... .......... .......... .......... .......... 93% 75.0M 0s 245500K .......... .......... .......... .......... .......... 93% 76.3M 0s 245550K .......... .......... .......... .......... .......... 93% 76.9M 0s 245600K .......... .......... .......... .......... .......... 93% 93.7M 0s 245650K .......... .......... .......... .......... .......... 93% 75.7M 0s 245700K .......... .......... .......... .......... .......... 93% 72.6M 0s 245750K .......... .......... .......... .......... .......... 93% 78.0M 0s 245800K .......... .......... .......... .......... .......... 93% 75.9M 0s 245850K .......... .......... .......... .......... .......... 93% 92.0M 0s 245900K .......... .......... .......... .......... .......... 93% 92.3M 0s 245950K .......... .......... .......... .......... .......... 93% 64.2M 0s 246000K .......... .......... .......... .......... .......... 93% 75.0M 0s 246050K .......... .......... .......... .......... .......... 93% 87.2M 0s 246100K .......... .......... .......... .......... .......... 93% 97.5M 0s 246150K .......... .......... .......... .......... .......... 93% 75.7M 0s 246200K .......... .......... .......... .......... .......... 93% 64.3M 0s 246250K .......... .......... .......... .......... .......... 93% 72.1M 0s 246300K .......... .......... .......... .......... .......... 93% 143M 0s 246350K .......... .......... .......... .......... .......... 93% 35.3M 0s 246400K .......... .......... .......... .......... .......... 93% 43.8M 0s 246450K .......... .......... .......... .......... .......... 94% 95.9M 0s 246500K .......... .......... .......... .......... .......... 94% 94.6M 0s 246550K .......... .......... .......... .......... .......... 94% 91.3M 0s 246600K .......... .......... .......... .......... .......... 94% 78.8M 0s 246650K .......... .......... .......... .......... .......... 94% 114M 0s 246700K .......... .......... .......... .......... .......... 94% 77.5M 0s 246750K .......... .......... .......... .......... .......... 94% 77.0M 0s 246800K .......... .......... .......... .......... .......... 94% 94.6M 0s 246850K .......... .......... .......... .......... .......... 94% 91.1M 0s 246900K .......... .......... .......... .......... .......... 94% 76.4M 0s 246950K .......... .......... .......... .......... .......... 94% 64.3M 0s 247000K .......... .......... .......... .......... .......... 94% 174M 0s 247050K .......... .......... .......... .......... .......... 94% 76.9M 0s 247100K .......... .......... .......... .......... .......... 94% 89.8M 0s 247150K .......... .......... .......... .......... .......... 94% 62.3M 0s 247200K .......... .......... .......... .......... .......... 94% 78.9M 0s 247250K .......... .......... .......... .......... .......... 94% 77.6M 0s 247300K .......... .......... .......... .......... .......... 94% 82.2M 0s 247350K .......... .......... .......... .......... .......... 94% 84.9M 0s 247400K .......... .......... .......... .......... .......... 94% 75.4M 0s 247450K .......... .......... .......... .......... .......... 94% 58.9M 0s 247500K .......... .......... .......... .......... .......... 94% 130M 0s 247550K .......... .......... .......... .......... .......... 94% 69.4M 0s 247600K .......... .......... .......... .......... .......... 94% 69.2M 0s 247650K .......... .......... .......... .......... .......... 94% 77.4M 0s 247700K .......... .......... .......... .......... .......... 94% 71.1M 0s 247750K .......... .......... .......... .......... .......... 94% 105M 0s 247800K .......... .......... .......... .......... .......... 94% 39.1M 0s 247850K .......... .......... .......... .......... .......... 94% 10.2M 0s 247900K .......... .......... .......... .......... .......... 94% 440M 0s 247950K .......... .......... .......... .......... .......... 94% 19.8M 0s 248000K .......... .......... .......... .......... .......... 94% 309M 0s 248050K .......... .......... .......... .......... .......... 94% 39.6M 0s 248100K .......... .......... .......... .......... .......... 94% 452M 0s 248150K .......... .......... .......... .......... .......... 94% 123M 0s 248200K .......... .......... .......... .......... .......... 94% 79.5M 0s 248250K .......... .......... .......... .......... .......... 94% 141M 0s 248300K .......... .......... .......... .......... .......... 94% 107M 0s 248350K .......... .......... .......... .......... .......... 94% 93.7M 0s 248400K .......... .......... .......... .......... .......... 94% 83.2M 0s 248450K .......... .......... .......... .......... .......... 94% 143M 0s 248500K .......... .......... .......... .......... .......... 94% 20.8M 0s 248550K .......... .......... .......... .......... .......... 94% 164M 0s 248600K .......... .......... .......... .......... .......... 94% 168M 0s 248650K .......... .......... .......... .......... .......... 94% 28.5M 0s 248700K .......... .......... .......... .......... .......... 94% 448M 0s 248750K .......... .......... .......... .......... .......... 94% 474M 0s 248800K .......... .......... .......... 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.......... 95% 94.3M 0s 249500K .......... .......... .......... .......... .......... 95% 118M 0s 249550K .......... .......... .......... .......... .......... 95% 102M 0s 249600K .......... .......... .......... .......... .......... 95% 74.8M 0s 249650K .......... .......... .......... .......... .......... 95% 134M 0s 249700K .......... .......... .......... .......... .......... 95% 139M 0s 249750K .......... .......... .......... .......... .......... 95% 92.5M 0s 249800K .......... .......... .......... .......... .......... 95% 131M 0s 249850K .......... .......... .......... .......... .......... 95% 79.1M 0s 249900K .......... .......... .......... .......... .......... 95% 79.0M 0s 249950K .......... .......... .......... .......... .......... 95% 190M 0s 250000K .......... .......... .......... .......... .......... 95% 145M 0s 250050K .......... .......... .......... .......... .......... 95% 107M 0s 250100K .......... .......... .......... .......... .......... 95% 8.90M 0s 250150K .......... .......... .......... .......... .......... 95% 303M 0s 250200K .......... .......... .......... .......... .......... 95% 414M 0s 250250K .......... .......... .......... .......... .......... 95% 29.9M 0s 250300K .......... .......... .......... .......... .......... 95% 126M 0s 250350K .......... .......... .......... .......... .......... 95% 161M 0s 250400K .......... .......... .......... .......... .......... 95% 43.9M 0s 250450K .......... .......... .......... .......... .......... 95% 107M 0s 250500K .......... .......... .......... .......... .......... 95% 114M 0s 250550K .......... .......... .......... .......... .......... 95% 126M 0s 250600K .......... .......... .......... .......... .......... 95% 53.8M 0s 250650K .......... .......... .......... .......... .......... 95% 174M 0s 250700K .......... .......... .......... .......... .......... 95% 152M 0s 250750K .......... .......... .......... .......... .......... 95% 43.1M 0s 250800K .......... 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.......... 96% 51.9M 0s 252800K .......... .......... .......... .......... .......... 96% 102M 0s 252850K .......... .......... .......... .......... .......... 96% 158M 0s 252900K .......... .......... .......... .......... .......... 96% 98.6M 0s 252950K .......... .......... .......... .......... .......... 96% 77.1M 0s 253000K .......... .......... .......... .......... .......... 96% 101M 0s 253050K .......... .......... .......... .......... .......... 96% 191M 0s 253100K .......... .......... .......... .......... .......... 96% 72.2M 0s 253150K .......... .......... .......... .......... .......... 96% 167M 0s 253200K .......... .......... .......... .......... .......... 96% 79.9M 0s 253250K .......... .......... .......... .......... .......... 96% 25.8M 0s 253300K .......... .......... .......... .......... .......... 96% 525M 0s 253350K .......... .......... .......... .......... .......... 96% 49.2M 0s 253400K .......... .......... .......... .......... .......... 96% 58.4M 0s 253450K .......... .......... .......... .......... .......... 96% 461M 0s 253500K .......... .......... .......... .......... .......... 96% 26.0M 0s 253550K .......... .......... .......... .......... .......... 96% 400M 0s 253600K .......... .......... .......... .......... .......... 96% 452M 0s 253650K .......... .......... .......... .......... .......... 96% 37.5M 0s 253700K .......... .......... .......... .......... .......... 96% 132M 0s 253750K .......... .......... .......... .......... .......... 96% 230M 0s 253800K .......... .......... .......... .......... .......... 96% 44.8M 0s 253850K .......... .......... .......... .......... .......... 96% 89.3M 0s 253900K .......... .......... .......... .......... .......... 96% 90.9M 0s 253950K .......... .......... .......... .......... .......... 96% 8.22M 0s 254000K .......... .......... .......... .......... .......... 96% 177M 0s 254050K .......... .......... .......... .......... .......... 96% 40.9M 0s 254100K 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262000K .......... .......... .......... .......... .......... 99% 92.3M 0s 262050K .......... .......... .......... .......... .......... 99% 77.4M 0s 262100K .......... .......... .......... .......... .......... 99% 73.5M 0s 262150K .......... .......... .......... .......... .......... 99% 97.7M 0s 262200K ........ 100% 380M=3.4s 2024-05-03 00:16:04 (75.8 MB/s) - ‘ESPbeta.tgz’ saved [268501958/268501958] + tar -xf ESPbeta.tgz + rm -rf EngSketchPad/data/Slugs + python --version Python 3.11.9 + [[ '' == *\.\i\f\o\r\t ]] + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/config/ + ./makeEnv ESP runtime AutoConfigurator CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 with contents: bin include lib share Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python found! Info: Python header /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found! Info: Python library /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.dylib found! ESP_ARCH = DARWIN_ARM64 ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad EFCOMP = gfortran CARCH = DARWIN_ARM64 CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 CASARCH = . CASREV = 7.8 PYTHONINC= /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 PYTHONLIB= -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 + source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/ESPenv.sh ++ export ESP_ARCH=DARWIN_ARM64 ++ ESP_ARCH=DARWIN_ARM64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASARCH=. ++ CASARCH=. ++ export CASREV=7.8 ++ CASREV=7.8 ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONINC=/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 ++ PYTHONINC=/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11' ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ export AFLR_ARCH=MacOSX-arm64 ++ AFLR_ARCH=MacOSX-arm64 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ export CAPS_GLYPH= ++ CAPS_GLYPH= ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/SLUGS/Slugs.html' ++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/SLUGS/Slugs.html' ++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/ESP/ESP.html' ++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/ESP/ESP.html' ++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/wvClient/wv.html' ++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/wvClient/wv.html' + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src + make (cd EGADS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64 rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64 cp -p ../include/DARWIN_ARM64 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/DARWIN_ARM64 touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads_dot.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads_dot.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.inc rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egads.inc touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/emp.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/emp.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/prm.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/prm.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.inc rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsserver.inc touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsss.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/wsss.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTris.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsTris.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/Surreal/always_inline.h clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsGeom.cpp -o ./egadsGeom.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsHLevel.cpp -o ./egadsHLevel.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTopo.cpp -o ./egadsTopo.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsCopy.cpp -o ./egadsCopy.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSpline.cpp -o ./egadsSpline.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsIO.cpp -o ./egadsIO.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSplineFit.cpp -o ./egadsSplineFit.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSkinning.cpp -o ./egadsSkinning.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTessSens.cpp -o ./egadsTessSens.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsBase.c -o ./egadsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o ./egadsMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTess.c -o ./egadsTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTris.c -o ./egadsTris.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o ./egadsQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsFit.c -o ./egadsFit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o ./egadsRobust.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o ./egadsSBO.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmCfit.c -o ./prmCfit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmGrid.c -o ./prmGrid.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmUV.c -o ./prmUV.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsExport.c -o ./egadsExport.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o ./egadsEffect.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o ./egadsSolids.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include ../util/emp.c \ -o ./emp.o clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/evaluate.c -o ./evaluate.o clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/rational.c -o ./rational.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \ ../util/regQuads.c -o ./regQuads.o clang++ -g -target arm64-apple-darwin -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp ./SurrealD1 SurrealD1_test_suite Complete! clang++ -g -target arm64-apple-darwin -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp ./SurrealD4 SurrealD4_test_suite Complete! clang++ -g -target arm64-apple-darwin -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp ./SurrealS1 SurrealS1_test_suite Complete! clang++ -g -target arm64-apple-darwin -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp ./SurrealS4 SurrealS4_test_suite Complete! /Library/Developer/CommandLineTools/usr/bin/make -C ../util clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \ -o ./uvmap.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 egadsUVmap.c -Iuvmap \ -o ./egadsUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a clang -g -target arm64-apple-darwin -o ./uvmap.exe ./uvmap.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib (cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \ egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.8 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a (cd .; \ ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \ evaluate.o rational.o regQuads.o; ) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsBase.c -o ./fgadsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsMemory.c -o ./fgadsMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsAttrs.c -o ./fgadsAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTess.c -o ./fgadsTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsHLevel.c -o ./fgadsHLevel.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsGeom.c -o ./fgadsGeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTopo.c -o ./fgadsTopo.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libfgads.a touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libemp.a *** EGADS Build Complete! *** (cd EGADS/lite; make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteBase.c -o ./liteBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteMemory.c -o ./liteMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteGeom.c -o ./liteGeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteTopo.c -o ./liteTopo.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteAttrs.c -o ./liteAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteImport.c -o ./liteImport.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteString.c -o ./liteString.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o ./liteTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o ./liteTris.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src \ ../src/egadsQuads.c -o ./liteQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o ./liteTessInp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 ../src/egadsRobust.c \ -o ./egadsRobust.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DDARWIN_ARM64 -I../include ../util/emp.c \ -o ./emp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o ./evaLite.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE ../util/rational.c \ -o ./ratLite.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I../util \ ../util/regQuads.c -o ./liteRegQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o ./liteEffect.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o ./liteUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib (cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslite.dylib \ liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \ egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \ liteEffect.o liteUVmap.o \ -install_name '@rpath/libegadslite.dylib' \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \ liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \ emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \ liteUVmap.o ; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libegadslitestatic.a (cd wvServer; make) clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict map.cpp -o ./map.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include base64-decode.c -o ./base64-decode.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include handshake.c -o ./handshake.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include client-handshake.c -o ./client-handshake.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include md5.c -o ./md5.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include parsers.c -o ./parsers.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include extension.c -o ./extension.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include sha-1.c -o ./sha-1.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include server.c -o ./server.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include wv.c -o ./wv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include browserMessage.c -o ./browserMessage.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fwv.c -o ./fwv.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \ ./fwv.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \ -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -o ./servertest.o clang++ -g -target arm64-apple-darwin -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib (cd .; clang++ -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libwsserver.dylib \ base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \ -install_name '@rpath/libwsserver.dylib' \ -compatibility_version 7.8 \ -current_version 1.0.25 ) (cd EGADS/examples; make -f egads2cart.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include egads2cart.c \ -o ./egads2cart.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm (cd EGADS/examples; make -f vCurvature.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vCurvature.c -o ./vCurvature.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vCurvature ./vCurvature.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd EGADS/examples; make -f vGeom.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vGeom.c -o ./vGeom.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd EGADS/examples; make -f vTess.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vTess.c -o ./vTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include ../util/retessFaces.c \ -o ./retessFaces.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd OpenCSM; make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udp.c -o ./udp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. tim.c -o ./tim.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25 clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bezier.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bezier.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/biconvex.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/biconvex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/box.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/box.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bspline.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bspline.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/catmull.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/catmull.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/compare.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/compare.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createBEM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createBEM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createPoly.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createPoly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/csm.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/csm.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/deform.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/deform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/droop.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/droop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/editAttr.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/editAttr.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ellipse.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ellipse.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flend.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flend.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/freeform.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/freeform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ganged.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ganged.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/guide.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/guide.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hex.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/import.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/import.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/kulfan.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/kulfan.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/linalg.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/linalg.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mechanism.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mechanism.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nacelle.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nacelle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nuscale.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nuscale.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/offset.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/offset.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parsec.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parsec.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pod.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pod.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/poly.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/poly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBbox.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBbox.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBrep.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBrep.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printEgo.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printEgo.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/prop.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/prop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/radwaf.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/radwaf.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sample.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sample.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sew.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sew.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/shadow.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/shadow.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slices.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slices.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stag.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stag.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stiffener.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stiffener.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/supell.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/supell.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester1.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester1.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester2.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vsp3.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vsp3.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/waffle.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/waffle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/warp.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/warp.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/warp.so ./udpWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/PDT2.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/PDT2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J . touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca456.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads -lm -static-libgfortran -static-libgcc -Wl,-w clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ereped.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ereped.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mitten.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mitten.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plotter.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plotter.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plugs.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slugs.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/common.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/common.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udp.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udp.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/esp.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/esp.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/tim.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/tim.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egg.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/egg.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/udpUtilities.c (cd Slugs; make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. Fitter.c \ -o ./Fitter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. RedBlackTree.c \ -o ./RedBlackTree.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. Tessellate.c \ -o ./Tessellate.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \ ./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lwsserver -legads \ -lpthread -lz -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads \ -lpthread -lz -lm (cd CAPS; make) /bin/cp Cart3D/M1_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libc3dio.a /bin/cp Cart3D/M1_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libCart3D.a /bin/cp Executables/DARWIN_ARM64/avl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/avl /bin/cp Executables/DARWIN_ARM64/pplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/pplot /bin/cp Executables/DARWIN_ARM64/pxplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/pxplot /bin/cp Executables/DARWIN_ARM64/xfoil /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/xfoil /bin/cp Executables/DARWIN_ARM64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/mastros.exe /bin/cp Executables/DARWIN_ARM64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/ASTRO.D01 /bin/cp Executables/DARWIN_ARM64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/ASTRO.IDX /bin/cp Executables/DARWIN_ARM64/mses /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/mses /bin/cp Executables/DARWIN_ARM64/mset /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/mset /bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include /bin/cp udunits/DARWIN_ARM64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib /bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libudunits2.dylib /bin/cp Libraries/DARWIN_ARM64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/aflr2AIM.so /bin/cp Libraries/DARWIN_ARM64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/aflr3AIM.so /bin/cp Libraries/DARWIN_ARM64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/aflr4AIM.so (cd CAPS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/caps.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/caps.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/capsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimUtil.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimUtil.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimMesh.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aimMesh.h clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../include \ -I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o ./aimTransferUtil.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../include \ aimMesh.c -o ./aimMesh.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \ ./aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libaimUtil.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsBase.c -o ./capsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsBound.c -o ./capsBound.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsValue.c -o ./capsValue.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. \ -I/usr/include/udunits2 printObject.c -o ./printObject.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib (cd .; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \ -install_name '@rpath/libcaps.dylib' \ -compatibility_version 1.0.25 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libcapsstatic.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include testingAIM.c \ -o ./testingAIM.o rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include testingWriter.c \ -o ./testingWriter.o rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include phaseUtil.c \ -o ./phaseUtil.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm (cd ../CAPSexamples; make) (make -C cCAPS -f aeroelastic_SU2.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o clang -g -target arm64-apple-darwin -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include avlTest.c -o ./avlTest.o clang -g -target arm64-apple-darwin -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include awaveTest.c -o ./awaveTest.o clang -g -target arm64-apple-darwin -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include frictionTest.c -o ./frictionTest.o clang -g -target arm64-apple-darwin -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o clang -g -target arm64-apple-darwin -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o clang -g -target arm64-apple-darwin -o ./fun3dTetgenTest ./fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o clang -g -target arm64-apple-darwin -o ./aeroelasticTest ./aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmTest.c -o ./hsmTest.o clang -g -target arm64-apple-darwin -o ./hsmTest ./hsmTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o clang -g -target arm64-apple-darwin -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o clang -g -target arm64-apple-darwin -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o clang -g -target arm64-apple-darwin -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include interferenceTest.c \ -o ./interferenceTest.o clang -g -target arm64-apple-darwin -o ./interferenceTest ./interferenceTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include msesTest.c -o ./msesTest.o clang -g -target arm64-apple-darwin -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include mystranTest.c -o ./mystranTest.o clang -g -target arm64-apple-darwin -o ./mystranTest ./mystranTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o clang -g -target arm64-apple-darwin -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd CAPS/aim; make) /Library/Developer/CommandLineTools/usr/bin/make -C utils clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libutils.a mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/aim/utils/vlmUtils.h /Library/Developer/CommandLineTools/usr/bin/make -C abaqus clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \ abaqusAIM.c -o ./abaqusAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \ abaqusUtils.c -o ./abaqusUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \ -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o echo "Building Abaqus with Python" Building Abaqus with Python clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib /Library/Developer/CommandLineTools/usr/bin/make -C aflr2 Not compiling aflr2AIM: AFLR must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C aflr3 Not compiling aflr3AIM: AFLR must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C aflr4 Not compiling aflr4AIM: AFLR must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C astros clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils astrosAIM.c \ -o ./astrosAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils astrosUtils.c \ -o ./astrosUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils astrosCards.c \ -o ./astrosCards.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C avl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C awave clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils awaveAIM.c \ -o ./awaveAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C cart3d clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/libCart3D -I./xddm \ cart3dAIM.c -o ./cart3dAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/libCart3D -I./xddm \ writeTrix.c -o ./writeTrix.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/libCart3D \ surfTrix.c -o ./surfTrix.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -pedantic -I./xddm -I. \ `xml2-config --cflags` ./xddm/xddm.c \ -o ./xddm.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include bodyTess.c -o ./bodyTess.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \ ./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/ \ -lc3dio -lCart3D -ldl -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include cart3dTest.c \ -o ./cart3dTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I./xddm \ -I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \ ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm /Library/Developer/CommandLineTools/usr/bin/make -C cbaero clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o clang -g -target arm64-apple-darwin -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C cgt clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include egads2cgt.c \ -o ./egads2cgt.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include aflr4egads.c \ -o ./aflr4egads.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C custom make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C delaundo clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils delaundoAIM.c \ -o ./delaundoAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C egadsTess clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils egadsTessAIM.c \ -o ./egadsTessAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C friction clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils frictionAIM.c \ -o ./frictionAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o gfortran -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/friction ./friction.o -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C fun3d clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \ -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \ fun3dUtils.c -o ./fun3dUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \ -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o Building FUN3D with Python clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \ ./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib /Library/Developer/CommandLineTools/usr/bin/make -C hsm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hsmAIM.c \ -o src/hsmAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hsmUtils.c \ -o src/hsmUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hsmAdj.c \ -o src/hsmAdj.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \ -o src/rcm.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict rcm/genrcmi.cpp -DREVISION=7.8 \ -o src/genrcmi.o /Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o /Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o /Library/Developer/CommandLineTools/usr/bin/make -C src cross.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o /Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o /Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o /Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/hsmAIM.so \ src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \ src/rcm.o src/genrcmi.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C interference clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include interferenceAIM.c \ -o ./interferenceAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. cloudFns.c \ -o ./cloudFns.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/interferenceAIM.so \ ./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C masstran clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils masstranAIM.cpp \ -o ./masstranAIM.o clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C meshWriter /Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include bstlWriter.c \ -o ./bstlWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include bvtkWriter.c \ -o ./bvtkWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include exodusWriter.cpp \ -o ./exodusWriter.o clang++ -g -target arm64-apple-darwin -bundle -std=c++11 -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/exodusWriter.so ./exodusWriter.o \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C fastWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include fastWriter.c \ -o ./fastWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include libmeshbWriter.c \ -o ./libmeshbWriter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C stlWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include stlWriter.c \ -o ./stlWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include su2Writer.c \ -o ./su2Writer.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include tecplotWriter.c \ -o ./tecplotWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include ugridWriter.c \ -o ./ugridWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include vtkWriter.c \ -o ./vtkWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C mses clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C mystran clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils mystranAIM.c \ -o ./mystranAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils mystranUtils.c \ -o ./mystranUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C nastran clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils nastranAIM.c \ -o ./nastranAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C plato clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include platoAIM.c \ -o ./platoAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/platoAIM.so ./platoAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C pointwise clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils pointwiseAIM.c \ -o ./pointwiseAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils hashElement.c \ -o ./hashElement.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -lpthread /Library/Developer/CommandLineTools/usr/bin/make -C refine clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \ -o ./refineAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 \ -I../meshWriter/libmeshbWriter/libMeshb/sources \ ../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C sierraSD clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSDAIM.c \ -o ./sierraSDAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sierraSDAIM.so ./sierraSDAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C sierraSM clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSMAIM.c \ -o ./sierraSMAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/sierraSMAIM.so ./sierraSMAIM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C skeleton clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils skeletonAIM.c \ -o ./skeletonAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C spinnaker clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include \ -I../meshWriter/exodusWriter \ -I../meshWriter/libmeshbWriter \ -I../utils -I/Users/jenkins/util/sandialabs/seacas/include \ -I/opt/homebrew/include \ spinnakerAIM.c \ -o ./spinnakerAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 \ -I../meshWriter/libmeshbWriter/libMeshb/sources \ ../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/spinnakerAIM.so ./spinnakerAIM.o ./libmeshb7.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib \ -L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2 clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \ -o ./su2AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2Utils.c \ -o ./su2Utils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_4_Cardinal.c \ -o ./su2_4_Cardinal.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_5_Raven.c \ -o ./su2_5_Raven.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_6_Falcon.c \ -o ./su2_6_Falcon.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_7_Blackbird.c \ -o ./su2_7_Blackbird.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils su2_801_Harrier.c \ -o ./su2_801_Harrier.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C tacs clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils tacsAIM.c \ -o ./tacsAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C tetgen clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils tetgenAIM.cpp \ -o ./tetgenAIM.o clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \ -DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \ ./tetgen_Interface.o ./tetgen.o \ ./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tsfoil clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \ tsfoilAIM.c -o ./tsfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C unitTest make[2]: Nothing to be done for `all'. /Library/Developer/CommandLineTools/usr/bin/make -C xfoil clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils \ xfoilAIM.c -o ./xfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C zaero clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl (cd OpenCSM; make -f serveESP.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/capsMode.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/capsMode.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flowchart.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flowchart.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/viewer.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/viewer.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/include -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pyscript.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pyscript.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib *** Build Completed! *** + export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data + CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin ++ uname -a + [[ Darwin VIGGEN.MIT.EDU 23.3.0 Darwin Kernel Version 23.3.0: Wed Dec 20 21:30:27 PST 2023; root:xnu-10002.81.5~7/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]] + sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/Verification.sh + bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/Verification.sh + expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/expressions + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/expressions WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set) ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set) ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set) ==> serveESP completed successfully with no verification data real 0m0.468s user 0m0.188s sys 0m0.011s + set +x ============================================= ESP verification case 01 passed (as expected) ============================================= + expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/demo2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/demo2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.375s user 0m0.390s sys 0m0.044s + set +x ============================================= ESP verification case 02 passed (as expected) ============================================= + expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial1_whole WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m2.218s user 0m2.879s sys 0m0.321s + set +x ============================================= ESP verification case 03 passed (as expected) ============================================= + expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.501s user 0m0.514s sys 0m0.039s + set +x ============================================= ESP verification case 04 passed (as expected) ============================================= + expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/design3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.594s user 0m0.660s sys 0m0.023s + set +x ============================================= ESP verification case 05 passed (as expected) ============================================= + expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.534s user 0m0.642s sys 0m0.024s + set +x ============================================= ESP verification case 06 passed (as expected) ============================================= + expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/tutorial3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m3.101s user 0m4.487s sys 0m0.301s + set +x ============================================= ESP verification case 07 passed (as expected) ============================================= + expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/CAPS/myPlane WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped ==> serveESP completed successfully with 12 warnings and no verification data real 0m24.924s user 0m36.412s sys 0m1.142s + set +x ============================================= ESP verification case 08 passed (as expected) ============================================= + expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/bottle + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/bottle WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.574s user 0m0.602s sys 0m0.019s + set +x ============================================= ESP verification case 09 passed (as expected) ============================================= + expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/wingMultiModel WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped ==> serveESP completed successfully with 4 warnings and no verification data real 0m33.951s user 0m54.807s sys 0m12.748s + set +x ============================================= ESP verification case 10 passed (as expected) ============================================= + expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/bullet + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/bullet WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped WARNING:: 8 _hist and/or __trace__ attributes removed WARNING:: 8 _hist and/or __trace__ attributes removed ==> serveESP completed successfully with 1 warnings and no verification data real 0m0.436s user 0m0.356s sys 0m0.021s + set +x ============================================= ESP verification case 11 passed (as expected) ============================================= + expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/connect5 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/connect5 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.603s user 0m0.798s sys 0m0.012s + set +x ============================================= ESP verification case 12 passed (as expected) ============================================= + expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/group2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/group2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.248s user 0m0.266s sys 0m0.010s + set +x ============================================= ESP verification case 13 passed (as expected) ============================================= + expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/csm3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/csm3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped nnode=8 nedge=12 nface=6 nnode=8 nedge=12 nface=6 nnode=16 nedge=24 nface=10 nnode=8 nedge=12 nface=6 ==> serveESP completed successfully with no verification data real 0m0.471s user 0m0.494s sys 0m0.018s + set +x ============================================= ESP verification case 14 passed (as expected) ============================================= + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP/testEGADS + make test python --version Python 3.11.9 python -u -m unittest discover .................................................... PCurve Map: 48 (alloc 48)! Surface Map: 12 (alloc 24)! Curve Map: 28 (alloc 28)! Writing PCurves... Writing Curves... Writing Surfaces... Writing 16 Nodes... Writing 28 Edges... Writing 12 Loops... Writing 12 Faces... Writing 1 Shells... EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close! ................... ---------------------------------------------------------------------- Ran 71 tests in 1.899s OK + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP/testOCSM + source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/test_pyOCSM.sh ++ set -x ++ python -u test_pyOCSM.py -skipHelp real 0m5.403s user 0m7.469s sys 0m0.143s ++ set +x ================================================= test_pyOCSM.py passed (as expected) ================================================= + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/pyESP/testCAPS + make test python --version Python 3.11.9 python -u -m unittest discover .. Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 143 Number of elements = 282 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 282 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 155 Number of elements = 306 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 306 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 298 Combined Number of elements = 588 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 588 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input .. . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ..Writing D3 Javascript library - d3.v3.min.js ........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 209 Number of elements = 414 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 414 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 186 Number of elements = 368 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 368 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 395 Combined Number of elements = 782 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 782 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Wing1 Property name - Wing2 Done getting FEA properties Updating mesh element types based on properties input . . .. . .. ...--> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . . EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! ..Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha No linkable data found for Altitude No linkable data found for Strings No linkable data found for Strings2 Linked Parameter Beta to analysis su2 input Beta Linked Parameter Alpha to analysis su2 input Alpha ............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . CAPS Info: Hit last success -- going live! ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> _body (EG_attributeDel)! EGADS Error: No Attribute -> _nface (EG_attributeDel)! EGADS Error: No Attribute -> __trace__ (EG_attributeDel)! EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! .--> Opening DESPMTR file "unitGeom.param" updating CFGPMTR series [ 1, 1] = 8412.000000 updating CFGPMTR series2 [ 1, 1] = 20.000000 updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000 updating CFGPMTR nrow [ 1, 1] = 3.000000 updating CFGPMTR ncol [ 1, 1] = 2.000000 updating DESPMTR area [ 1, 1] = 40.000000 updating DESPMTR aspect [ 1, 1] = 5.000000 updating DESPMTR taper [ 1, 1] = 0.500000 updating DESPMTR twist [ 1, 1] = 15.000000 updating DESPMTR wing:lesweep [ 1, 1] = 30.000000 updating DESPMTR wing:dihedral [ 1, 1] = 1.000000 updating DESPMTR wing:chord:root [ 1, 1] = 1.560000 updating DESPMTR htail [ 1, 1] = 1.000000 updating DESPMTR htail:chord [ 1, 1] = 2.000000 updating DESPMTR vtail:chord [ 1, 1] = 3.000000 updating DESPMTR vtail [ 1, 1] = 4.000000 updating DESPMTR sphereR [ 1, 1] = 80.000000 updating DESPMTR v@1:d_name [ 1, 1] = 1.000000 updating DESPMTR despMat [ 1, 1] = 11.000000 updating DESPMTR despMat [ 1, 2] = 12.000000 updating DESPMTR despMat [ 2, 1] = 13.000000 updating DESPMTR despMat [ 2, 2] = 14.000000 updating DESPMTR despMat [ 3, 1] = 15.000000 updating DESPMTR despMat [ 3, 2] = 16.000000 updating DESPMTR despCol [ 1, 1] = 11.000000 updating DESPMTR despCol [ 2, 1] = 13.000000 updating DESPMTR despCol [ 3, 1] = 15.000000 updating DESPMTR despRow [ 1, 1] = 11.000000 updating DESPMTR despRow [ 1, 2] = 12.000000 updating DESPMTR despRow [ 1, 3] = 13.000000 ERROR:: DESPMTR file "unitGeom.param" not found CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ---------------------------------------------------------------------- Ran 100 tests in 17.085s OK WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/ + make test python --version Python 3.11.9 python -u -m unittest discover --verbose test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.028 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.061 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.014 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4120 6016 AFLR2 GG : Nodes, Faces = 5820 9416 AFLR2 GG : Nodes, Faces = 7322 12420 AFLR2 GG : Nodes, Faces = 8613 15002 AFLR2 GG : Nodes, Faces = 9793 17362 AFLR2 GG : Nodes, Faces = 10847 19470 AFLR2 GG : Nodes, Faces = 11828 21432 AFLR2 GG : Nodes, Faces = 12749 23274 AFLR2 GG : Nodes, Faces = 13580 24936 AFLR2 GG : Nodes, Faces = 14355 26486 AFLR2 GG : Nodes, Faces = 15088 27952 AFLR2 GG : Nodes, Faces = 15774 29324 AFLR2 GG : Nodes, Faces = 16420 30616 AFLR2 GG : Nodes, Faces = 17013 31802 AFLR2 GG : Nodes, Faces = 17571 32918 AFLR2 GG : Nodes, Faces = 18089 33954 AFLR2 GG : Nodes, Faces = 18573 34922 AFLR2 GG : Nodes, Faces = 19005 35786 AFLR2 GG : Nodes, Faces = 19413 36602 AFLR2 GG : Nodes, Faces = 19779 37334 AFLR2 GG : Nodes, Faces = 20116 38008 AFLR2 GG : Nodes, Faces = 20443 38662 AFLR2 GG : Nodes, Faces = 20756 39288 AFLR2 GG : Nodes, Faces = 21054 39884 AFLR2 GG : Nodes, Faces = 21344 40464 AFLR2 GG : Nodes, Faces = 21621 41018 AFLR2 GG : Nodes, Faces = 21885 41546 AFLR2 GG : Nodes, Faces = 22137 42050 AFLR2 GG : Nodes, Faces = 22387 42550 AFLR2 GG : Nodes, Faces = 22603 42982 AFLR2 GG : Nodes, Faces = 22772 43320 AFLR2 GG : Nodes, Faces = 22912 43600 AFLR2 GG : Nodes, Faces = 23039 43854 AFLR2 GG : Nodes, Faces = 23142 44060 AFLR2 GG : Nodes, Faces = 23205 44186 AFLR2 GG : Nodes, Faces = 23240 44256 AFLR2 GG : Nodes, Faces = 23257 44290 AFLR2 GG : Nodes, Faces = 23269 44314 AFLR2 GG : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.045 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23273 Number of elements = 46546 Number of tris = 44322 Number of quad = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.024 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.057 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.011 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.041 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4120 6016 AFLR2 GG : Nodes, Faces = 5820 9416 AFLR2 GG : Nodes, Faces = 7322 12420 AFLR2 GG : Nodes, Faces = 8613 15002 AFLR2 GG : Nodes, Faces = 9793 17362 AFLR2 GG : Nodes, Faces = 10847 19470 AFLR2 GG : Nodes, Faces = 11828 21432 AFLR2 GG : Nodes, Faces = 12749 23274 AFLR2 GG : Nodes, Faces = 13580 24936 AFLR2 GG : Nodes, Faces = 14355 26486 AFLR2 GG : Nodes, Faces = 15088 27952 AFLR2 GG : Nodes, Faces = 15774 29324 AFLR2 GG : Nodes, Faces = 16420 30616 AFLR2 GG : Nodes, Faces = 17013 31802 AFLR2 GG : Nodes, Faces = 17571 32918 AFLR2 GG : Nodes, Faces = 18089 33954 AFLR2 GG : Nodes, Faces = 18573 34922 AFLR2 GG : Nodes, Faces = 19005 35786 AFLR2 GG : Nodes, Faces = 19413 36602 AFLR2 GG : Nodes, Faces = 19779 37334 AFLR2 GG : Nodes, Faces = 20116 38008 AFLR2 GG : Nodes, Faces = 20443 38662 AFLR2 GG : Nodes, Faces = 20756 39288 AFLR2 GG : Nodes, Faces = 21054 39884 AFLR2 GG : Nodes, Faces = 21344 40464 AFLR2 GG : Nodes, Faces = 21621 41018 AFLR2 GG : Nodes, Faces = 21885 41546 AFLR2 GG : Nodes, Faces = 22137 42050 AFLR2 GG : Nodes, Faces = 22387 42550 AFLR2 GG : Nodes, Faces = 22603 42982 AFLR2 GG : Nodes, Faces = 22772 43320 AFLR2 GG : Nodes, Faces = 22912 43600 AFLR2 GG : Nodes, Faces = 23039 43854 AFLR2 GG : Nodes, Faces = 23142 44060 AFLR2 GG : Nodes, Faces = 23205 44186 AFLR2 GG : Nodes, Faces = 23240 44256 AFLR2 GG : Nodes, Faces = 23257 44290 AFLR2 GG : Nodes, Faces = 23269 44314 AFLR2 GG : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.053 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23273 44322 AFLR2 : CPU Time = 0.008 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23273 Number of elements = 46546 Number of tris = 44322 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 ok test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.022 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4285 6326 AFLR2 GG : Nodes, Faces = 6135 10026 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9485 16726 AFLR2 GG : Nodes, Faces = 10981 19718 AFLR2 GG : Nodes, Faces = 12372 22500 AFLR2 GG : Nodes, Faces = 13686 25128 AFLR2 GG : Nodes, Faces = 14908 27572 AFLR2 GG : Nodes, Faces = 16063 29882 AFLR2 GG : Nodes, Faces = 17170 32096 AFLR2 GG : Nodes, Faces = 18222 34200 AFLR2 GG : Nodes, Faces = 19208 36172 AFLR2 GG : Nodes, Faces = 20165 38086 AFLR2 GG : Nodes, Faces = 21087 39930 AFLR2 GG : Nodes, Faces = 21975 41706 AFLR2 GG : Nodes, Faces = 22803 43362 AFLR2 GG : Nodes, Faces = 23582 44920 AFLR2 GG : Nodes, Faces = 24330 46416 AFLR2 GG : Nodes, Faces = 25041 47838 AFLR2 GG : Nodes, Faces = 25723 49202 AFLR2 GG : Nodes, Faces = 26365 50486 AFLR2 GG : Nodes, Faces = 26993 51742 AFLR2 GG : Nodes, Faces = 27556 52868 AFLR2 GG : Nodes, Faces = 28054 53864 AFLR2 GG : Nodes, Faces = 28487 54730 AFLR2 GG : Nodes, Faces = 28847 55450 AFLR2 GG : Nodes, Faces = 29118 55992 AFLR2 GG : Nodes, Faces = 29355 56466 AFLR2 GG : Nodes, Faces = 29553 56862 AFLR2 GG : Nodes, Faces = 29735 57226 AFLR2 GG : Nodes, Faces = 29878 57512 AFLR2 GG : Nodes, Faces = 29969 57694 AFLR2 GG : Nodes, Faces = 30009 57774 AFLR2 GG : Nodes, Faces = 30018 57792 AFLR2 GG : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.055 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 30019 57794 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 30019 Number of elements = 60038 Number of tris = 57794 Number of quad = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 48 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 10 22 AFLR2 IG : Nodes, Faces = 20 42 AFLR2 IG : Nodes, Faces = 30 62 AFLR2 IG : Nodes, Faces = 40 82 AFLR2 IG : Nodes, Faces = 45 92 AFLR2 IG : Nodes, Faces = 46 94 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 98 AFLR2 IG : Nodes, Faces = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 48 48 AFLR2 GG : Nodes, Faces = 88 128 AFLR2 GG : Nodes, Faces = 109 170 AFLR2 GG : Nodes, Faces = 124 200 AFLR2 GG : Nodes, Faces = 136 224 AFLR2 GG : Nodes, Faces = 148 248 AFLR2 GG : Nodes, Faces = 160 272 AFLR2 GG : Nodes, Faces = 172 296 AFLR2 GG : Nodes, Faces = 182 316 AFLR2 GG : Nodes, Faces = 188 328 AFLR2 GG : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 190 Number of elements = 380 Number of tris = 332 Number of quad = 0 ok test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 344 344 AFLR2 GG : Nodes, Faces = 679 1014 AFLR2 GG : Nodes, Faces = 1006 1668 AFLR2 GG : Nodes, Faces = 1321 2298 AFLR2 GG : Nodes, Faces = 1604 2864 AFLR2 GG : Nodes, Faces = 1886 3428 AFLR2 GG : Nodes, Faces = 2155 3966 AFLR2 GG : Nodes, Faces = 2409 4474 AFLR2 GG : Nodes, Faces = 2649 4954 AFLR2 GG : Nodes, Faces = 2867 5390 AFLR2 GG : Nodes, Faces = 3063 5782 AFLR2 GG : Nodes, Faces = 3243 6142 AFLR2 GG : Nodes, Faces = 3400 6456 AFLR2 GG : Nodes, Faces = 3540 6736 AFLR2 GG : Nodes, Faces = 3665 6986 AFLR2 GG : Nodes, Faces = 3786 7228 AFLR2 GG : Nodes, Faces = 3900 7456 AFLR2 GG : Nodes, Faces = 4010 7676 AFLR2 GG : Nodes, Faces = 4114 7884 AFLR2 GG : Nodes, Faces = 4209 8074 AFLR2 GG : Nodes, Faces = 4292 8240 AFLR2 GG : Nodes, Faces = 4368 8392 AFLR2 GG : Nodes, Faces = 4439 8534 AFLR2 GG : Nodes, Faces = 4503 8662 AFLR2 GG : Nodes, Faces = 4560 8776 AFLR2 GG : Nodes, Faces = 4611 8878 AFLR2 GG : Nodes, Faces = 4650 8956 AFLR2 GG : Nodes, Faces = 4677 9010 AFLR2 GG : Nodes, Faces = 4695 9046 AFLR2 GG : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.005 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.001 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4705 Number of elements = 9410 Number of tris = 9066 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing FAST file .... Finished writing FAST file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing exodus file .... Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Block: 'Block1_tri', blk_id 1, num_entries 9066 Sideset: 'Airfoil', set_id 1, num_entries 198 Sideset: 'InFlow', set_id 2, num_entries 24 Sideset: 'OutFlow', set_id 3, num_entries 24 Sideset: 'TunnelWall', set_id 4, num_entries 98 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.014 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.009 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing exodus file .... Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Block: 'Block1_tri', blk_id 1, num_entries 386 Block: 'Block2_quad', blk_id 2, num_entries 3690 Sideset: 'Airfoil', set_id 1, num_entries 198 Sideset: 'InFlow', set_id 2, num_entries 24 Sideset: 'OutFlow', set_id 3, num_entries 24 Sideset: 'TunnelWall', set_id 4, num_entries 98 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.006 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Tecplot file .... Finished writing Tecplot file ok test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1198 Number of elements = 6307 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4975 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 6226 Number of elements = 34532 Number of triangles = 4438 Number of quadrilatarals = 0 Number of tetrahedrals = 30094 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 13688 Number of elements = 76798 Number of triangles = 8142 Number of quadrilatarals = 0 Number of tetrahedrals = 68656 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 41861 Number of elements = 237846 Number of triangles = 19888 Number of quadrilatarals = 0 Number of tetrahedrals = 217958 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 4339 Number of elements = 24073 Number of triangles = 3010 Number of quadrilatarals = 0 Number of tetrahedrals = 21063 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 11025 Number of elements = 60915 Number of triangles = 8632 Number of quadrilatarals = 0 Number of tetrahedrals = 52283 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 10398 Number of elements = 58234 Number of triangles = 6366 Number of quadrilatarals = 0 Number of tetrahedrals = 51868 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 88735 Number of elements = 498705 Number of triangles = 51808 Number of quadrilatarals = 0 Number of tetrahedrals = 446897 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16607 Number of elements = 94482 Number of triangles = 7926 Number of quadrilatarals = 0 Number of tetrahedrals = 86556 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2585 Number of elements = 13784 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3615 Number of elements = 19589 Number of triangles = 3392 Number of quadrilatarals = 0 Number of tetrahedrals = 16197 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5438 Number of elements = 30214 Number of triangles = 3654 Number of quadrilatarals = 0 Number of tetrahedrals = 26560 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4697 Number of elements = 26013 Number of triangles = 3324 Number of quadrilatarals = 0 Number of tetrahedrals = 22689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5467 Number of elements = 30346 Number of triangles = 3754 Number of quadrilatarals = 0 Number of tetrahedrals = 26592 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2273 Number of elements = 12220 Number of triangles = 2222 Number of quadrilatarals = 0 Number of tetrahedrals = 9998 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2405 Number of elements = 12664 Number of triangles = 2666 Number of quadrilatarals = 0 Number of tetrahedrals = 9998 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3357 Number of elements = 18188 Number of triangles = 3110 Number of quadrilatarals = 0 Number of tetrahedrals = 15078 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3622 Number of elements = 19080 Number of triangles = 4002 Number of quadrilatarals = 0 Number of tetrahedrals = 15078 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4425 Number of elements = 24045 Number of triangles = 4000 Number of quadrilatarals = 0 Number of tetrahedrals = 20045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4822 Number of elements = 25381 Number of triangles = 5336 Number of quadrilatarals = 0 Number of tetrahedrals = 20045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 4): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 4): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 4): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 4): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5483 Number of elements = 29853 Number of triangles = 4890 Number of quadrilatarals = 0 Number of tetrahedrals = 24963 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6012 Number of elements = 31633 Number of triangles = 6670 Number of quadrilatarals = 0 Number of tetrahedrals = 24963 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6555 Number of elements = 35742 Number of triangles = 5780 Number of quadrilatarals = 0 Number of tetrahedrals = 29962 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7216 Number of elements = 37966 Number of triangles = 8004 Number of quadrilatarals = 0 Number of tetrahedrals = 29962 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 6): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 6): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 6): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 6): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 6): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 6): Number of nodes = 1204 Number of elements = 6333 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4999 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7634 Number of elements = 41677 Number of triangles = 6670 Number of quadrilatarals = 0 Number of tetrahedrals = 35007 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8427 Number of elements = 44345 Number of triangles = 9338 Number of quadrilatarals = 0 Number of tetrahedrals = 35007 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 1204 Number of elements = 6333 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4999 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 1211 Number of elements = 6379 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19879 Number of elements = 110275 Number of triangles = 15558 Number of quadrilatarals = 0 Number of tetrahedrals = 94717 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 8 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 9 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 10 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 11 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 12 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 13 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 14 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 15 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 16 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 17 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 18 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 19 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22822 Number of elements = 120055 Number of triangles = 25338 Number of quadrilatarals = 0 Number of tetrahedrals = 94717 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 19): Number of nodes = 1212 Number of elements = 6382 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 19): Number of nodes = 1193 Number of elements = 6282 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 19): Number of nodes = 1217 Number of elements = 6416 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5080 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 19): Number of nodes = 1200 Number of elements = 6301 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4967 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 19): Number of nodes = 1190 Number of elements = 6252 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4918 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 19): Number of nodes = 1204 Number of elements = 6333 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4999 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 19): Number of nodes = 1211 Number of elements = 6379 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5045 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 8 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 8 (of 19): Number of nodes = 1220 Number of elements = 6413 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5077 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 9 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 9 (of 19): Number of nodes = 1214 Number of elements = 6396 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5060 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 10 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 10 (of 19): Number of nodes = 1192 Number of elements = 6262 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4930 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 11 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 11 (of 19): Number of nodes = 1201 Number of elements = 6326 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4994 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 12 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 12 (of 19): Number of nodes = 1206 Number of elements = 6356 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5022 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 13 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 13 (of 19): Number of nodes = 1187 Number of elements = 6236 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4904 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 14 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 14 (of 19): Number of nodes = 1197 Number of elements = 6293 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 15 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 15 (of 19): Number of nodes = 1180 Number of elements = 6202 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4870 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 16 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 16 (of 19): Number of nodes = 1197 Number of elements = 6289 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4957 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 17 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 17 (of 19): Number of nodes = 1208 Number of elements = 6351 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 18 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 18 (of 19): Number of nodes = 1193 Number of elements = 6277 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4945 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 19 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 19 (of 19): Number of nodes = 1200 Number of elements = 6309 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 4975 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8499 Number of elements = 47040 Number of triangles = 6258 Number of quadrilatarals = 0 Number of tetrahedrals = 40782 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8631 Number of elements = 47484 Number of triangles = 6702 Number of quadrilatarals = 0 Number of tetrahedrals = 40782 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 7444 Number of elements = 41254 Number of triangles = 5370 Number of quadrilatarals = 0 Number of tetrahedrals = 35884 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1187 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9625 Number of elements = 53328 Number of triangles = 7146 Number of quadrilatarals = 0 Number of tetrahedrals = 46182 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9899 Number of elements = 54216 Number of triangles = 8034 Number of quadrilatarals = 0 Number of tetrahedrals = 46182 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7485 Number of elements = 41497 Number of triangles = 5370 Number of quadrilatarals = 0 Number of tetrahedrals = 36127 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1212 Number of elements = 6385 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5053 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1202 Number of elements = 6334 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5002 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9302 Number of elements = 51451 Number of triangles = 6968 Number of quadrilatarals = 0 Number of tetrahedrals = 44483 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9522 Number of elements = 52179 Number of triangles = 7696 Number of quadrilatarals = 0 Number of tetrahedrals = 44483 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7466 Number of elements = 41416 Number of triangles = 5368 Number of quadrilatarals = 0 Number of tetrahedrals = 36048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1187 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 869 Number of elements = 4533 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3537 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8956 Number of elements = 49469 Number of triangles = 6784 Number of quadrilatarals = 0 Number of tetrahedrals = 42685 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9139 Number of elements = 50065 Number of triangles = 7380 Number of quadrilatarals = 0 Number of tetrahedrals = 42685 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7430 Number of elements = 41197 Number of triangles = 5360 Number of quadrilatarals = 0 Number of tetrahedrals = 35837 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1187 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 522 Number of elements = 2638 Number of triangles = 688 Number of quadrilatarals = 0 Number of tetrahedrals = 1950 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8638 Number of elements = 47663 Number of triangles = 6598 Number of quadrilatarals = 0 Number of tetrahedrals = 41065 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8777 Number of elements = 48099 Number of triangles = 7034 Number of quadrilatarals = 0 Number of tetrahedrals = 41065 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7402 Number of elements = 41032 Number of triangles = 5352 Number of quadrilatarals = 0 Number of tetrahedrals = 35680 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 848 Number of elements = 4402 Number of triangles = 994 Number of quadrilatarals = 0 Number of tetrahedrals = 3408 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2665 Number of triangles = 688 Number of quadrilatarals = 0 Number of tetrahedrals = 1977 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9771 Number of elements = 54406 Number of triangles = 6748 Number of quadrilatarals = 0 Number of tetrahedrals = 47658 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10261 Number of elements = 56170 Number of triangles = 8512 Number of quadrilatarals = 0 Number of tetrahedrals = 47658 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7355 Number of elements = 40784 Number of triangles = 5334 Number of quadrilatarals = 0 Number of tetrahedrals = 35450 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 2663 Number of elements = 14238 Number of triangles = 2794 Number of quadrilatarals = 0 Number of tetrahedrals = 11444 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 243 Number of elements = 1148 Number of triangles = 384 Number of quadrilatarals = 0 Number of tetrahedrals = 764 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1510 Number of elements = 7821 Number of triangles = 1986 Number of quadrilatarals = 0 Number of tetrahedrals = 5835 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1574 Number of elements = 7945 Number of triangles = 2110 Number of quadrilatarals = 0 Number of tetrahedrals = 5835 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1170 Number of elements = 6155 Number of triangles = 1308 Number of quadrilatarals = 0 Number of tetrahedrals = 4847 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 360 Number of elements = 1630 Number of triangles = 718 Number of quadrilatarals = 0 Number of tetrahedrals = 912 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 44 Number of elements = 160 Number of triangles = 84 Number of quadrilatarals = 0 Number of tetrahedrals = 76 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5096 Number of elements = 27903 Number of triangles = 4076 Number of quadrilatarals = 0 Number of tetrahedrals = 23827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5242 Number of elements = 28455 Number of triangles = 4628 Number of quadrilatarals = 0 Number of tetrahedrals = 23827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 4905 Number of elements = 26939 Number of triangles = 4044 Number of quadrilatarals = 0 Number of tetrahedrals = 22895 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 337 Number of elements = 1516 Number of triangles = 584 Number of quadrilatarals = 0 Number of tetrahedrals = 932 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 33115 Number of elements = 191815 Number of triangles = 8476 Number of quadrilatarals = 0 Number of tetrahedrals = 183339 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 36459 Number of elements = 205159 Number of triangles = 21820 Number of quadrilatarals = 0 Number of tetrahedrals = 183339 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 28820 Number of elements = 163772 Number of triangles = 15148 Number of quadrilatarals = 0 Number of tetrahedrals = 148624 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1416 Number of elements = 7524 Number of triangles = 1456 Number of quadrilatarals = 0 Number of tetrahedrals = 6068 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 4240 Number of elements = 23511 Number of triangles = 2950 Number of quadrilatarals = 0 Number of tetrahedrals = 20561 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 720 Number of elements = 3724 Number of triangles = 842 Number of quadrilatarals = 0 Number of tetrahedrals = 2882 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1263 Number of elements = 6628 Number of triangles = 1424 Number of quadrilatarals = 0 Number of tetrahedrals = 5204 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16667 Number of elements = 94472 Number of triangles = 8798 Number of quadrilatarals = 0 Number of tetrahedrals = 85674 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 18591 Number of elements = 101848 Number of triangles = 16174 Number of quadrilatarals = 0 Number of tetrahedrals = 85674 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 12023 Number of elements = 67478 Number of triangles = 7138 Number of quadrilatarals = 0 Number of tetrahedrals = 60340 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 6568 Number of elements = 34370 Number of triangles = 9036 Number of quadrilatarals = 0 Number of tetrahedrals = 25334 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2838 Number of elements = 12404 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 6952 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2494 Number of elements = 10977 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6425 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2838 Number of elements = 12404 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 6952 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2494 Number of elements = 10977 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6425 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2838 Number of elements = 12404 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 6952 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2494 Number of elements = 10977 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6425 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2838 Number of elements = 12404 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 6952 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tet', blk_id 1, num_entries 6952 Sideset: 'Farfield', set_id 1, num_entries 12 Sideset: 'Wing1', set_id 2, num_entries 5440 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2494 Number of elements = 10977 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6425 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tet', blk_id 1, num_entries 6425 Sideset: 'Farfield', set_id 1, num_entries 12 Sideset: 'Wing1', set_id 2, num_entries 4540 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4972 Number of elements = 27531 Number of triangles = 3460 Number of quadrilatarals = 0 Number of tetrahedrals = 24071 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6395 Number of elements = 35692 Number of triangles = 4048 Number of quadrilatarals = 0 Number of tetrahedrals = 31644 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 60123 Number of elements = 350900 Number of triangles = 12928 Number of quadrilatarals = 0 Number of tetrahedrals = 337972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 59547 Number of elements = 346940 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 334512 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 60123 Number of elements = 350400 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 337972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required ok test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - trailingEdge Done getting mesh sizing parameters ok test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Farfield_tri', blk_id 1, num_entries 1332 Block: 'Wing1_tri', blk_id 2, num_entries 73442 Sideset: 'Farfield', set_id 1, num_entries 1332 Sideset: 'Wing1', set_id 2, num_entries 73442 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Farfield_tri', blk_id 1, num_entries 300 Block: 'Wing1_tri', blk_id 2, num_entries 32990 Sideset: 'Farfield', set_id 1, num_entries 300 Sideset: 'Wing1', set_id 2, num_entries 32990 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 44 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 3 Surface 2: Number of points found for aero-spline = 6 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 8 automatic connections were made for capsConnect Rib_Root (node id 1) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Done running Astros! ok test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG ok test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing ok test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - VTail1 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - VTail2 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - VTail1 (ID = 0) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - VTail2 (ID = 1) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Writing surface - Wing (ID = 2) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice control surface data VLM control surface name - Elevator VLM control surface name - LeftAileron VLM control surface name - RightAileron VLM control surface name - Rudder Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 28.284271 -nDiv 9 -maxR 7 -mesh2d > autoInputs.out Executing: ./aero.csh > aero.out ok test_outputs (test_cart3d.TestCart3D.test_outputs) ... ok test_reenter (test_cart3d.TestCart3D.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Getting CFD functional....... Number of design variables - 1 Objective name - Drag Done getting CFD functional Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out Executing: ./aero.csh > aero.out Executing: ./aero.csh > aero.out Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.307131 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out Executing: ./aero.csh > aero.out ok test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Getting CFD design variables....... Number of design variables - 1 Design Variable name - Mach Done getting CFD design variables Getting CFD functional....... Number of design variables - 3 Objective name - C_A Objective name - C_N Objective name - C_Y Done getting CFD functional Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:24:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:24:47) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:24:48) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:24:54) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:24:54) Linearizing cut-cells (00:24:54) ... done o Number of simultaneous xsensit jobs: 1 (00:24:54) Computing gradients (00:25:02) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:06) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 3 Objective name - C_D Objective name - C_L Objective name - C_S Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:07) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:10) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:17) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:25:17) Linearizing cut-cells (00:25:17) ... done o Number of simultaneous xsensit jobs: 1 (00:25:17) Computing gradients (00:25:25) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:26) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:29) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_l Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:34) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:38) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:25:39) Linearizing cut-cells (00:25:39) ... done o Number of simultaneous xsensit jobs: 1 (00:25:39) Computing gradients (00:25:43) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:47) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_m Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:49) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:51) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:25:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:25:56) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:25:56) Linearizing cut-cells (00:25:56) ... done o Number of simultaneous xsensit jobs: 1 (00:25:56) Computing gradients (00:26:00) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:04) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_n Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:08) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:09) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:12) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:26:12) Linearizing cut-cells (00:26:12) ... done o Number of simultaneous xsensit jobs: 1 (00:26:12) Computing gradients (00:26:16) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:18) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:20) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_x Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:24) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:25) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:28) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:26:28) Linearizing cut-cells (00:26:28) ... done o Number of simultaneous xsensit jobs: 1 (00:26:28) Computing gradients (00:26:32) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:34) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:36) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_y Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:37) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:40) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:41) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:44) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:26:44) Linearizing cut-cells (00:26:44) ... done o Number of simultaneous xsensit jobs: 1 (00:26:44) Computing gradients (00:26:48) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:50) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:52) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) Getting CFD functional....... Number of design variables - 1 Objective name - C_M_z Done getting CFD functional o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:56) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:26:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:26:59) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 1 o Number of simultaneous cutter jobs: 1 (00:26:59) Linearizing cut-cells (00:26:59) ... done o Number of simultaneous xsensit jobs: 1 (00:27:00) Computing gradients (00:27:04) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:27:05) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:27:07) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) ok test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Getting CFD design variables....... Number of design variables - 2 Design Variable name - Mach Design Variable name - area Done getting CFD design variables Getting CFD functional....... Number of design variables - 3 Objective name - C_A Objective name - C_N Objective name - C_Y Done getting CFD functional Body size = 15.356535 Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:27:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:27:13) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:27:14) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:27:19) aero.csh done Max memory allowed: 32 GB Flow hexes: 8744 Estimated cutter memory: 0.000874 GB / DV Estimated xsensit memory: 0.016614 GB / DV Available threads: 2 # DVs: 2 o Number of simultaneous cutter jobs: 2 (00:27:20) Linearizing cut-cells (00:27:22) ... done o Number of simultaneous xsensit jobs: 2 (00:27:22) Computing gradients Adjusted OMP_NUM_THREADS to 1 for xsensit (00:27:30) ... done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) o Evaluating Cart3D functionals and/or gradients ATTENTION: using static geometry ../inputs/Components.i.tri (00:27:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1 (00:27:34) aero.csh done o case M0.5A1B0_DP1, averaging data over 1 cycle(s) ok test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Wing1, index = 1 Name = trailingEdge, index = 2 Writing FAST file .... Finished writing FAST file Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 17181B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 17181B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 17181B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 17181B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_box (test_egadsTess.TestEGADS.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_egadsTess.TestEGADS.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ok test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = nodeBody, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Farfield_tri', blk_id 1, num_entries 48 Block: 'Wing1_tri', blk_id 2, num_entries 19110 Sideset: 'Farfield', set_id 1, num_entries 48 Sideset: 'Wing1', set_id 2, num_entries 19110 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Farfield_tri', blk_id 1, num_entries 12 Block: 'Wing1_tri', blk_id 2, num_entries 14282 Sideset: 'Farfield', set_id 1, num_entries 12 Sideset: 'Wing1', set_id 2, num_entries 14282 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_egadsTess.TestEGADS.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7800 Number of elements = 15596 Number of triangle elements = 15596 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5906 Number of elements = 11808 Number of triangle elements = 11808 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 542 Number of elements = 1080 Number of triangle elements = 1080 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14248 Total number of elements = 28484 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14248, elements - 28484 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.113577 Creating surface mesh ... Surface mesh seconds: 0.015469 Recovering boundaries... Boundary recovery seconds: 0.12527 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.030088 Recovering Delaunayness... Delaunay recovery seconds: 0.057712 Refining mesh... 18992 insertions, added 13405 points, 688228 tetrahedra in queue. 6324 insertions, added 2619 points, 589108 tetrahedra in queue. 8430 insertions, added 2014 points, 124223 tetrahedra in queue. Refinement seconds: 2.06175 Smoothing vertices... Mesh smoothing seconds: 1.80891 Improving mesh... Mesh improvement seconds: 0.040675 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.006546 Total running seconds: 4.26035 Statistics: Input points: 14248 Input facets: 28484 Input segments: 42726 Input holes: 2 Input regions: 0 Mesh points: 33028 Mesh tetrahedra: 159264 Mesh faces: 332770 Mesh faces on exterior boundary: 28484 Mesh faces on input facets: 28484 Mesh edges on input segments: 42726 Steiner points inside domain: 18780 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 5 Design Variable name - Mach Warning: No initial value set for Mach Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. ok test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 6 Design Variable name - Alpha Design Variable name - Beta Warning: No initial value set for Beta Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Overwrite_NML is set to 'True' - a new namelist will be created Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Reading rubber.data Getting CFD design variables....... Number of design variables - 1 Design Variable name - Alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Creating FUN3D directory tree DesignVariable = Alpha Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Overwrite_NML is set to 'True' - a new namelist will be created Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Reading rubber.data ok test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 6 Design Variable name - Alpha Design Variable name - Beta Warning: No initial value set for Beta Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing rubber.data Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Projecting tessellation 1 (of 3) on to new body Projecting tessellation 2 (of 3) on to new body Projecting tessellation 3 (of 3) on to new body Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Projecting tessellation 1 (of 3) on to new body Projecting tessellation 2 (of 3) on to new body Projecting tessellation 3 (of 3) on to new body Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data ok test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7800 Number of elements = 15596 Number of triangle elements = 15596 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5906 Number of elements = 11808 Number of triangle elements = 11808 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 542 Number of elements = 1080 Number of triangle elements = 1080 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14248 Total number of elements = 28484 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14248, elements - 28484 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.147865 Creating surface mesh ... Surface mesh seconds: 0.014424 Recovering boundaries... Boundary recovery seconds: 0.132412 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.026383 Recovering Delaunayness... Delaunay recovery seconds: 0.04932 Refining mesh... 18992 insertions, added 13405 points, 688228 tetrahedra in queue. 6324 insertions, added 2619 points, 589108 tetrahedra in queue. 8430 insertions, added 2014 points, 124223 tetrahedra in queue. Refinement seconds: 1.99747 Smoothing vertices... Mesh smoothing seconds: 1.8306 Improving mesh... Mesh improvement seconds: 0.052351 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00595 Total running seconds: 4.25707 Statistics: Input points: 14248 Input facets: 28484 Input segments: 42726 Input holes: 2 Input regions: 0 Mesh points: 33028 Mesh tetrahedra: 159264 Mesh faces: 332770 Mesh faces on exterior boundary: 28484 Mesh faces on input facets: 28484 Mesh edges on input segments: 42726 Steiner points inside domain: 18780 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. ok test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found! Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. ok test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions Boundary condition name - Wing1 ok test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X ok test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 5097, elements - 10182 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 5097, elements - 10182 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! ok test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Writing moving_body.input ok test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14248, elements - 28484 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. ok test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - box2 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ok test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4048 Number of elements = 8092 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8092 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6217 Combined Number of elements = 12425 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12424 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 3908 Number of elements = 7812 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7812 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6077 Combined Number of elements = 12145 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12144 Combined Elemental Quad4 = 0 Updating mesh element types based on properties input EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4048 Number of elements = 8092 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8092 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6217 Combined Number of elements = 12425 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12424 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4048 Number of elements = 8092 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8092 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6217 Combined Number of elements = 12425 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12424 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 3908 Number of elements = 7812 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7812 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6077 Combined Number of elements = 12145 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12144 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 3908 Number of elements = 7812 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7812 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6077 Combined Number of elements = 12145 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12144 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input ok test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ok test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... Getting CFD design variables....... Number of design variables - 4 Design Variable name - alowervar Design Variable name - auppervar Design Variable name - classvar Design Variable name - ztailvar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - avar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... Getting CFD design variables....... Number of design variables - 2 Design Variable name - camber Design Variable name - thick Done getting CFD design variables ok test_journal (test_mses.TestMSES_NACA.test_journal) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable' test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable' test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable' test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable' test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable' test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable' test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable' test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable' test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable' test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable' EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 54 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 54 54 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 12 26 AFLR2 IG : Nodes, Faces = 24 50 AFLR2 IG : Nodes, Faces = 36 74 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 106 AFLR2 IG : Nodes, Faces = 53 108 AFLR2 IG : Nodes, Faces = 54 110 AFLR2 IG : Nodes, Faces = 58 110 AFLR2 IG : Nodes, Faces = 54 54 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 54 54 AFLR2 GG : Nodes, Faces = 100 146 AFLR2 GG : Nodes, Faces = 122 190 AFLR2 GG : Nodes, Faces = 138 222 AFLR2 GG : Nodes, Faces = 153 252 AFLR2 GG : Nodes, Faces = 168 282 AFLR2 GG : Nodes, Faces = 180 306 AFLR2 GG : Nodes, Faces = 192 330 AFLR2 GG : Nodes, Faces = 201 348 AFLR2 GG : Nodes, Faces = 210 366 AFLR2 GG : Nodes, Faces = 216 378 AFLR2 GG : Nodes, Faces = 221 388 AFLR2 GG : Nodes, Faces = 224 394 AFLR2 GG : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 225 Number of elements = 450 Number of tris = 396 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tri', blk_id 1, num_entries 396 Sideset: 'Airfoil', set_id 1, num_entries 18 Sideset: 'InFlow', set_id 2, num_entries 9 Sideset: 'OutFlow', set_id 3, num_entries 9 Sideset: 'TunnelWall', set_id 4, num_entries 18 Finished writing Exodus file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tri', blk_id 1, num_entries 719 Sideset: 'Airfoil', set_id 1, num_entries 17 Sideset: 'InFlow', set_id 2, num_entries 4 Sideset: 'OutFlow', set_id 3, num_entries 18 Sideset: 'TunnelWall', set_id 4, num_entries 22 Finished writing Exodus file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tri', blk_id 1, num_entries 1200 Sideset: 'Airfoil', set_id 1, num_entries 20 Sideset: 'InFlow', set_id 2, num_entries 4 Sideset: 'OutFlow', set_id 3, num_entries 36 Sideset: 'TunnelWall', set_id 4, num_entries 40 Finished writing Exodus file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1579 Number of elements = 8634 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7394 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2600 Number of elements = 13872 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11114 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1039 Number of elements = 5509 Number of triangles = 998 Number of quadrilatarals = 0 Number of tetrahedrals = 4511 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 15766 Number of elements = 90668 Number of triangles = 4632 Number of quadrilatarals = 0 Number of tetrahedrals = 86036 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tet', blk_id 1, num_entries 86036 Sideset: 'Farfield', set_id 1, num_entries 36 Sideset: 'Wing1', set_id 2, num_entries 4596 Finished writing Exodus file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tet', blk_id 1, num_entries 98795 Sideset: 'Farfield', set_id 1, num_entries 144 Sideset: 'Wing1', set_id 2, num_entries 4086 Finished writing Exodus file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tet', blk_id 1, num_entries 163296 Sideset: 'Farfield', set_id 1, num_entries 576 Sideset: 'Wing1', set_id 2, num_entries 5666 Finished writing Exodus file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1579 Number of elements = 8634 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7394 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_refine.TestREFINE.test_inputs) ... ok test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 432 Number of elements = 2132 Number of triangles = 644 Number of quadrilatarals = 0 Number of tetrahedrals = 1488 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 ok test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 935 Number of elements = 5010 Number of triangles = 758 Number of quadrilatarals = 0 Number of tetrahedrals = 4252 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 3 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 8 Faces EGADS : Body 0 has 15 Edges EGADS : Body 0 has 8 Loops EGADS : Body 0 has 9 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 8 Faces EGADS : Body 1 has 15 Edges EGADS : Body 1 has 8 Loops EGADS : Body 1 has 9 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 2 Faces EGADS : Body 2 has 6 Edges EGADS : Body 2 has 2 Loops EGADS : Body 2 has 2 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 4 5 EGADS : 2 Yes 0 0 1 1 1 1 3 4 6 EGADS : 3 Yes 0 0 1 1 1 1 2 4 7 EGADS : 4 Yes 0 0 1 1 1 1 2 3 EGADS : 5 Yes 0 0 1 1 1 1 6 7 8 EGADS : 6 Yes 0 0 1 1 1 2 5 7 8 EGADS : 7 Yes 0 0 1 1 1 3 5 6 8 EGADS : 8 Yes 0 0 1 1 1 5 6 7 EGADS : 9 Yes 1 0 1 0 10 10 11 12 13 EGADS : 10 Yes 1 0 1 0 10 9 11 12 14 EGADS : 11 Yes 1 0 1 0 10 9 10 12 15 EGADS : 12 Yes 1 0 1 0 10 9 10 11 EGADS : 13 Yes 1 0 1 0 10 9 14 15 16 EGADS : 14 Yes 1 0 1 0 10 10 13 15 16 EGADS : 15 Yes 1 0 1 0 10 11 13 14 16 EGADS : 16 Yes 1 0 1 0 10 13 14 15 EGADS : 17 Yes 2 0 1 NA NA 18 EGADS : 18 Yes 2 0 1 NA NA 17 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 4 -3 -2 EGADS : 2 3 7 -6 -5 EGADS : 3 6 9 -1 -8 EGADS : 4 -4 -9 -7 EGADS : 5 -10 2 11 -12 EGADS : 6 -11 5 13 -14 EGADS : 7 -13 8 10 -15 EGADS : 8 12 14 15 EGADS : 9 16 19 -18 -17 EGADS : 10 18 22 -21 -20 EGADS : 11 21 24 -16 -23 EGADS : 12 -19 -24 -22 EGADS : 13 -25 17 26 -27 EGADS : 14 -26 20 28 -29 EGADS : 15 -28 23 25 -30 EGADS : 16 27 29 30 EGADS : 17 -31 -32 33 34 EGADS : 18 -35 -34 36 32 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 4 -3 -2 EGADS : 2 Yes 3 7 -6 -5 EGADS : 3 Yes 6 9 -1 -8 EGADS : 4 Yes -4 -9 -7 EGADS : 5 Yes -10 2 11 -12 EGADS : 6 Yes -11 5 13 -14 EGADS : 7 Yes -13 8 10 -15 EGADS : 8 Yes 12 14 15 EGADS : 9 Yes 16 19 -18 -17 EGADS : 10 Yes 18 22 -21 -20 EGADS : 11 Yes 21 24 -16 -23 EGADS : 12 Yes -19 -24 -22 EGADS : 13 Yes -25 17 26 -27 EGADS : 14 Yes -26 20 28 -29 EGADS : 15 Yes -28 23 25 -30 EGADS : 16 Yes 27 29 30 EGADS : 17 Yes -31 -32 33 34 EGADS : 18 Yes -35 -34 36 32 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 3 EGADS : 2 0 Yes 1 3 1 1 5 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 4 EGADS : 5 0 Yes 3 5 1 2 6 EGADS : 6 0 Yes 5 6 1 2 3 EGADS : 7 0 Yes 4 6 1 2 4 EGADS : 8 0 Yes 5 1 1 3 7 EGADS : 9 0 Yes 6 2 1 3 4 EGADS : 10 0 Yes 1 7 1 5 7 EGADS : 11 0 Yes 3 8 1 5 6 EGADS : 12 0 Yes 7 8 1 5 8 EGADS : 13 0 Yes 5 9 1 6 7 EGADS : 14 0 Yes 8 9 1 6 8 EGADS : 15 0 Yes 9 7 1 7 8 EGADS : 16 1 Yes 10 11 1 9 11 EGADS : 17 1 Yes 10 12 1 9 13 EGADS : 18 1 Yes 12 13 1 9 10 EGADS : 19 1 Yes 11 13 1 9 12 EGADS : 20 1 Yes 12 14 1 10 14 EGADS : 21 1 Yes 14 15 1 10 11 EGADS : 22 1 Yes 13 15 1 10 12 EGADS : 23 1 Yes 14 10 1 11 15 EGADS : 24 1 Yes 15 11 1 11 12 EGADS : 25 1 Yes 10 16 1 13 15 EGADS : 26 1 Yes 12 17 1 13 14 EGADS : 27 1 Yes 16 17 1 13 16 EGADS : 28 1 Yes 14 18 1 14 15 EGADS : 29 1 Yes 17 18 1 14 16 EGADS : 30 1 Yes 18 16 1 15 16 EGADS : 31 2 DEGEN 19 19 - 17 EGADS : 32 2 Yes 20 19 NA 17 18 EGADS : 33 2 DEGEN 20 20 - 17 EGADS : 34 2 Yes 20 19 NA 17 18 EGADS : 35 2 DEGEN 19 19 - 18 EGADS : 36 2 DEGEN 20 20 - 18 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 3.77246052 0 0.00459131419 EGADS : 2 Yes 5.90487498 7.07106781 0 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 4.0824829 7.07106781 0.123425948 EGADS : 5 Yes 3.77001182 0 0 EGADS : 6 Yes 5.90282524 7.07106781 0 EGADS : 7 Yes 5.90487498 0 0 EGADS : 8 Yes 4.0824829 0 0.123425948 EGADS : 9 Yes 5.90282524 0 0 EGADS : 10 Yes 11.5089842 0 0.00183652568 EGADS : 11 Yes 12.36195 2.82842712 0 EGADS : 12 Yes 10 0 0 EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791 EGADS : 14 Yes 11.5080047 0 0 EGADS : 15 Yes 12.3611301 2.82842712 0 EGADS : 16 Yes 12.36195 0 0 EGADS : 17 Yes 11.6329932 0 0.0493703791 EGADS : 18 Yes 12.3611301 0 0 EGADS : 19 Yes 0 0 80 EGADS : 20 Yes 0 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 160 AFLR4 : Min Bounding Box Length = 160 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 0.890888 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 15.6122 AFLR4 : Abs Min Surf Spacing = 0.00222722 AFLR4 : Min Surf Spacing = 0.00445444 AFLR4 : Max Surf Spacing = 0.0890888 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD AFLR4 : 2 CAD geometry 0 STD AFLR4 : 3 CAD geometry 0 STD AFLR4 : 4 CAD geometry 0 STD AFLR4 : 5 CAD geometry 0 STD AFLR4 : 6 CAD geometry 0 STD AFLR4 : 7 CAD geometry 0 STD AFLR4 : 8 CAD geometry 0 STD AFLR4 : 9 CAD geometry 0 STD AFLR4 : 10 CAD geometry 0 STD AFLR4 : 11 CAD geometry 0 STD AFLR4 : 12 CAD geometry 0 STD AFLR4 : 13 CAD geometry 0 STD AFLR4 : 14 CAD geometry 0 STD AFLR4 : 15 CAD geometry 0 STD AFLR4 : 16 CAD geometry 0 STD AFLR4 : 17 CAD geometry 0 FARFIELD AFLR4 : 18 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 12428 AFLR43 : Nodes = 6220 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.50 AFLR3 : Version Date 10/31/23 @ 06:31PM AFLR3 : Compile OS Darwin 23.3.0 arm64 AFLR3 : Compile Date 02/08/24 @ 04:22PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 6220 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid UG3 : 7 Solid UG3 : 8 Solid UG3 : 9 Solid UG3 : 10 Solid UG3 : 11 Solid UG3 : 12 Solid UG3 : 13 Solid UG3 : 14 Solid UG3 : 15 Solid UG3 : 16 Solid UG3 : 17 FarField UG3 : 18 FarField AFLR3 : CPU Time = 0.014 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 6220 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1246 7333 AFLR3 IG : Nodes, Elements = 2492 16261 AFLR3 IG : Nodes, Elements = 3738 25026 AFLR3 IG : Nodes, Elements = 4984 34312 AFLR3 IG : Nodes, Elements = 6227 43517 AFLR3 IG : Nodes, Elements = 6227 43439 AFLR3 IG : Nodes, Elements = 6227 43476 AFLR3 IG : Nodes, Elements = 6227 43444 AFLR3 IG : Nodes, Elements = 6220 26114 AFLR3 IG : Nodes, Elements = 6220 26132 AFLR3 IG : Nodes, Elements = 6220 21569 AFLR3 IG : Nodes, Elements = 6220 19193 AFLR3 : CPU Time = 0.132 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 6220 19193 AFLR3 GG : Nodes, Elements = 9101 28053 AFLR3 GG : Nodes, Elements = 9101 39640 AFLR3 GG : Nodes, Elements = 9101 36690 AFLR3 GG : Nodes, Elements = 9101 35155 AFLR3 GG : Nodes, Elements = 11687 43216 AFLR3 GG : Nodes, Elements = 11687 54497 AFLR3 GG : Nodes, Elements = 11687 51170 AFLR3 GG : Nodes, Elements = 11687 50185 AFLR3 GG : Nodes, Elements = 14519 58970 AFLR3 GG : Nodes, Elements = 14519 71103 AFLR3 GG : Nodes, Elements = 14519 67722 AFLR3 GG : Nodes, Elements = 14519 66894 AFLR3 GG : Nodes, Elements = 17597 76360 AFLR3 GG : Nodes, Elements = 17597 89686 AFLR3 GG : Nodes, Elements = 17597 86040 AFLR3 GG : Nodes, Elements = 17597 85134 AFLR3 GG : Nodes, Elements = 20802 94942 AFLR3 GG : Nodes, Elements = 20802 108532 AFLR3 GG : Nodes, Elements = 20802 104847 AFLR3 GG : Nodes, Elements = 20802 104019 AFLR3 GG : Nodes, Elements = 24174 114290 AFLR3 GG : Nodes, Elements = 24174 128631 AFLR3 GG : Nodes, Elements = 24174 124801 AFLR3 GG : Nodes, Elements = 24174 123982 AFLR3 GG : Nodes, Elements = 27742 134809 AFLR3 GG : Nodes, Elements = 27742 150037 AFLR3 GG : Nodes, Elements = 27742 145948 AFLR3 GG : Nodes, Elements = 27742 145081 AFLR3 GG : Nodes, Elements = 31383 156143 AFLR3 GG : Nodes, Elements = 31383 171588 AFLR3 GG : Nodes, Elements = 31383 167421 AFLR3 GG : Nodes, Elements = 31383 166536 AFLR3 GG : Nodes, Elements = 35115 177837 AFLR3 GG : Nodes, Elements = 35115 193748 AFLR3 GG : Nodes, Elements = 35115 189548 AFLR3 GG : Nodes, Elements = 35115 188723 AFLR3 GG : Nodes, Elements = 38948 200319 AFLR3 GG : Nodes, Elements = 38948 216342 AFLR3 GG : Nodes, Elements = 38948 212298 AFLR3 GG : Nodes, Elements = 38948 211481 AFLR3 GG : Nodes, Elements = 42740 222940 AFLR3 GG : Nodes, Elements = 42740 239184 AFLR3 GG : Nodes, Elements = 42740 234883 AFLR3 GG : Nodes, Elements = 42740 234060 AFLR3 GG : Nodes, Elements = 46416 245151 AFLR3 GG : Nodes, Elements = 46416 260680 AFLR3 GG : Nodes, Elements = 46416 256642 AFLR3 GG : Nodes, Elements = 46416 255866 AFLR3 GG : Nodes, Elements = 50035 266777 AFLR3 GG : Nodes, Elements = 50035 281993 AFLR3 GG : Nodes, Elements = 50035 278055 AFLR3 GG : Nodes, Elements = 50035 277383 AFLR3 GG : Nodes, Elements = 53591 288088 AFLR3 GG : Nodes, Elements = 53591 303095 AFLR3 GG : Nodes, Elements = 53591 299307 AFLR3 GG : Nodes, Elements = 53591 298569 AFLR3 GG : Nodes, Elements = 57005 308827 AFLR3 GG : Nodes, Elements = 57005 323244 AFLR3 GG : Nodes, Elements = 57005 319601 AFLR3 GG : Nodes, Elements = 57005 318957 AFLR3 GG : Nodes, Elements = 60293 328832 AFLR3 GG : Nodes, Elements = 60293 342689 AFLR3 GG : Nodes, Elements = 60293 339197 AFLR3 GG : Nodes, Elements = 60293 338647 AFLR3 GG : Nodes, Elements = 63359 347851 AFLR3 GG : Nodes, Elements = 63359 360783 AFLR3 GG : Nodes, Elements = 63359 357437 AFLR3 GG : Nodes, Elements = 63359 356932 AFLR3 GG : Nodes, Elements = 66259 365641 AFLR3 GG : Nodes, Elements = 66259 377775 AFLR3 GG : Nodes, Elements = 66259 374741 AFLR3 GG : Nodes, Elements = 66259 374315 AFLR3 GG : Nodes, Elements = 68879 382177 AFLR3 GG : Nodes, Elements = 68879 393099 AFLR3 GG : Nodes, Elements = 68879 390371 AFLR3 GG : Nodes, Elements = 68879 390020 AFLR3 GG : Nodes, Elements = 71152 396844 AFLR3 GG : Nodes, Elements = 71152 406357 AFLR3 GG : Nodes, Elements = 71152 403836 AFLR3 GG : Nodes, Elements = 71152 403561 AFLR3 GG : Nodes, Elements = 73068 409315 AFLR3 GG : Nodes, Elements = 73068 417362 AFLR3 GG : Nodes, Elements = 73068 415318 AFLR3 GG : Nodes, Elements = 73068 415069 AFLR3 GG : Nodes, Elements = 74529 419454 AFLR3 GG : Nodes, Elements = 74529 425587 AFLR3 GG : Nodes, Elements = 74529 423928 AFLR3 GG : Nodes, Elements = 74529 423776 AFLR3 GG : Nodes, Elements = 75631 427084 AFLR3 GG : Nodes, Elements = 75631 431714 AFLR3 GG : Nodes, Elements = 75631 430512 AFLR3 GG : Nodes, Elements = 75631 430423 AFLR3 GG : Nodes, Elements = 76419 432787 AFLR3 GG : Nodes, Elements = 76419 436211 AFLR3 GG : Nodes, Elements = 76419 435175 AFLR3 GG : Nodes, Elements = 76419 435106 AFLR3 GG : Nodes, Elements = 76934 436651 AFLR3 GG : Nodes, Elements = 76934 438851 AFLR3 GG : Nodes, Elements = 76934 438238 AFLR3 GG : Nodes, Elements = 76934 438198 AFLR3 GG : Nodes, Elements = 77241 439119 AFLR3 GG : Nodes, Elements = 77241 440474 AFLR3 GG : Nodes, Elements = 77241 440052 AFLR3 GG : Nodes, Elements = 77241 440022 AFLR3 GG : Nodes, Elements = 77416 440547 AFLR3 GG : Nodes, Elements = 77416 441274 AFLR3 GG : Nodes, Elements = 77416 441066 AFLR3 GG : Nodes, Elements = 77416 441056 AFLR3 GG : Nodes, Elements = 77509 441335 AFLR3 GG : Nodes, Elements = 77509 441739 AFLR3 GG : Nodes, Elements = 77509 441625 AFLR3 GG : Nodes, Elements = 77509 441612 AFLR3 GG : Nodes, Elements = 77549 441732 AFLR3 GG : Nodes, Elements = 77549 441904 AFLR3 GG : Nodes, Elements = 77549 441849 AFLR3 GG : Nodes, Elements = 77549 441848 AFLR3 GG : Nodes, Elements = 77559 441878 AFLR3 GG : Nodes, Elements = 77559 441913 AFLR3 GG : Nodes, Elements = 77559 441902 AFLR3 GG : Nodes, Elements = 77564 441917 AFLR3 GG : Nodes, Elements = 77564 441932 AFLR3 GG : Nodes, Elements = 77564 441928 AFLR3 GG : Nodes, Elements = 77565 441931 AFLR3 GG : Nodes, Elements = 77565 441938 AFLR3 GG : Nodes, Elements = 77565 441933 AFLR3 GG : Nodes, Elements = 77595 442023 AFLR3 GG : Nodes, Elements = 77595 442128 AFLR3 GG : Nodes, Elements = 77595 442098 AFLR3 GG : Nodes, Elements = 77595 442094 AFLR3 GG : Nodes, Elements = 77599 442106 AFLR3 GG : Nodes, Elements = 77599 442119 AFLR3 GG : Nodes, Elements = 77599 442116 AFLR3 GG : Nodes, Elements = 77599 442115 AFLR3 GG : Nodes, Elements = 77600 442118 AFLR3 GG : Nodes, Elements = 77600 442125 AFLR3 GG : Nodes, Elements = 77600 442121 AFLR3 : CPU Time = 5.500 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 77600 442121 AFLR3 QI : Nodes, Elements = 76105 433678 AFLR3 QI : Nodes, Elements = 75842 432198 AFLR3 QI : Nodes, Elements = 75829 432123 AFLR3 QI : Nodes, Elements = 75827 432113 AFLR3 QI : Nodes, Elements = 75826 432107 AFLR3 QI : Nodes, Elements = 75826 436049 AFLR3 QI : Nodes, Elements = 75826 431912 AFLR3 QI : Nodes, Elements = 75826 431430 AFLR3 QI : Nodes, Elements = 75826 431831 AFLR3 QI : Nodes, Elements = 75826 431146 AFLR3 QI : Nodes, Elements = 75826 430921 AFLR3 QI : Nodes, Elements = 75826 431306 AFLR3 QI : Nodes, Elements = 75826 430921 AFLR3 QI : Nodes, Elements = 75826 430900 AFLR3 QI : Nodes, Elements = 75826 431192 AFLR3 QI : Nodes, Elements = 75826 430885 AFLR3 QI : Nodes, Elements = 75826 430832 AFLR3 QI : Nodes, Elements = 75826 431117 AFLR3 QI : Nodes, Elements = 75826 430836 AFLR3 QI : Nodes, Elements = 75826 430821 AFLR3 QI : Nodes, Elements = 75831 430843 AFLR3 QI : Nodes, Elements = 75831 431136 AFLR3 QI : Nodes, Elements = 75831 430863 AFLR3 QI : Nodes, Elements = 75831 430845 AFLR3 QI : Nodes, Elements = 75831 431106 AFLR3 QI : Nodes, Elements = 75831 430850 AFLR3 QI : Nodes, Elements = 75831 430821 AFLR3 : CPU Time = 1.711 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 75831 430821 AFLR3 QRG: Nodes, Elements = 75839 430867 AFLR3 QRG: Nodes, Elements = 75842 430887 AFLR3 QRG: Nodes, Elements = 75841 430884 AFLR3 QRG: Nodes, Elements = 75841 430883 AFLR3 QRG: Nodes, Elements = 75848 430923 AFLR3 QRG: Nodes, Elements = 75847 430916 AFLR3 : CPU Time = 0.070 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 430916 UG3 : Min, Max Ang = 1.198 173.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 54 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 430916 UG3 : Min Vol = 6.52e-10 UG3 : Average Vol = 4.92 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 430916 UG3 : Min, Max Q = 0.073 1 UG3 : Average Q = 0.892 UG3 : No. Q< 0.1 = 27 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 7.813 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 430916 UG3 : Min, Max Ang = 1.198 173.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 54 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 430916 UG3 : Min Vol = 6.52e-10 UG3 : Average Vol = 4.92 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 430916 UG3 : Min, Max Q = 0.189 1 UG3 : Average Q = 0.85 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16 EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32 EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34 EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17 EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18 EGADS : EGADS TESS CREATED EGADS : CHECK TESS FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16 EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17 EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18 Volume mesh: Number of nodes = 75847 Number of elements = 443344 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 430916 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Cardinal" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Raven" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Falcon" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions Boundary condition name - Wing1 ok test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X ok test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 75847 Number of elements = 443344 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 430916 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2 1 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2 2 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 75847 Number of elements = 443344 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 430916 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" CAPS Info: Hit last success -- going live! Running SU2 1 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" CAPS Info: Hit last success -- going live! Running SU2 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions ok test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 75847 Number of elements = 443344 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 430916 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards ok test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 17181B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 298 Number of elements = 592 Number of triangle elements = 592 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 Body 4 (of 7) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 7) Number of nodes = 152 Number of elements = 300 Number of triangle elements = 300 Number of quadrilateral elements = 0 Body 6 (of 7) Number of nodes = 624 Number of elements = 1248 Number of triangle elements = 1248 Number of quadrilateral elements = 0 Body 7 (of 7) Number of nodes = 489 Number of elements = 974 Number of triangle elements = 974 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4197 Total number of elements = 8374 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 298, elements - 592 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 489, elements - 974 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 298, elements - 592 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 489, elements - 974 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Number of surface: nodes - 4197, elements - 8374 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 374 Number of elements = 744 Number of triangle elements = 744 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 472 Total number of elements = 936 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 386 Number of elements = 768 Number of triangle elements = 768 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 582 Total number of elements = 1152 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 351 Number of elements = 698 Number of triangle elements = 698 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 491 Total number of elements = 970 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 376 Number of elements = 748 Number of triangle elements = 748 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1020 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 454 Total number of elements = 896 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 126 Number of elements = 252 Number of triangle elements = 252 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1024 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 109 Number of elements = 214 Number of triangle elements = 214 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 48 Number of elements = 96 Number of triangle elements = 96 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 12 Number of elements = 20 Number of triangle elements = 20 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 169 Total number of elements = 330 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 536 Number of elements = 1072 Number of triangle elements = 1072 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 544 Number of elements = 1084 Number of triangle elements = 1084 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1080 Total number of elements = 2156 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 5) Getting surface mesh for body 2 (of 5) Getting surface mesh for body 3 (of 5) Getting surface mesh for body 4 (of 5) Getting surface mesh for body 5 (of 5) Body 1 (of 5) Number of nodes = 1351 Number of elements = 2682 Number of triangle elements = 2682 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 288 Number of elements = 572 Number of triangle elements = 572 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 173 Number of elements = 342 Number of triangle elements = 342 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 26 Number of elements = 48 Number of triangle elements = 48 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 482 Number of elements = 960 Number of triangle elements = 960 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2320 Total number of elements = 4604 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 173, elements - 342 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 173, elements - 342 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 443 Number of elements = 882 Number of triangle elements = 882 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 522 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 965 Total number of elements = 1926 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 443, elements - 882 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 443, elements - 882 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9583, elements - 19158 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9583, elements - 19158 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9583, elements - 19158 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9583, elements - 19158 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9583, elements - 19158 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7151, elements - 14294 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9583 Number of elements = 19158 Number of triangle elements = 19158 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9583 Total number of elements = 19158 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9583, elements - 19158 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tet', blk_id 1, num_entries 104182 Sideset: 'Farfield', set_id 1, num_entries 48 Sideset: 'Wing1', set_id 2, num_entries 19110 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9583, elements - 19158 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing exodus file .... Block: 'Block1_tet', blk_id 1, num_entries 69273 Sideset: 'Farfield', set_id 1, num_entries 48 Sideset: 'Wing1', set_id 2, num_entries 19110 Finished writing Exodus file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok test_Output (test_zaero.TestZAERO.test_Output) ... ok test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1220 Number of elements = 2680 Number of triangle elements = 2680 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1221 Total number of elements = 2680 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1220 Number of elements = 2680 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 2680 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1221 Combined Number of elements = 2681 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2680 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - Rib_Root Property name - Rib_Root_Point Property name - Ribs Property name - Skin Property name - Spar1 Property name - Spar2 Done getting FEA properties Updating mesh element types based on properties input 'Smart_Restart' is ON Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting vortex lattice control surface data VLM control surface name - CntrlLE VLM control surface name - CntrlTE Done getting vortex lattice control surface data Getting FEA vortex lattice mesh Getting ZAERO UAIC Configurations....... Number of UAIC Configurations - 2 UAIC Configuration: climb, id = 1 - Mach Number : 0.200000 - Reduced Freq: [0.020000, ... , 0.250000] UAIC Configuration: cruise, id = 2 - Mach Number : 0.700000 - Reduced Freq: [0.040000, ... , 0.350000] Getting ZAERO Analysis Subcases....... Number of Analysis Subcases - 2 Analysis Subcase: FlutterCruise, id = 1 - Discipline : flutter - UAIC : cruise Analysis Subcase: Trim, id = 2 - Discipline : Trim - UAIC : climb Getting ZAERO Trim Variables....... Number of Trim Variables - 2 Trim Variable: ANGLEA - Label : ALPHA - Value : free Trim Variable: URDD3 - Label : NZ - Value : 1.0 Updating StaticAeroelastic subcase: Trim - vectorToCG -> [0.345898, 1.652951, -0.041403] - weight -> 476456.149985 - weightMomentOfInertia -> [304902.643270, 98963.803823, 69822.813293, 6179.981375, 19723.152208, 370546.335525] ok ---------------------------------------------------------------------- Ran 143 tests in 761.759s OK (skipped=10) + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/ + make test TYPE=MINIMAL (make -C cCAPS -f aeroelastic_SU2.make) make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date. (make -C cCAPS -f avlTest.make) make[1]: `avlTest' is up to date. (make -C cCAPS -f awaveTest.make) make[1]: `awaveTest' is up to date. (make -C cCAPS -f frictionTest.make) make[1]: `frictionTest' is up to date. (make -C cCAPS -f fun3d.make) make[1]: Nothing to be done for `fun3d'. (make -C cCAPS -f hsm.make) make[1]: `hsm' is up to date. (make -C cCAPS -f interferenceTest.make) make[1]: `interferenceTest' is up to date. (make -C cCAPS -f msesTest.make) make[1]: `msesTest' is up to date. (make -C cCAPS -f mystran.make) make[1]: `mystranTest' is up to date. (make -C cCAPS -f pointwiseTest.make) make[1]: `pointwiseTest' is up to date. (cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL) Running.... MINIMAL c-Tests All tests pass! ================================================= ================================================= (cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL) ================================================= Using python : /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/ESP_venv/bin/python ================================================= Running.... MINIMAL PyTests ================================================= + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) CXtot 0.0006119078685800925 CYtot -6.292592518559147e-15 CZtot -0.3012861394881712 Cltot -4.783069014642483e-14 Cmtot -0.1945055953448147 Cntot -2.338890054396671e-15 Cl'tot -4.786422456048383e-14 Cn'tot -1.50377318550154e-15 CLtot 0.3012509314146395 CDtot 0.00464635348821979 CDvis 0.0 CLff 0.3009503023516151 CYff -7.7198870803959e-15 CDind 0.00464635348821979 CDff 0.004968969500894849 e 0.9669902146155998 StripForces Wing cl = [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407] Wing cd = [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453] real 0m0.825s user 0m0.720s sys 0m0.245s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected) ================================================= ================================================= + echo 'xfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Cl = [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053] Cd = [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433] real 0m3.808s user 0m3.303s sys 0m0.132s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= ================================================= + echo 'mses_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Cl = 0.3783791085548177 Cd = 0.007775858417209677 Cm = 0.005262636995835036 real 0m3.671s user 0m3.130s sys 0m0.157s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected) ================================================= ================================================= + echo 'friction_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Setting Mach & Altitude Values Lifting Surface: Body = 1, units m XLE: 1.571946 -3.872983 0.249728 XTE: 2.536563 -3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 2, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.614012 0.000000 0.002015 Chord: 1.614013 Arc: 3.308635 T/C: 0.127839 Type: Wing Lifting Surface: Body = 3, units m XLE: 1.571946 3.872983 0.249728 XTE: 2.536563 3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 4, units m XLE: 5.484123 0.000000 1.468246 XTE: 6.210307 0.000915 1.468246 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: VTail Lifting Surface: Body = 5, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.210307 0.001525 0.500000 Chord: 1.210308 Arc: 2.471195 T/C: 0.120035 Type: VTail Lifting Surface: Body = 6, units m XLE: 5.484123 -0.968246 0.500000 XTE: 6.210307 -0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Lifting Surface: Body = 7, units m XLE: 5.484123 0.968246 0.500000 XTE: 6.210307 0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Body of Revolution: Body = 8, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 9, units m Arc: 3.714180 Diameter: 1.020621 Type: Fuse Body of Revolution: Body = 10, units m Arc: 2.771209 Diameter: 0.645497 Type: Fuse Body of Revolution: Body = 11, units m Arc: 1.013945 Diameter: 0.322749 Type: Fuse Body of Revolution: Body = 12, units m Arc: 0.101394 Diameter: 0.032275 Type: Fuse Number of sections 4, number of revolution sections 1 Number of Mach-Altitude cases = 2 Total drag = [0.0132, 0.01226] Form drag = [0.0033, 0.00307] Friction drag = [0.0099, 0.00919] real 0m0.633s user 0m0.659s sys 0m0.129s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tsfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results PAUSE Press the ENTER key to exit To resume execution, type go. Other input will terminate the job. Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG Cl = 0.933407 Cd = 0.000284 Cd Wave = 0.0 Cm = -0.203436 Cp _Critcal = -1.303869 real 0m0.522s user 0m0.641s sys 0m0.103s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected) ================================================= ================================================= + echo 'delaundo_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt delaundo_PyTest.py test; + python -u delaundo_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Name = AirfoilTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 6 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Name = AirfoilTE, index = 6 Getting mesh sizing parameters Mesh sizing name - Airfoil Mesh sizing name - AirfoilTE Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting edge discretization for body 1 Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping! Swapping z and y coordinates! Writing delaundo control file - delaundo.ctr Writing out *.pts file Reading delaundo mesh file - delaundo_CAPS.mesh Swapping y and z coordinates! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file real 0m0.720s user 0m0.843s sys 0m0.343s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected) ================================================= ================================================= + echo 'egadsTess_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_PyTest.py test; + python -u egadsTess_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Name = Wing, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting mesh sizing parameters Mesh sizing name - LeadingEdge Done getting mesh sizing parameters Getting surface mesh for body 1 (of 4) Getting surface mesh for body 2 (of 4) Getting surface mesh for body 3 (of 4) Getting surface mesh for body 4 (of 4) Body 1 (of 4) Number of nodes = 3793 Number of elements = 4001 Number of triangle elements = 0 Number of quadrilateral elements = 4001 Body 2 (of 4) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 3 (of 4) Number of nodes = 76 Number of elements = 55 Number of triangle elements = 0 Number of quadrilateral elements = 55 Body 4 (of 4) Number of nodes = 100 Number of elements = 73 Number of triangle elements = 0 Number of quadrilateral elements = 73 ---------------------------- Total number of nodes = 3970 Total number of elements = 4129 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file real 0m6.422s user 0m12.509s sys 0m5.004s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr2_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr2_PyTest.py test; + python -u aflr2_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 681 1018 AFLR2 GGp: Nodes, Faces = 1013 1682 AFLR2 GGp: Nodes, Faces = 1339 2334 AFLR2 GGp: Nodes, Faces = 1652 2960 AFLR2 GGp: Nodes, Faces = 1957 3570 AFLR2 GGp: Nodes, Faces = 2252 4160 AFLR2 GGp: Nodes, Faces = 2526 4708 AFLR2 GGp: Nodes, Faces = 2809 5274 AFLR2 GGp: Nodes, Faces = 3083 5822 AFLR2 GGp: Nodes, Faces = 3327 6310 AFLR2 GGp: Nodes, Faces = 3564 6784 AFLR2 GGp: Nodes, Faces = 3788 7232 AFLR2 GGp: Nodes, Faces = 3995 7646 AFLR2 GGp: Nodes, Faces = 4194 8044 AFLR2 GGp: Nodes, Faces = 4394 8444 AFLR2 GGp: Nodes, Faces = 4585 8826 AFLR2 GGp: Nodes, Faces = 4772 9200 AFLR2 GGp: Nodes, Faces = 4943 9542 AFLR2 GGp: Nodes, Faces = 5129 9914 AFLR2 GGp: Nodes, Faces = 5293 10242 AFLR2 GGp: Nodes, Faces = 5447 10550 AFLR2 GGp: Nodes, Faces = 5594 10844 AFLR2 GGp: Nodes, Faces = 5716 11088 AFLR2 GGp: Nodes, Faces = 5830 11316 AFLR2 GGp: Nodes, Faces = 5909 11474 AFLR2 GGp: Nodes, Faces = 5964 11584 AFLR2 GGp: Nodes, Faces = 6006 11668 AFLR2 GGp: Nodes, Faces = 6025 11706 AFLR2 GGp: Nodes, Faces = 6034 11724 AFLR2 : CPU Time = 0.010 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6034 11724 AFLR2 QI : Nodes, Faces = 6033 454 AFLR2 QI : Nodes, Faces = 6033 5634 AFLR2 QI : Nodes, Faces = 6033 11722 AFLR2 QI : Nodes, Faces = 6032 462 AFLR2 QI : Nodes, Faces = 6032 5629 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 456 AFLR2 QI : Nodes, Faces = 6032 5632 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 474 AFLR2 QI : Nodes, Faces = 6032 5623 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6031 486 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 QI : Nodes, Faces = 6031 488 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file real 0m0.806s user 0m0.945s sys 0m0.347s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_and_aflr3_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_and_aflr3_PyTest.py test; + python -u aflr4_and_aflr3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 150214 Number of elements = 450024 Number of triangles = 14380 Number of quadrilatarals = 0 Number of tetrahedrals = 214592 Number of pyramids = 425 Number of prisms = 220627 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m14.287s user 0m11.276s sys 0m0.368s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tetgen_PyTest.py test; + python -u tetgen_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 2236 Number of elements = 4468 Number of triangle elements = 4468 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 636 Number of elements = 1268 Number of triangle elements = 1268 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 258 Number of elements = 512 Number of triangle elements = 512 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3130 Total number of elements = 6248 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 3130, elements - 6248 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.030698 Creating surface mesh ... Surface mesh seconds: 0.006452 Recovering boundaries... Boundary recovery seconds: 0.080571 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.00354 Suppressing Steiner points ... Steiner suppression seconds: 9e-06 Recovering Delaunayness... Delaunay recovery seconds: 0.014129 Refining mesh... 4177 insertions, added 2159 points, 136953 tetrahedra in queue. 1390 insertions, added 372 points, 139199 tetrahedra in queue. 1853 insertions, added 454 points, 136118 tetrahedra in queue. 2470 insertions, added 521 points, 118263 tetrahedra in queue. 3293 insertions, added 464 points, 66933 tetrahedra in queue. 4389 insertions, added 406 points, 1337 tetrahedra in queue. 5851 insertions, added 599 points, 33 tetrahedra in queue. Refinement seconds: 0.758419 Smoothing vertices... Mesh smoothing seconds: 0.450576 Improving mesh... Mesh improvement seconds: 0.00858 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002192 Total running seconds: 1.35547 Statistics: Input points: 3130 Input facets: 6248 Input segments: 9372 Input holes: 2 Input regions: 0 Mesh points: 8156 Mesh tetrahedra: 40155 Mesh faces: 83435 Mesh faces on exterior boundary: 6250 Mesh faces on input facets: 6250 Mesh edges on input segments: 9373 Steiner points on input segments: 1 Steiner points inside domain: 5025 Done meshing using TetGen! Volume mesher did not preserve surface elements - data transfer will NOT be possible. Writing Tecplot file .... Finished writing Tecplot file real 0m3.120s user 0m2.736s sys 0m0.218s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_AFLR2_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt su2_and_AFLR2_PyTest.py test; + python -u su2_and_AFLR2_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Saving geometry Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 545 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 545 545 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 110 222 AFLR2 IG : Nodes, Faces = 220 442 AFLR2 IG : Nodes, Faces = 330 662 AFLR2 IG : Nodes, Faces = 440 882 AFLR2 IG : Nodes, Faces = 517 1036 AFLR2 IG : Nodes, Faces = 545 1092 AFLR2 IG : Nodes, Faces = 549 1092 AFLR2 IG : Nodes, Faces = 545 545 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 545 545 AFLR2 GGp: Nodes, Faces = 1083 1621 AFLR2 GGp: Nodes, Faces = 1616 2687 AFLR2 GGp: Nodes, Faces = 2144 3743 AFLR2 GGp: Nodes, Faces = 2661 4777 AFLR2 GGp: Nodes, Faces = 3171 5797 AFLR2 GGp: Nodes, Faces = 3672 6799 AFLR2 GGp: Nodes, Faces = 4158 7771 AFLR2 GGp: Nodes, Faces = 4653 8761 AFLR2 GGp: Nodes, Faces = 5142 9739 AFLR2 GGp: Nodes, Faces = 5608 10671 AFLR2 GGp: Nodes, Faces = 6055 11565 AFLR2 GGp: Nodes, Faces = 6482 12419 AFLR2 GGp: Nodes, Faces = 6880 13215 AFLR2 GGp: Nodes, Faces = 7257 13969 AFLR2 GGp: Nodes, Faces = 7614 14683 AFLR2 GGp: Nodes, Faces = 7947 15349 AFLR2 GGp: Nodes, Faces = 8276 16007 AFLR2 GGp: Nodes, Faces = 8575 16605 AFLR2 GGp: Nodes, Faces = 8869 17193 AFLR2 GGp: Nodes, Faces = 9140 17735 AFLR2 GGp: Nodes, Faces = 9401 18257 AFLR2 GGp: Nodes, Faces = 9654 18763 AFLR2 GGp: Nodes, Faces = 9887 19229 AFLR2 GGp: Nodes, Faces = 10110 19675 AFLR2 GGp: Nodes, Faces = 10315 20085 AFLR2 GGp: Nodes, Faces = 10497 20449 AFLR2 GGp: Nodes, Faces = 10656 20767 AFLR2 GGp: Nodes, Faces = 10791 21037 AFLR2 GGp: Nodes, Faces = 10919 21293 AFLR2 GGp: Nodes, Faces = 11022 21499 AFLR2 GGp: Nodes, Faces = 11092 21639 AFLR2 GGp: Nodes, Faces = 11145 21745 AFLR2 GGp: Nodes, Faces = 11156 21767 AFLR2 : CPU Time = 0.035 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 11156 21767 AFLR2 QI : Nodes, Faces = 11155 819 AFLR2 QI : Nodes, Faces = 11155 10473 AFLR2 QI : Nodes, Faces = 11155 21765 AFLR2 QI : Nodes, Faces = 11154 811 AFLR2 QI : Nodes, Faces = 11154 10476 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11154 805 AFLR2 QI : Nodes, Faces = 11154 10479 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11154 911 AFLR2 QI : Nodes, Faces = 11154 10426 AFLR2 QI : Nodes, Faces = 11154 21763 AFLR2 QI : Nodes, Faces = 11153 915 AFLR2 QI : Nodes, Faces = 11153 10423 AFLR2 QI : Nodes, Faces = 11153 917 AFLR2 QI : Nodes, Faces = 11153 10423 AFLR2 : CPU Time = 0.018 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 11153 Number of elements = 11885 Number of tris = 917 Number of quad = 10423 EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Airfoil Boundary condition name - InFlow Boundary condition name - OutFlow Boundary condition name - TunnelWall Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.4. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_5. Surface(s) plotted in the output file: BC_5, BC_2. Input mesh file name: ../aflr2/aflr2_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat. Surface file name: surface_flow_pyCAPS_su2_aflr2. Volume file name: flow_pyCAPS_su2_aflr2. Restart file name: restart_flow_pyCAPS_su2_aflr2.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 11153 grid points. 11340 volume elements. 4 surface markers. 98 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_4). 399 boundary elements in index 3 (Marker = BC_5). 917 triangles. 10423 quadrilaterals. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 917 TRIANGLE volume elements. There has been a re-orientation of 10423 QUADRILATERAL volume elements. There has been a re-orientation of 73 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.878. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 49.3184| 90| | CV Face Area Aspect Ratio| 1.00035| 33.4982| | CV Sub-Volume Ratio| 1.00001| 7.89914| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11153| 1/1.00| 10| | 1| 2702| 1/4.13| 7.38309| | 2| 549| 1/4.92| 4.99198| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.06265 m. Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m. Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is NOT a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.1771e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.1697e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.1153e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.0696e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.0313e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.0202e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.8707e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.9186e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 9.9078e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 9.7687e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.22124| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |CSV file |surface_flow_pyCAPS_su2_aflr2.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary |flow_pyCAPS_su2_aflr2.szplt | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt| Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 994 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.072253 Cd = -0.01151 Cmz = 0.070975 Cx = -0.01151 Cy = 0.072253 Pressure Contribution Cl_p = 0.072253 Cd_p = -0.01151 Cmz_p = 0.070975 Cx_p = -0.01151 Cy_p = 0.072253 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m2.894s user 0m2.355s sys 0m0.759s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected) ================================================= ./execute_PyTestRegression.sh: line 198: ulimit: stack size: cannot modify limit: Operation not permitted ================================================= + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'cart3d_PyTest.py test;' cart3d_PyTest.py test; + python -u cart3d_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Body size = 3.796888 Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out Executing: ./aero.csh > aero.out C_A 0.023693377 C_Y -0.0012129281 C_N 0.065395002 C_D 0.025961197 C_S -0.0012129281 C_L 0.064528279 C_l 0.0510971 C_m 0.000248187 C_n -0.017525 C_M_x 0.0504544 C_M_y 0.000248187 C_M_z -0.0192976 real 0m44.481s user 0m30.898s sys 0m1.465s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_ThreeBar_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_ThreeBar_PyTest.py test; + python -u astros_ThreeBar_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards real 0m1.110s user 0m0.770s sys 0m0.210s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_Flutter_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt astros_Flutter_15degree.py test; + python -u astros_Flutter_15degree.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Root_Point, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = WingSurface, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 96 Number of elements = 77 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 77 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 97 Combined Number of elements = 78 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 77 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 96 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Body Property name - Edge Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 8 automatic connections were made for capsConnect Root (node id 97) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aero card Writing analysis cards Writing constraint cards--each subcase individually Writing material cards Writing property cards Writing unsteady aeroelastic cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG real 0m1.597s user 0m0.914s sys 0m0.274s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected) ================================================= ================================================= + echo 'masstran_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results mass properties..... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1159 Number of elements = 798 Number of triangle elements = 0 Number of quadrilateral elements = 798 ---------------------------- Total number of nodes = 1159 Total number of elements = 798 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Constraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1159 Number of elements = 798 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 798 Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - Ribs_and_Spars No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Area 3.428666259749 Mass 5383.006027806 Centroid [1.222256036872, 0.1634981473779, -4.647736192456e-11] CG [1.222256036872, 0.1634981473779, -4.647907951721e-11] Ixx 22133.97306031 Iyy 23448.30046704 Izz 1389.213122564 Ixy 164.2055275655 Ixz -7.485782319314e-06 Iyz 1.710545499156e-06 I [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06] II [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]] real 0m5.598s user 0m5.760s sys 0m5.795s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected) ================================================= ================================================= + echo 'hsm_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u hsm_SingleLoadCase_PyTest.py -outLevel=0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 81 Number of elements = 96 Elemental Tria3 = 0 Elemental Quad4 = 64 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 32 ->HSMSOL Matrix Non-zero Entries = 5741 Converging HSM equation system ... iter dr dd dp rlx max 1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00) 1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00) 2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00) 2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00) 4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00) 5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00) 6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00) 7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00) Converging n vectors ... it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 ) it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 ) Converging e1,e2 vectors ... it = 1 de = 0.691E-03 rlx = 1.000 ( 45 ) it = 2 de = 0.404E-04 rlx = 1.000 ( 9 ) it = 3 de = 0.142E-07 rlx = 1.000 ( 46 ) it = 4 de = 0.521E-11 rlx = 1.000 ( 62 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat real 0m0.889s user 0m0.676s sys 0m0.073s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo '../corsairlite/qp.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt ../corsairlite/qp.py test; + python -u ../corsairlite/qp.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Objective --------- -21.56250 dimensionless Variables --------- x : 1.62500 [-] The X variable y : 1.37500 [-] The Y variable Constants --------- c : 3 [-] A constant c2 : 2 [-] A constant Sensitivities ------------- c : + 0.46957 A constant c2 : - 0.22338 A constant Solve Report ------------ Solve Method : Quadratic Program Classification : Convex Solver : cvxopt real 0m6.508s user 0m1.394s sys 0m0.146s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: abaqus awave Mystran ================================================= All tests pass! ================================================= ================================================= + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64 + mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/test/plugs + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/test/plugs + sort -f + find /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs -name 'plugs0*.csm' + awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/data/plugs/plugsFailure.txt + cp /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/JenkinsESP/data/plugs/plugsIgnore.txt . + set +x Testing CSM files: data/Plugs/plugs0a.csm data/Plugs/plugs0b.csm data/Plugs/plugs0c.csm data/Plugs/plugs0d.csm total 46336 -rw-r--r-- 1 jenkins staff 1.2M May 3 00:18 ASTRO.D01 -rw-r--r-- 1 jenkins staff 277K May 3 00:18 ASTRO.IDX -rwxr-xr-x 1 jenkins staff 130K May 3 00:19 ESPxddm -rwxr-xr-x 1 jenkins staff 212K May 3 00:18 Slugs -rwxr-xr-x 1 jenkins staff 86K May 3 00:18 TestFit -rwxr-xr-x 1 jenkins staff 1.6M May 3 00:18 avl -rwxr-xr-x 1 jenkins staff 35K May 3 00:19 cart3dTest -rwxr-xr-x 1 jenkins staff 34K May 3 00:17 egads2cart -rwxr-xr-x 1 jenkins staff 70K May 3 00:19 egads2cgt -rwxr-xr-x 1 jenkins staff 345K May 3 00:19 friction -rwxr-xr-x 1 jenkins staff 10M May 3 00:18 mastros.exe -rwxr-xr-x 1 jenkins staff 749K May 3 00:18 mses -rwxr-xr-x 1 jenkins staff 1.4M May 3 00:18 mset -rwxr-xr-x 1 jenkins staff 34K May 3 00:18 phaseUtil -rw-r--r-- 1 jenkins staff 1.6K May 3 00:20 pod.egads -rw-r--r-- 1 jenkins staff 0B May 3 00:20 port7681.jrnl -rwxr-xr-x 1 jenkins staff 1.2M May 3 00:18 pplot -rwxr-xr-x 1 jenkins staff 1.1M May 3 00:18 pxplot -rwxr-xr-x 1 jenkins staff 68K May 3 00:18 sensCSM -rwxr-xr-x 1 jenkins staff 192K May 3 00:18 serveCSM -rwxr-xr-x 1 jenkins staff 175K May 3 00:18 serveESP -rwxr-xr-x 1 jenkins staff 52K May 3 00:17 vCurvature -rwxr-xr-x 1 jenkins staff 51K May 3 00:17 vGeom -rwxr-xr-x 1 jenkins staff 36K May 3 00:17 vTess -rwxr-xr-x 1 jenkins staff 1.7M May 3 00:17 vTesstatic -rw-r--r-- 1 jenkins staff 195K May 3 00:20 wingMultiModel.bdf -rwxr-xr-x 1 jenkins staff 1.7M May 3 00:18 xfoil ( 1 / 4 ) data/Plugs/plugs0a.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0 Starting pass 3 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m9.210s user 0m6.056s sys 0m0.370s ++ set +x data/Plugs/plugs0a passed (as expected) -------------------------------------------------------------------------------------------------- ( 2 / 4 ) data/Plugs/plugs0b.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0 Starting pass 5 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m9.863s user 0m6.939s sys 0m0.075s ++ set +x data/Plugs/plugs0b passed (as expected) -------------------------------------------------------------------------------------------------- ( 3 / 4 ) data/Plugs/plugs0c.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0 Starting pass 5 (of 25) of phase2 Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0 Starting pass 6 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m24.393s user 0m28.733s sys 0m0.172s ++ set +x data/Plugs/plugs0c passed (as expected) -------------------------------------------------------------------------------------------------- ( 4 / 4 ) data/Plugs/plugs0d.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0 Starting pass 5 (of 25) of phase2 Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0 Starting pass 6 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m23.584s user 0m28.635s sys 0m0.176s ++ set +x data/Plugs/plugs0d passed (as expected) -------------------------------------------------------------------------------------------------- [Execution node] check if [viggen] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN_ARM64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.8,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #713'. [Checks API] No suitable checks publisher found. [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] done Finished: SUCCESS