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Started by upstream project "ESP_Beta" build number 717 originally caused by: Started by remote host 18.18.33.14 Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on macys_VM in workspace /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64 [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/7.7/DARWIN64 Cleaning local Directory . Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-22T10:57:45.053 -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 2496 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP doesn't exist Cleaning local Directory JenkinsESP Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-22T10:57:45.053 -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 863 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 [macys_VM] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]] Run condition [Execution node ] enabling perform for step [Execute shell] [DARWIN64] $ /bin/bash -ex /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jenkins14625061189388220367.sh + bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Beta.sh + source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 ++ [[ macys_VM == \r\e\y\n\o\l\d\s ]] ++ [[ DARWIN64 == *\.\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 ++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.8 != '' ]] ++ [[ '' != '' ]] ++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]] ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile +++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]] +++ . /usr/local/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/udunits/udunits2.xml ++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib ++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-x86-64 ++ AFLR_ARCH=MacOSX-x86-64 ++ 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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ 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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ [[ macys_VM == \m\a\c\y\s* ]] ++ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/intercept-*' ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ ln -s /usr/local/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python ++ ln -s /usr/local/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python-config ++ ln -s /usr/local/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/virtualenv +++ python-config --includes ++ export 'PYTHONINC=. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11' ++ PYTHONINC='. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation' ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.5 ++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/data + virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv created virtual environment CPython3.11.5.final.0-64 in 869ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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==69.5.1, wheel==0.43.0 activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator + . /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/activate ++ '[' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Beta.sh ']' ++ deactivate nondestructive ++ unset -f pydoc ++ '[' -z '' ']' ++ '[' -z '' ']' ++ hash -r ++ '[' -z '' ']' ++ unset VIRTUAL_ENV ++ unset VIRTUAL_ENV_PROMPT ++ '[' '!' nondestructive = nondestructive ']' ++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv ++ '[' darwin20 = cygwin ']' ++ '[' darwin20 = msys ']' ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH ++ '[' x '!=' x ']' +++ basename /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv ++ VIRTUAL_ENV_PROMPT=ESP_venv ++ export VIRTUAL_ENV_PROMPT ++ '[' -z '' ']' ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ PS1='(ESP_venv) ' ++ export PS1 ++ alias pydoc ++ true ++ hash -r + pip_install pip + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0) + pip_install f90nml + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml Collecting f90nml Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB) Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB) Installing collected packages: f90nml Successfully installed f90nml-1.4.4 + pip_install numpy + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy Collecting numpy Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl.metadata (61 kB) Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl (20.6 MB) Installing collected packages: numpy Successfully installed numpy-1.26.4 + pip_install openmdao + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao Collecting openmdao Using cached openmdao-3.32.0-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<2 in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4) Collecting packaging (from openmdao) Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB) Collecting requests (from openmdao) Using cached requests-2.32.2-py3-none-any.whl.metadata (4.6 kB) Collecting scipy (from openmdao) Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB) Collecting charset-normalizer<4,>=2 (from requests->openmdao) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.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-2.32.2-py3-none-any.whl (63 kB) Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl (39.3 MB) Using cached certifi-2024.2.2-py3-none-any.whl (163 kB) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl (121 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-3.32.0 packaging-24.0 requests-2.32.2 scipy-1.13.0 urllib3-2.2.1 + [[ macys_VM == *\v\i\g\g\e\n* ]] + pip_install cvxopt + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (1.3 kB) Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl (13.8 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 + pip_install dill + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill Collecting dill Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB) Using cached dill-0.3.8-py3-none-any.whl (116 kB) Installing collected packages: dill Successfully installed dill-0.3.8 + pip_install packaging + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0) + pip_install matplotlib + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.9.0-cp311-cp311-macosx_10_12_x86_64.whl.metadata (11 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.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_x86_64.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl.metadata (6.4 kB) Requirement already satisfied: numpy>=1.23 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_10_10_x86_64.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-3.9.0-cp311-cp311-macosx_10_12_x86_64.whl (7.9 MB) Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl (262 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_x86_64.whl (2.3 MB) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl (68 kB) Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl (3.5 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-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0 + pip_install scipy + /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 --2024-05-22 11:18:00-- 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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119M 14s 2650K .......... .......... .......... .......... .......... 1% 144M 14s 2700K .......... .......... .......... .......... .......... 1% 88.6M 13s 2750K .......... .......... .......... .......... .......... 1% 186M 13s 2800K .......... .......... .......... .......... .......... 1% 138M 13s 2850K .......... .......... .......... .......... .......... 1% 111M 13s 2900K .......... .......... .......... .......... .......... 1% 108M 13s 2950K .......... .......... .......... .......... .......... 1% 90.1M 12s 3000K .......... .......... .......... .......... .......... 1% 131M 12s 3050K .......... .......... .......... .......... .......... 1% 152M 12s 3100K .......... .......... .......... .......... .......... 1% 104M 12s 3150K .......... .......... .......... .......... .......... 1% 107M 12s 3200K .......... .......... .......... .......... .......... 1% 132M 12s 3250K .......... .......... .......... .......... .......... 1% 151M 12s 3300K .......... .......... .......... 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.......... .......... .......... .......... .......... 1% 95.9M 10s 4050K .......... .......... .......... .......... .......... 1% 133M 10s 4100K .......... .......... .......... .......... .......... 1% 108M 10s 4150K .......... .......... .......... .......... .......... 1% 119M 10s 4200K .......... .......... .......... .......... .......... 1% 109M 9s 4250K .......... .......... .......... .......... .......... 1% 79.8M 9s 4300K .......... .......... .......... .......... .......... 1% 162M 9s 4350K .......... .......... .......... .......... .......... 1% 152M 9s 4400K .......... .......... .......... .......... .......... 1% 204M 9s 4450K .......... .......... .......... .......... .......... 1% 569K 14s 4500K .......... .......... .......... .......... .......... 1% 126M 14s 4550K .......... .......... .......... .......... .......... 1% 143M 14s 4600K .......... .......... .......... .......... .......... 1% 122M 14s 4650K .......... .......... .......... .......... .......... 1% 141M 14s 4700K .......... .......... .......... .......... .......... 1% 121M 13s 4750K .......... .......... .......... .......... .......... 1% 142M 13s 4800K .......... .......... .......... .......... .......... 1% 144M 13s 4850K .......... .......... .......... .......... .......... 1% 121M 13s 4900K .......... .......... .......... .......... .......... 1% 140M 13s 4950K .......... .......... .......... .......... .......... 1% 116M 13s 5000K .......... .......... .......... .......... .......... 1% 139M 13s 5050K .......... .......... .......... .......... .......... 1% 138M 13s 5100K .......... .......... .......... .......... .......... 1% 119M 13s 5150K .......... .......... .......... .......... .......... 1% 143M 12s 5200K .......... .......... .......... .......... .......... 1% 121M 12s 5250K .......... .......... .......... .......... .......... 1% 142M 12s 5300K .......... .......... .......... .......... .......... 2% 144M 12s 5350K .......... .......... .......... .......... .......... 2% 119M 12s 5400K .......... .......... .......... .......... .......... 2% 136M 12s 5450K .......... .......... .......... .......... .......... 2% 122M 12s 5500K .......... .......... .......... .......... .......... 2% 28.3M 12s 5550K .......... .......... .......... .......... .......... 2% 119M 12s 5600K .......... .......... .......... .......... .......... 2% 36.2M 12s 5650K .......... .......... .......... .......... .......... 2% 139M 12s 5700K .......... .......... .......... .......... .......... 2% 112M 11s 5750K .......... .......... .......... .......... .......... 2% 29.3M 11s 5800K .......... .......... .......... .......... .......... 2% 119M 11s 5850K .......... .......... .......... .......... .......... 2% 1.24M 13s 5900K .......... .......... .......... .......... .......... 2% 34.9M 13s 5950K .......... .......... .......... .......... .......... 2% 110M 13s 6000K .......... .......... .......... .......... .......... 2% 135M 13s 6050K .......... .......... .......... .......... .......... 2% 140M 13s 6100K .......... .......... .......... .......... .......... 2% 138M 13s 6150K .......... .......... .......... .......... .......... 2% 151M 13s 6200K .......... .......... .......... .......... .......... 2% 117M 12s 6250K .......... .......... .......... .......... .......... 2% 121M 12s 6300K .......... .......... .......... .......... .......... 2% 154M 12s 6350K .......... .......... .......... .......... .......... 2% 24.7M 12s 6400K .......... .......... .......... .......... .......... 2% 117M 12s 6450K .......... .......... .......... .......... .......... 2% 122M 12s 6500K .......... .......... .......... .......... .......... 2% 142M 12s 6550K .......... .......... .......... .......... .......... 2% 134M 12s 6600K .......... .......... .......... .......... .......... 2% 123M 12s 6650K .......... .......... .......... .......... .......... 2% 135M 12s 6700K .......... .......... .......... .......... .......... 2% 114M 12s 6750K .......... .......... .......... .......... .......... 2% 140M 12s 6800K .......... .......... .......... .......... .......... 2% 213M 12s 6850K .......... .......... .......... .......... .......... 2% 178M 11s 6900K .......... .......... .......... .......... .......... 2% 96.3M 11s 6950K .......... .......... .......... .......... .......... 2% 133M 11s 7000K .......... .......... .......... .......... .......... 2% 143M 11s 7050K .......... .......... .......... .......... .......... 2% 218M 11s 7100K .......... .......... .......... .......... .......... 2% 155M 11s 7150K .......... .......... .......... .......... .......... 2% 180M 11s 7200K .......... .......... .......... .......... .......... 2% 177M 11s 7250K .......... .......... .......... .......... .......... 2% 152M 11s 7300K .......... .......... .......... .......... .......... 2% 1.42M 12s 7350K .......... .......... .......... .......... .......... 2% 84.9M 12s 7400K .......... .......... .......... .......... .......... 2% 50.0M 12s 7450K .......... .......... .......... .......... .......... 2% 99.9M 12s 7500K .......... .......... .......... .......... .......... 2% 121M 12s 7550K .......... .......... .......... .......... .......... 2% 94.8M 12s 7600K .......... .......... .......... .......... .......... 2% 106M 12s 7650K .......... .......... .......... .......... .......... 2% 202M 12s 7700K .......... .......... .......... .......... .......... 2% 91.3M 12s 7750K .......... .......... .......... .......... .......... 2% 145M 11s 7800K .......... .......... .......... .......... .......... 2% 120M 11s 7850K .......... .......... .......... .......... .......... 2% 112M 11s 7900K .......... .......... .......... .......... .......... 2% 153M 11s 7950K .......... .......... .......... .......... .......... 3% 90.9M 11s 8000K .......... .......... .......... .......... .......... 3% 117M 11s 8050K .......... .......... .......... .......... .......... 3% 102M 11s 8100K .......... .......... .......... .......... .......... 3% 95.9M 11s 8150K .......... .......... .......... .......... .......... 3% 47.3M 11s 8200K .......... .......... .......... .......... .......... 3% 107M 11s 8250K .......... .......... .......... .......... .......... 3% 128M 11s 8300K .......... .......... .......... .......... .......... 3% 102M 11s 8350K .......... .......... .......... .......... .......... 3% 78.9M 11s 8400K .......... .......... .......... .......... .......... 3% 145M 11s 8450K .......... .......... .......... .......... .......... 3% 134M 11s 8500K .......... .......... .......... .......... .......... 3% 100M 11s 8550K .......... .......... .......... .......... .......... 3% 84.5M 11s 8600K .......... .......... .......... .......... .......... 3% 100M 11s 8650K .......... .......... .......... .......... .......... 3% 74.5M 11s 8700K .......... .......... .......... .......... .......... 3% 1.18M 12s 8750K .......... .......... .......... .......... .......... 3% 56.3M 12s 8800K .......... .......... .......... .......... .......... 3% 207M 12s 8850K .......... .......... .......... .......... .......... 3% 132M 12s 8900K .......... .......... .......... .......... .......... 3% 146M 11s 8950K .......... .......... .......... .......... .......... 3% 132M 11s 9000K .......... .......... .......... .......... .......... 3% 211M 11s 9050K .......... .......... .......... .......... .......... 3% 222M 11s 9100K .......... .......... .......... .......... .......... 3% 138M 11s 9150K .......... .......... .......... .......... .......... 3% 133M 11s 9200K .......... .......... .......... .......... .......... 3% 32.6M 11s 9250K .......... .......... .......... .......... .......... 3% 90.8M 11s 9300K .......... .......... .......... .......... .......... 3% 123M 11s 9350K .......... .......... .......... .......... .......... 3% 162M 11s 9400K .......... .......... .......... .......... .......... 3% 154M 11s 9450K .......... .......... .......... .......... .......... 3% 173M 11s 9500K .......... .......... .......... .......... .......... 3% 115M 11s 9550K .......... .......... .......... .......... .......... 3% 142M 11s 9600K .......... .......... .......... .......... .......... 3% 78.4M 11s 9650K .......... .......... .......... .......... .......... 3% 93.4M 11s 9700K .......... .......... .......... .......... .......... 3% 72.1M 11s 9750K .......... .......... .......... .......... .......... 3% 124M 11s 9800K .......... .......... .......... .......... .......... 3% 139M 11s 9850K .......... .......... .......... .......... .......... 3% 87.3M 11s 9900K .......... .......... .......... .......... .......... 3% 80.8M 11s 9950K .......... .......... .......... .......... .......... 3% 122M 10s 10000K .......... .......... .......... .......... .......... 3% 95.9M 10s 10050K .......... .......... .......... .......... .......... 3% 1.07M 12s 10100K .......... .......... .......... .......... .......... 3% 104M 11s 10150K .......... .......... .......... .......... .......... 3% 116M 11s 10200K .......... .......... .......... .......... .......... 3% 80.3M 11s 10250K .......... .......... .......... .......... .......... 3% 174M 11s 10300K .......... .......... .......... .......... .......... 3% 231M 11s 10350K .......... .......... .......... .......... .......... 3% 163M 11s 10400K .......... .......... .......... .......... .......... 3% 143M 11s 10450K .......... .......... .......... .......... .......... 3% 138M 11s 10500K .......... .......... .......... .......... .......... 3% 188M 11s 10550K .......... .......... .......... .......... .......... 3% 160M 11s 10600K .......... .......... .......... .......... .......... 4% 137M 11s 10650K .......... .......... .......... .......... .......... 4% 150M 11s 10700K .......... .......... .......... .......... .......... 4% 115M 11s 10750K .......... .......... .......... .......... .......... 4% 122M 11s 10800K .......... .......... .......... .......... .......... 4% 131M 11s 10850K .......... .......... .......... .......... .......... 4% 109M 11s 10900K .......... .......... .......... .......... .......... 4% 153M 11s 10950K .......... .......... .......... .......... .......... 4% 104M 11s 11000K .......... .......... .......... .......... .......... 4% 133M 11s 11050K .......... .......... .......... .......... .......... 4% 124M 11s 11100K .......... .......... .......... .......... .......... 4% 144M 11s 11150K .......... .......... .......... .......... .......... 4% 137M 11s 11200K .......... .......... .......... .......... .......... 4% 110M 10s 11250K .......... .......... .......... .......... .......... 4% 71.6M 10s 11300K .......... .......... .......... .......... .......... 4% 121M 10s 11350K .......... .......... .......... .......... .......... 4% 1.49M 11s 11400K .......... .......... .......... .......... .......... 4% 88.0M 11s 11450K .......... .......... .......... .......... .......... 4% 135M 11s 11500K .......... .......... .......... .......... .......... 4% 62.9M 11s 11550K .......... .......... .......... .......... .......... 4% 83.3M 11s 11600K .......... .......... .......... .......... .......... 4% 118M 11s 11650K .......... .......... .......... .......... .......... 4% 131M 11s 11700K .......... .......... .......... .......... .......... 4% 106M 11s 11750K .......... .......... .......... .......... .......... 4% 5.51M 11s 11800K .......... .......... .......... .......... .......... 4% 35.1M 11s 11850K .......... .......... .......... .......... .......... 4% 81.1M 11s 11900K .......... .......... .......... .......... .......... 4% 139M 11s 11950K .......... .......... .......... .......... .......... 4% 166M 11s 12000K .......... .......... .......... .......... .......... 4% 201M 11s 12050K .......... .......... .......... .......... .......... 4% 203M 11s 12100K .......... .......... .......... .......... .......... 4% 109M 11s 12150K .......... .......... .......... .......... .......... 4% 126M 11s 12200K .......... .......... .......... .......... .......... 4% 100M 11s 12250K .......... .......... .......... .......... .......... 4% 1.34M 11s 12300K .......... .......... .......... .......... .......... 4% 103M 11s 12350K .......... .......... .......... .......... .......... 4% 117M 11s 12400K .......... .......... .......... .......... .......... 4% 114M 11s 12450K .......... .......... .......... .......... .......... 4% 35.5M 11s 12500K .......... .......... .......... .......... .......... 4% 128M 11s 12550K .......... .......... .......... .......... .......... 4% 110M 11s 12600K .......... .......... .......... .......... .......... 4% 130M 11s 12650K .......... .......... .......... .......... .......... 4% 88.5M 11s 12700K .......... .......... .......... .......... .......... 4% 81.4M 11s 12750K .......... .......... .......... .......... .......... 4% 84.9M 11s 12800K .......... .......... .......... .......... .......... 4% 168M 11s 12850K .......... .......... .......... .......... .......... 4% 83.6M 11s 12900K .......... .......... .......... .......... .......... 4% 141M 11s 12950K .......... .......... .......... .......... .......... 4% 117M 11s 13000K .......... .......... .......... .......... .......... 4% 145M 11s 13050K .......... .......... .......... .......... .......... 4% 138M 11s 13100K .......... .......... .......... .......... .......... 4% 126M 11s 13150K .......... .......... .......... .......... .......... 4% 226M 11s 13200K .......... .......... .......... .......... .......... 4% 193M 11s 13250K .......... .......... .......... .......... .......... 5% 224M 11s 13300K .......... .......... .......... .......... .......... 5% 4.17M 11s 13350K .......... .......... .......... .......... .......... 5% 45.6M 11s 13400K .......... .......... .......... .......... .......... 5% 161M 11s 13450K .......... .......... .......... .......... .......... 5% 162M 11s 13500K .......... .......... .......... .......... .......... 5% 178M 11s 13550K .......... .......... .......... .......... .......... 5% 135M 11s 13600K .......... .......... .......... .......... .......... 5% 79.4M 11s 13650K .......... .......... .......... .......... .......... 5% 140M 11s 13700K .......... .......... .......... .......... .......... 5% 177M 11s 13750K .......... .......... .......... .......... .......... 5% 202M 10s 13800K .......... .......... .......... .......... .......... 5% 197M 10s 13850K .......... .......... .......... .......... .......... 5% 163M 10s 13900K .......... .......... .......... .......... .......... 5% 203M 10s 13950K .......... .......... .......... .......... .......... 5% 169M 10s 14000K .......... .......... .......... .......... .......... 5% 200M 10s 14050K .......... .......... .......... .......... .......... 5% 186M 10s 14100K .......... .......... .......... .......... .......... 5% 76.2M 10s 14150K .......... .......... .......... .......... .......... 5% 184M 10s 14200K .......... .......... .......... .......... .......... 5% 145M 10s 14250K .......... .......... .......... .......... .......... 5% 87.3M 10s 14300K .......... .......... .......... .......... .......... 5% 70.1M 10s 14350K .......... .......... .......... .......... .......... 5% 75.4M 10s 14400K .......... .......... .......... .......... .......... 5% 121M 10s 14450K .......... .......... .......... .......... .......... 5% 121M 10s 14500K .......... .......... .......... .......... .......... 5% 149M 10s 14550K .......... .......... .......... .......... .......... 5% 116M 10s 14600K .......... .......... .......... .......... .......... 5% 107M 10s 14650K .......... .......... .......... .......... .......... 5% 217M 10s 14700K .......... .......... .......... .......... .......... 5% 143M 10s 14750K .......... .......... .......... .......... .......... 5% 215M 10s 14800K .......... .......... .......... .......... .......... 5% 215M 10s 14850K .......... .......... .......... .......... .......... 5% 144M 10s 14900K .......... .......... .......... .......... .......... 5% 146M 10s 14950K .......... .......... .......... .......... .......... 5% 185M 10s 15000K .......... .......... .......... .......... .......... 5% 105M 10s 15050K .......... .......... .......... .......... .......... 5% 111M 10s 15100K .......... .......... .......... .......... .......... 5% 132M 10s 15150K .......... .......... .......... .......... .......... 5% 164M 10s 15200K .......... .......... .......... .......... .......... 5% 148M 10s 15250K .......... .......... .......... .......... .......... 5% 158M 10s 15300K .......... .......... .......... .......... .......... 5% 133M 10s 15350K .......... .......... .......... .......... .......... 5% 786K 11s 15400K .......... .......... .......... .......... .......... 5% 53.8M 11s 15450K .......... .......... .......... .......... .......... 5% 35.7M 11s 15500K .......... .......... .......... .......... .......... 5% 37.0M 11s 15550K .......... .......... .......... .......... .......... 5% 59.5M 10s 15600K .......... .......... .......... .......... .......... 5% 48.3M 10s 15650K .......... .......... .......... .......... .......... 5% 61.0M 10s 15700K .......... .......... .......... .......... .......... 5% 54.3M 10s 15750K .......... .......... .......... .......... .......... 5% 51.6M 10s 15800K .......... .......... .......... .......... .......... 5% 48.1M 10s 15850K .......... .......... .......... .......... .......... 5% 37.1M 10s 15900K .......... .......... .......... .......... .......... 6% 54.8M 10s 15950K .......... .......... .......... .......... .......... 6% 54.3M 10s 16000K .......... .......... .......... .......... .......... 6% 48.0M 10s 16050K .......... .......... .......... .......... .......... 6% 31.9M 10s 16100K .......... .......... .......... .......... .......... 6% 54.0M 10s 16150K .......... .......... .......... .......... .......... 6% 69.5M 10s 16200K .......... .......... .......... .......... .......... 6% 54.1M 10s 16250K .......... .......... .......... .......... .......... 6% 53.9M 10s 16300K .......... .......... .......... .......... .......... 6% 35.8M 10s 16350K .......... .......... .......... .......... .......... 6% 2.69M 10s 16400K .......... .......... .......... .......... .......... 6% 33.9M 10s 16450K .......... .......... .......... .......... .......... 6% 34.6M 10s 16500K .......... .......... .......... .......... .......... 6% 19.3M 10s 16550K .......... .......... .......... .......... .......... 6% 115M 10s 16600K .......... .......... .......... .......... .......... 6% 181M 10s 16650K .......... .......... .......... .......... .......... 6% 219M 10s 16700K .......... .......... .......... .......... .......... 6% 174M 10s 16750K .......... .......... .......... .......... .......... 6% 210M 10s 16800K .......... .......... .......... .......... .......... 6% 222M 10s 16850K .......... .......... .......... .......... .......... 6% 191M 10s 16900K .......... .......... .......... .......... .......... 6% 217M 10s 16950K .......... .......... .......... .......... .......... 6% 196M 10s 17000K .......... .......... .......... .......... .......... 6% 224M 10s 17050K .......... .......... .......... .......... .......... 6% 223M 10s 17100K .......... .......... .......... .......... .......... 6% 192M 10s 17150K .......... .......... .......... .......... .......... 6% 225M 10s 17200K .......... .......... .......... .......... .......... 6% 193M 10s 17250K .......... .......... .......... .......... .......... 6% 222M 10s 17300K .......... .......... .......... .......... .......... 6% 226M 10s 17350K .......... .......... .......... .......... .......... 6% 191M 10s 17400K .......... .......... .......... .......... .......... 6% 18.6M 10s 17450K .......... .......... .......... .......... .......... 6% 70.4M 10s 17500K .......... .......... .......... .......... .......... 6% 127M 10s 17550K .......... .......... .......... .......... .......... 6% 145M 10s 17600K .......... .......... .......... .......... .......... 6% 129M 10s 17650K .......... .......... .......... .......... .......... 6% 173M 10s 17700K .......... .......... .......... .......... .......... 6% 180M 10s 17750K .......... .......... .......... .......... .......... 6% 170M 10s 17800K .......... .......... .......... .......... .......... 6% 201M 10s 17850K .......... .......... .......... .......... .......... 6% 113M 10s 17900K .......... .......... .......... .......... .......... 6% 193M 10s 17950K .......... .......... .......... .......... .......... 6% 114M 10s 18000K .......... .......... .......... .......... .......... 6% 131M 10s 18050K .......... .......... .......... .......... .......... 6% 208M 10s 18100K .......... .......... .......... .......... .......... 6% 114M 10s 18150K .......... .......... .......... .......... .......... 6% 143M 10s 18200K .......... .......... .......... .......... .......... 6% 119M 10s 18250K .......... .......... .......... .......... .......... 6% 132M 10s 18300K .......... .......... .......... .......... .......... 6% 151M 10s 18350K .......... .......... .......... .......... .......... 6% 125M 10s 18400K .......... .......... .......... .......... .......... 6% 2.31M 10s 18450K .......... .......... .......... .......... .......... 6% 26.8M 10s 18500K .......... .......... .......... .......... .......... 6% 141M 10s 18550K .......... .......... .......... .......... .......... 6% 207M 10s 18600K .......... .......... .......... .......... .......... 7% 92.1M 10s 18650K .......... .......... .......... .......... .......... 7% 163M 10s 18700K .......... .......... .......... .......... .......... 7% 100M 10s 18750K .......... .......... .......... .......... .......... 7% 205M 10s 18800K .......... .......... .......... .......... .......... 7% 147M 10s 18850K .......... .......... .......... .......... .......... 7% 139M 10s 18900K .......... .......... .......... .......... .......... 7% 142M 10s 18950K .......... .......... .......... .......... .......... 7% 166M 10s 19000K .......... .......... .......... .......... .......... 7% 120M 9s 19050K .......... .......... .......... .......... .......... 7% 95.2M 9s 19100K .......... .......... .......... .......... .......... 7% 113M 9s 19150K .......... .......... .......... .......... .......... 7% 115M 9s 19200K .......... .......... .......... .......... .......... 7% 69.2M 9s 19250K .......... .......... .......... .......... .......... 7% 200M 9s 19300K .......... .......... .......... .......... .......... 7% 90.3M 9s 19350K .......... .......... .......... .......... .......... 7% 141M 9s 19400K .......... .......... .......... .......... .......... 7% 163M 9s 19450K .......... .......... .......... .......... .......... 7% 118M 9s 19500K .......... .......... .......... .......... .......... 7% 166M 9s 19550K .......... .......... .......... .......... .......... 7% 167M 9s 19600K .......... .......... .......... .......... .......... 7% 120M 9s 19650K .......... .......... .......... .......... .......... 7% 153M 9s 19700K .......... .......... .......... .......... .......... 7% 128M 9s 19750K .......... .......... .......... .......... .......... 7% 137M 9s 19800K .......... .......... .......... .......... .......... 7% 151M 9s 19850K .......... .......... .......... .......... .......... 7% 141M 9s 19900K .......... .......... .......... .......... .......... 7% 161M 9s 19950K .......... .......... .......... .......... .......... 7% 144M 9s 20000K .......... .......... .......... .......... .......... 7% 165M 9s 20050K .......... .......... .......... .......... .......... 7% 164M 9s 20100K .......... .......... .......... .......... .......... 7% 140M 9s 20150K .......... .......... .......... .......... .......... 7% 166M 9s 20200K .......... .......... .......... .......... .......... 7% 141M 9s 20250K .......... .......... .......... .......... .......... 7% 164M 9s 20300K .......... .......... .......... .......... .......... 7% 166M 9s 20350K .......... .......... .......... .......... .......... 7% 140M 9s 20400K .......... .......... .......... .......... .......... 7% 161M 9s 20450K .......... .......... .......... .......... .......... 7% 115M 9s 20500K .......... .......... .......... .......... .......... 7% 152M 9s 20550K .......... .......... .......... .......... .......... 7% 161M 9s 20600K .......... .......... .......... .......... .......... 7% 137M 9s 20650K .......... .......... .......... .......... .......... 7% 164M 9s 20700K .......... .......... .......... .......... .......... 7% 140M 9s 20750K .......... .......... .......... .......... .......... 7% 160M 9s 20800K .......... .......... .......... .......... .......... 7% 166M 9s 20850K .......... .......... .......... .......... .......... 7% 138M 9s 20900K .......... .......... .......... .......... .......... 7% 159M 9s 20950K .......... .......... .......... .......... .......... 7% 140M 9s 21000K .......... .......... .......... .......... .......... 7% 160M 9s 21050K .......... .......... .......... .......... .......... 7% 160M 9s 21100K .......... .......... .......... .......... .......... 7% 135M 9s 21150K .......... .......... .......... .......... .......... 7% 163M 9s 21200K .......... .......... .......... .......... .......... 7% 136M 9s 21250K .......... .......... .......... .......... .......... 8% 159M 9s 21300K .......... .......... .......... .......... .......... 8% 162M 9s 21350K .......... .......... .......... .......... .......... 8% 137M 9s 21400K .......... .......... .......... .......... .......... 8% 155M 9s 21450K .......... .......... .......... .......... .......... 8% 135M 9s 21500K .......... .......... .......... .......... .......... 8% 479K 10s 21550K .......... .......... .......... .......... .......... 8% 143M 10s 21600K .......... .......... .......... .......... .......... 8% 109M 10s 21650K .......... .......... .......... .......... .......... 8% 160M 10s 21700K .......... .......... .......... .......... .......... 8% 137M 10s 21750K .......... .......... .......... .......... .......... 8% 51.8M 10s 21800K .......... .......... .......... .......... .......... 8% 35.3M 10s 21850K .......... .......... .......... .......... .......... 8% 98.6M 10s 21900K .......... .......... .......... .......... .......... 8% 131M 10s 21950K .......... .......... .......... .......... .......... 8% 48.2M 10s 22000K .......... .......... .......... .......... .......... 8% 159M 10s 22050K .......... .......... .......... .......... .......... 8% 131M 9s 22100K .......... .......... .......... .......... .......... 8% 83.8M 9s 22150K .......... .......... .......... .......... .......... 8% 31.9M 9s 22200K .......... .......... .......... .......... .......... 8% 88.3M 9s 22250K .......... .......... .......... .......... .......... 8% 112M 9s 22300K .......... .......... .......... .......... .......... 8% 82.1M 9s 22350K .......... .......... .......... .......... .......... 8% 74.2M 9s 22400K .......... .......... .......... .......... .......... 8% 133M 9s 22450K .......... .......... .......... .......... .......... 8% 125M 9s 22500K .......... .......... .......... .......... .......... 8% 28.5M 9s 22550K .......... .......... .......... .......... .......... 8% 120M 9s 22600K .......... .......... .......... .......... .......... 8% 74.5M 9s 22650K .......... .......... .......... .......... .......... 8% 133M 9s 22700K .......... .......... .......... .......... .......... 8% 114M 9s 22750K .......... .......... .......... .......... .......... 8% 159M 9s 22800K .......... .......... .......... .......... .......... 8% 113M 9s 22850K .......... .......... .......... .......... .......... 8% 131M 9s 22900K .......... .......... 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23600K .......... .......... .......... .......... .......... 8% 82.2M 9s 23650K .......... .......... .......... .......... .......... 8% 121M 9s 23700K .......... .......... .......... .......... .......... 8% 126M 9s 23750K .......... .......... .......... .......... .......... 8% 145M 9s 23800K .......... .......... .......... .......... .......... 8% 149M 9s 23850K .......... .......... .......... .......... .......... 8% 93.0M 9s 23900K .......... .......... .......... .......... .......... 9% 108M 9s 23950K .......... .......... .......... .......... .......... 9% 120M 9s 24000K .......... .......... .......... .......... .......... 9% 122M 9s 24050K .......... .......... .......... .......... .......... 9% 86.6M 9s 24100K .......... .......... .......... .......... .......... 9% 78.8M 9s 24150K .......... .......... .......... .......... .......... 9% 144M 9s 24200K .......... .......... .......... .......... .......... 9% 170M 9s 24250K .......... .......... .......... 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.......... 9% 1002K 9s 25650K .......... .......... .......... .......... .......... 9% 108M 9s 25700K .......... .......... .......... .......... .......... 9% 97.7M 9s 25750K .......... .......... .......... .......... .......... 9% 89.4M 9s 25800K .......... .......... .......... .......... .......... 9% 107M 9s 25850K .......... .......... .......... .......... .......... 9% 93.9M 9s 25900K .......... .......... .......... .......... .......... 9% 133M 9s 25950K .......... .......... .......... .......... .......... 9% 121M 9s 26000K .......... .......... .......... .......... .......... 9% 176M 9s 26050K .......... .......... .......... .......... .......... 9% 139M 9s 26100K .......... .......... .......... .......... .......... 9% 84.2M 9s 26150K .......... .......... .......... .......... .......... 9% 145M 9s 26200K .......... .......... .......... .......... .......... 9% 130M 9s 26250K .......... .......... .......... .......... .......... 9% 138M 9s 26300K .......... 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.......... 10% 144M 9s 27000K .......... .......... .......... .......... .......... 10% 154M 9s 27050K .......... .......... .......... .......... .......... 10% 212M 9s 27100K .......... .......... .......... .......... .......... 10% 205M 9s 27150K .......... .......... .......... .......... .......... 10% 223M 9s 27200K .......... .......... .......... .......... .......... 10% 160M 9s 27250K .......... .......... .......... .......... .......... 10% 231M 9s 27300K .......... .......... .......... .......... .......... 10% 233M 9s 27350K .......... .......... .......... .......... .......... 10% 204M 9s 27400K .......... .......... .......... .......... .......... 10% 230M 9s 27450K .......... .......... .......... .......... .......... 10% 151M 9s 27500K .......... .......... .......... .......... .......... 10% 223M 9s 27550K .......... .......... .......... .......... .......... 10% 185M 9s 27600K .......... .......... .......... .......... .......... 10% 33.5M 9s 27650K 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.......... .......... .......... 11% 334M 9s 29700K .......... .......... .......... .......... .......... 11% 203M 9s 29750K .......... .......... .......... .......... .......... 11% 298M 9s 29800K .......... .......... .......... .......... .......... 11% 339M 9s 29850K .......... .......... .......... .......... .......... 11% 289M 9s 29900K .......... .......... .......... .......... .......... 11% 344M 9s 29950K .......... .......... .......... .......... .......... 11% 296M 9s 30000K .......... .......... .......... .......... .......... 11% 341M 9s 30050K .......... .......... .......... .......... .......... 11% 341M 9s 30100K .......... .......... .......... .......... .......... 11% 291M 9s 30150K .......... .......... .......... .......... .......... 11% 344M 9s 30200K .......... .......... .......... .......... .......... 11% 291M 9s 30250K .......... .......... .......... .......... .......... 11% 344M 9s 30300K .......... .......... .......... .......... .......... 11% 346M 9s 30350K .......... .......... .......... .......... .......... 11% 292M 9s 30400K .......... .......... .......... .......... .......... 11% 341M 9s 30450K .......... .......... .......... .......... .......... 11% 300M 9s 30500K .......... .......... .......... .......... .......... 11% 339M 9s 30550K .......... .......... .......... .......... .......... 11% 344M 9s 30600K .......... .......... .......... .......... .......... 11% 289M 9s 30650K .......... .......... .......... .......... .......... 11% 344M 8s 30700K .......... .......... .......... .......... .......... 11% 225M 8s 30750K .......... .......... .......... .......... .......... 11% 321M 8s 30800K .......... .......... .......... .......... .......... 11% 344M 8s 30850K .......... .......... .......... .......... .......... 11% 201M 8s 30900K .......... .......... .......... .......... .......... 11% 337M 8s 30950K .......... .......... .......... .......... .......... 11% 296M 8s 31000K .......... .......... 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337M 8s 31700K .......... .......... .......... .......... .......... 11% 1.85M 8s 31750K .......... .......... .......... .......... .......... 11% 40.5M 8s 31800K .......... .......... .......... .......... .......... 11% 44.3M 8s 31850K .......... .......... .......... .......... .......... 12% 70.9M 8s 31900K .......... .......... .......... .......... .......... 12% 46.4M 8s 31950K .......... .......... .......... .......... .......... 12% 44.4M 8s 32000K .......... .......... .......... .......... .......... 12% 61.5M 8s 32050K .......... .......... .......... .......... .......... 12% 59.0M 8s 32100K .......... .......... .......... .......... .......... 12% 38.5M 8s 32150K .......... .......... .......... .......... .......... 12% 58.8M 8s 32200K .......... .......... .......... .......... .......... 12% 54.5M 8s 32250K .......... .......... .......... .......... .......... 12% 74.9M 8s 32300K .......... .......... .......... .......... .......... 12% 86.6M 8s 32350K .......... .......... .......... .......... .......... 12% 35.5M 8s 32400K .......... .......... .......... .......... .......... 12% 54.2M 8s 32450K .......... .......... .......... .......... .......... 12% 35.6M 8s 32500K .......... .......... .......... .......... .......... 12% 53.8M 8s 32550K .......... .......... .......... .......... .......... 12% 60.4M 8s 32600K .......... .......... .......... .......... .......... 12% 50.7M 8s 32650K .......... .......... .......... .......... .......... 12% 95.7M 8s 32700K .......... .......... .......... .......... .......... 12% 67.8M 8s 32750K .......... .......... .......... .......... .......... 12% 7.09M 8s 32800K .......... .......... .......... .......... .......... 12% 1.30M 9s 32850K .......... .......... .......... .......... .......... 12% 34.7M 9s 32900K .......... .......... .......... .......... .......... 12% 148M 8s 32950K .......... .......... .......... .......... .......... 12% 5.38M 9s 33000K .......... .......... .......... 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33700K .......... .......... .......... .......... .......... 12% 153M 8s 33750K .......... .......... .......... .......... .......... 12% 2.91M 8s 33800K .......... .......... .......... .......... .......... 12% 45.8M 8s 33850K .......... .......... .......... .......... .......... 12% 113M 8s 33900K .......... .......... .......... .......... .......... 12% 152M 8s 33950K .......... .......... .......... .......... .......... 12% 13.2M 8s 34000K .......... .......... .......... .......... .......... 12% 199M 8s 34050K .......... .......... .......... .......... .......... 12% 198M 8s 34100K .......... .......... .......... .......... .......... 12% 182M 8s 34150K .......... .......... .......... .......... .......... 12% 219M 8s 34200K .......... .......... .......... .......... .......... 12% 185M 8s 34250K .......... .......... .......... .......... .......... 12% 140M 8s 34300K .......... .......... .......... .......... .......... 12% 193M 8s 34350K .......... .......... 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201M 8s 35050K .......... .......... .......... .......... .......... 13% 233M 8s 35100K .......... .......... .......... .......... .......... 13% 179M 8s 35150K .......... .......... .......... .......... .......... 13% 185M 8s 35200K .......... .......... .......... .......... .......... 13% 127M 8s 35250K .......... .......... .......... .......... .......... 13% 172M 8s 35300K .......... .......... .......... .......... .......... 13% 118M 8s 35350K .......... .......... .......... .......... .......... 13% 132M 8s 35400K .......... .......... .......... .......... .......... 13% 270M 8s 35450K .......... .......... .......... .......... .......... 13% 121M 8s 35500K .......... .......... .......... .......... .......... 13% 176M 8s 35550K .......... .......... .......... .......... .......... 13% 225M 8s 35600K .......... .......... .......... .......... .......... 13% 203M 8s 35650K .......... .......... .......... .......... .......... 13% 328M 8s 35700K .......... .......... 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286M 8s 36400K .......... .......... .......... .......... .......... 13% 296M 8s 36450K .......... .......... .......... .......... .......... 13% 5.77M 8s 36500K .......... .......... .......... .......... .......... 13% 40.2M 8s 36550K .......... .......... .......... .......... .......... 13% 183M 8s 36600K .......... .......... .......... .......... .......... 13% 171M 8s 36650K .......... .......... .......... .......... .......... 13% 156M 8s 36700K .......... .......... .......... .......... .......... 13% 170M 8s 36750K .......... .......... .......... .......... .......... 13% 168M 8s 36800K .......... .......... .......... .......... .......... 13% 136M 8s 36850K .......... .......... .......... .......... .......... 13% 6.28M 8s 36900K .......... .......... .......... .......... .......... 13% 28.9M 8s 36950K .......... .......... .......... .......... .......... 13% 156M 8s 37000K .......... .......... .......... .......... .......... 13% 129M 8s 37050K .......... 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210M 8s 41100K .......... .......... .......... .......... .......... 15% 111M 8s 41150K .......... .......... .......... .......... .......... 15% 211M 8s 41200K .......... .......... .......... .......... .......... 15% 234M 8s 41250K .......... .......... .......... .......... .......... 15% 311M 8s 41300K .......... .......... .......... .......... .......... 15% 212M 8s 41350K .......... .......... .......... .......... .......... 15% 180M 8s 41400K .......... .......... .......... .......... .......... 15% 239M 8s 41450K .......... .......... .......... .......... .......... 15% 277M 8s 41500K .......... .......... .......... .......... .......... 15% 157M 8s 41550K .......... .......... .......... .......... .......... 15% 326M 8s 41600K .......... .......... .......... .......... .......... 15% 204M 8s 41650K .......... .......... .......... .......... .......... 15% 5.61M 8s 41700K .......... .......... .......... .......... .......... 15% 86.0M 8s 41750K .......... .......... 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17% 77.1M 8s 47150K .......... .......... .......... .......... .......... 17% 154M 8s 47200K .......... .......... .......... .......... .......... 17% 205M 8s 47250K .......... .......... .......... .......... .......... 17% 233M 8s 47300K .......... .......... .......... .......... .......... 17% 176M 8s 47350K .......... .......... .......... .......... .......... 17% 171M 8s 47400K .......... .......... .......... .......... .......... 17% 326M 8s 47450K .......... .......... .......... .......... .......... 17% 175M 8s 47500K .......... .......... .......... .......... .......... 17% 3.46M 8s 47550K .......... .......... .......... .......... .......... 17% 131M 8s 47600K .......... .......... .......... .......... .......... 17% 190M 8s 47650K .......... .......... .......... .......... .......... 17% 225M 8s 47700K .......... .......... .......... .......... .......... 17% 198M 8s 47750K .......... .......... .......... .......... .......... 17% 231M 8s 47800K .......... 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.......... 18% 113M 8s 48500K .......... .......... .......... .......... .......... 18% 201M 8s 48550K .......... .......... .......... .......... .......... 18% 337M 8s 48600K .......... .......... .......... .......... .......... 18% 281M 8s 48650K .......... .......... .......... .......... .......... 18% 344M 8s 48700K .......... .......... .......... .......... .......... 18% 252M 8s 48750K .......... .......... .......... .......... .......... 18% 344M 8s 48800K .......... .......... .......... .......... .......... 18% 3.60M 8s 48850K .......... .......... .......... .......... .......... 18% 84.2M 8s 48900K .......... .......... .......... .......... .......... 18% 177M 8s 48950K .......... .......... .......... .......... .......... 18% 189M 8s 49000K .......... .......... .......... .......... .......... 18% 214M 8s 49050K .......... .......... .......... .......... .......... 18% 142M 8s 49100K .......... .......... .......... .......... .......... 18% 136M 8s 49150K .......... .......... .......... .......... .......... 18% 65.4M 8s 49200K .......... .......... .......... .......... .......... 18% 3.07M 8s 49250K .......... .......... .......... .......... .......... 18% 155M 8s 49300K .......... .......... .......... .......... .......... 18% 46.7M 8s 49350K .......... .......... .......... .......... .......... 18% 177M 8s 49400K .......... .......... .......... .......... .......... 18% 248M 8s 49450K .......... .......... .......... .......... .......... 18% 273M 8s 49500K .......... .......... .......... .......... .......... 18% 344M 8s 49550K .......... .......... .......... .......... .......... 18% 287M 8s 49600K .......... .......... .......... .......... .......... 18% 107M 7s 49650K .......... .......... .......... .......... .......... 18% 3.56M 8s 49700K .......... .......... .......... .......... .......... 18% 169M 8s 49750K .......... .......... .......... .......... .......... 18% 222M 8s 49800K .......... .......... .......... 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50500K .......... .......... .......... .......... .......... 19% 3.31M 8s 50550K .......... .......... .......... .......... .......... 19% 195M 8s 50600K .......... .......... .......... .......... .......... 19% 129M 8s 50650K .......... .......... .......... .......... .......... 19% 191M 8s 50700K .......... .......... .......... .......... .......... 19% 105M 8s 50750K .......... .......... .......... .......... .......... 19% 195M 7s 50800K .......... .......... .......... .......... .......... 19% 168M 7s 50850K .......... .......... .......... .......... .......... 19% 163M 7s 50900K .......... .......... .......... .......... .......... 19% 184M 7s 50950K .......... .......... .......... .......... .......... 19% 3.53M 8s 51000K .......... .......... .......... .......... .......... 19% 281M 8s 51050K .......... .......... .......... .......... .......... 19% 236M 8s 51100K .......... .......... .......... .......... .......... 19% 175M 7s 51150K .......... .......... 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19% 3.36M 8s 51850K .......... .......... .......... .......... .......... 19% 112M 8s 51900K .......... .......... .......... .......... .......... 19% 41.2M 8s 51950K .......... .......... .......... .......... .......... 19% 169M 7s 52000K .......... .......... .......... .......... .......... 19% 321M 7s 52050K .......... .......... .......... .......... .......... 19% 161M 7s 52100K .......... .......... .......... .......... .......... 19% 114M 7s 52150K .......... .......... .......... .......... .......... 19% 104M 7s 52200K .......... .......... .......... .......... .......... 19% 19.1M 7s 52250K .......... .......... .......... .......... .......... 19% 2.88M 8s 52300K .......... .......... .......... .......... .......... 19% 147M 8s 52350K .......... .......... .......... .......... .......... 19% 116M 8s 52400K .......... .......... .......... .......... .......... 19% 163M 8s 52450K .......... .......... .......... .......... .......... 19% 140M 8s 52500K .......... 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64600K .......... .......... .......... .......... .......... 24% 207M 7s 64650K .......... .......... .......... .......... .......... 24% 243M 7s 64700K .......... .......... .......... .......... .......... 24% 3.45M 8s 64750K .......... .......... .......... .......... .......... 24% 191M 7s 64800K .......... .......... .......... .......... .......... 24% 223M 7s 64850K .......... .......... .......... .......... .......... 24% 113M 7s 64900K .......... .......... .......... .......... .......... 24% 210M 7s 64950K .......... .......... .......... .......... .......... 24% 179M 7s 65000K .......... .......... .......... .......... .......... 24% 1.65M 8s 65050K .......... .......... .......... .......... .......... 24% 164M 8s 65100K .......... .......... .......... .......... .......... 24% 162M 8s 65150K .......... .......... .......... .......... .......... 24% 138M 8s 65200K .......... .......... .......... .......... .......... 24% 204M 8s 65250K .......... .......... 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8s 82050K .......... .......... .......... .......... .......... 30% 270M 8s 82100K .......... .......... .......... .......... .......... 30% 90.9M 8s 82150K .......... .......... .......... .......... .......... 30% 119M 8s 82200K .......... .......... .......... .......... .......... 30% 184M 8s 82250K .......... .......... .......... .......... .......... 30% 146M 8s 82300K .......... .......... .......... .......... .......... 30% 4.82M 8s 82350K .......... .......... .......... .......... .......... 31% 185M 8s 82400K .......... .......... .......... .......... .......... 31% 305M 8s 82450K .......... .......... .......... .......... .......... 31% 135M 8s 82500K .......... .......... .......... .......... .......... 31% 210M 8s 82550K .......... .......... .......... .......... .......... 31% 158M 8s 82600K .......... .......... .......... .......... .......... 31% 176M 8s 82650K .......... .......... .......... .......... .......... 31% 4.39M 8s 82700K .......... .......... 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92800K .......... .......... .......... .......... .......... 34% 2.95M 8s 92850K .......... .......... .......... .......... .......... 34% 119M 8s 92900K .......... .......... .......... .......... .......... 34% 194M 8s 92950K .......... .......... .......... .......... .......... 34% 196M 8s 93000K .......... .......... .......... .......... .......... 35% 226M 8s 93050K .......... .......... .......... .......... .......... 35% 217M 8s 93100K .......... .......... .......... .......... .......... 35% 134M 8s 93150K .......... .......... .......... .......... .......... 35% 170M 8s 93200K .......... .......... .......... .......... .......... 35% 2.94M 8s 93250K .......... .......... .......... .......... .......... 35% 158M 8s 93300K .......... .......... .......... .......... .......... 35% 192M 8s 93350K .......... .......... .......... .......... .......... 35% 210M 8s 93400K .......... .......... .......... .......... .......... 35% 168M 8s 93450K .......... .......... 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35% 40.4M 8s 94150K .......... .......... .......... .......... .......... 35% 315M 8s 94200K .......... .......... .......... .......... .......... 35% 223M 8s 94250K .......... .......... .......... .......... .......... 35% 346M 8s 94300K .......... .......... .......... .......... .......... 35% 346M 8s 94350K .......... .......... .......... .......... .......... 35% 3.45M 8s 94400K .......... .......... .......... .......... .......... 35% 182M 8s 94450K .......... .......... .......... .......... .......... 35% 167M 8s 94500K .......... .......... .......... .......... .......... 35% 190M 8s 94550K .......... .......... .......... .......... .......... 35% 203M 8s 94600K .......... .......... .......... .......... .......... 35% 167M 8s 94650K .......... .......... .......... .......... .......... 35% 146M 8s 94700K .......... .......... .......... .......... .......... 35% 298M 8s 94750K .......... .......... .......... .......... .......... 35% 3.30M 8s 94800K .......... 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7s 100850K .......... .......... .......... .......... .......... 37% 156M 7s 100900K .......... .......... .......... .......... .......... 37% 130M 7s 100950K .......... .......... .......... .......... .......... 38% 164M 7s 101000K .......... .......... .......... .......... .......... 38% 245M 7s 101050K .......... .......... .......... .......... .......... 38% 3.01M 7s 101100K .......... .......... .......... .......... .......... 38% 248M 7s 101150K .......... .......... .......... .......... .......... 38% 221M 7s 101200K .......... .......... .......... .......... .......... 38% 142M 7s 101250K .......... .......... .......... .......... .......... 38% 282M 7s 101300K .......... .......... .......... .......... .......... 38% 334M 7s 101350K .......... .......... .......... .......... .......... 38% 3.12M 7s 101400K .......... .......... .......... .......... .......... 38% 214M 7s 101450K .......... .......... .......... .......... .......... 38% 3.64M 7s 101500K .......... 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.......... 40% 169M 7s 107500K .......... .......... .......... .......... .......... 40% 12.2M 7s 107550K .......... .......... .......... .......... .......... 40% 27.8M 7s 107600K .......... .......... .......... .......... .......... 40% 2.70M 7s 107650K .......... .......... .......... .......... .......... 40% 226M 7s 107700K .......... .......... .......... .......... .......... 40% 195M 7s 107750K .......... .......... .......... .......... .......... 40% 214M 7s 107800K .......... .......... .......... .......... .......... 40% 205M 7s 107850K .......... .......... .......... .......... .......... 40% 197M 7s 107900K .......... .......... .......... .......... .......... 40% 191M 7s 107950K .......... .......... .......... .......... .......... 40% 203M 7s 108000K .......... .......... .......... .......... .......... 40% 2.61M 7s 108050K .......... .......... .......... .......... .......... 40% 271M 7s 108100K .......... .......... .......... .......... .......... 40% 258M 7s 108150K .......... .......... .......... .......... .......... 40% 252M 7s 108200K .......... .......... .......... .......... .......... 40% 184M 7s 108250K .......... .......... .......... .......... .......... 40% 241M 7s 108300K .......... .......... .......... .......... .......... 40% 216M 7s 108350K .......... .......... .......... .......... .......... 40% 198M 7s 108400K .......... .......... .......... .......... .......... 40% 2.44M 7s 108450K .......... .......... .......... .......... .......... 40% 142M 7s 108500K .......... .......... .......... .......... .......... 40% 7.84M 7s 108550K .......... .......... .......... .......... .......... 40% 113M 7s 108600K .......... .......... .......... .......... .......... 40% 95.2M 7s 108650K .......... .......... .......... .......... .......... 40% 108M 7s 108700K .......... .......... .......... .......... .......... 40% 70.1M 7s 108750K .......... .......... .......... .......... .......... 40% 231M 7s 108800K .......... 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41% 4.08M 7s 110150K .......... .......... .......... .......... .......... 41% 87.2M 7s 110200K .......... .......... .......... .......... .......... 41% 71.5M 7s 110250K .......... .......... .......... .......... .......... 41% 191M 7s 110300K .......... .......... .......... .......... .......... 41% 165M 7s 110350K .......... .......... .......... .......... .......... 41% 128M 7s 110400K .......... .......... .......... .......... .......... 41% 153M 7s 110450K .......... .......... .......... .......... .......... 41% 160M 7s 110500K .......... .......... .......... .......... .......... 41% 3.42M 7s 110550K .......... .......... .......... .......... .......... 41% 10.1M 7s 110600K .......... .......... .......... .......... .......... 41% 164M 7s 110650K .......... .......... .......... .......... .......... 41% 165M 7s 110700K .......... .......... .......... .......... .......... 41% 218M 7s 110750K .......... .......... .......... .......... .......... 41% 136M 7s 110800K 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.......... 42% 179M 7s 112150K .......... .......... .......... .......... .......... 42% 210M 7s 112200K .......... .......... .......... .......... .......... 42% 2.53M 7s 112250K .......... .......... .......... .......... .......... 42% 99.2M 7s 112300K .......... .......... .......... .......... .......... 42% 238M 7s 112350K .......... .......... .......... .......... .......... 42% 267M 7s 112400K .......... .......... .......... .......... .......... 42% 339M 7s 112450K .......... .......... .......... .......... .......... 42% 274M 7s 112500K .......... .......... .......... .......... .......... 42% 303M 7s 112550K .......... .......... .......... .......... .......... 42% 154M 7s 112600K .......... .......... .......... .......... .......... 42% 1.85M 7s 112650K .......... .......... .......... .......... .......... 42% 50.9M 7s 112700K .......... .......... .......... .......... .......... 42% 36.9M 7s 112750K .......... .......... .......... .......... .......... 42% 164M 7s 112800K .......... .......... .......... .......... .......... 42% 89.1M 7s 112850K .......... .......... .......... .......... .......... 42% 65.1M 7s 112900K .......... .......... .......... .......... .......... 42% 38.7M 7s 112950K .......... .......... .......... .......... .......... 42% 2.65M 7s 113000K .......... .......... .......... .......... .......... 42% 1.61M 7s 113050K .......... .......... .......... .......... .......... 42% 20.2M 7s 113100K .......... .......... .......... .......... .......... 42% 18.5M 7s 113150K .......... .......... .......... .......... .......... 42% 26.7M 7s 113200K .......... .......... .......... .......... .......... 42% 102M 7s 113250K .......... .......... .......... .......... .......... 42% 42.2M 7s 113300K .......... .......... .......... .......... .......... 42% 43.0M 7s 113350K .......... .......... .......... .......... .......... 42% 73.3M 7s 113400K .......... .......... .......... .......... .......... 42% 51.7M 7s 113450K 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116100K .......... .......... .......... .......... .......... 43% 281M 7s 116150K .......... .......... .......... .......... .......... 43% 332M 7s 116200K .......... .......... .......... .......... .......... 43% 161M 7s 116250K .......... .......... .......... .......... .......... 43% 155M 7s 116300K .......... .......... .......... .......... .......... 43% 294M 7s 116350K .......... .......... .......... .......... .......... 43% 242M 7s 116400K .......... .......... .......... .......... .......... 43% 219M 7s 116450K .......... .......... .......... .......... .......... 43% 2.36M 7s 116500K .......... .......... .......... .......... .......... 43% 198M 7s 116550K .......... .......... .......... .......... .......... 43% 229M 7s 116600K .......... .......... .......... .......... .......... 43% 199M 7s 116650K .......... .......... .......... .......... .......... 43% 234M 7s 116700K .......... .......... .......... .......... .......... 43% 11.1M 7s 116750K .......... 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.......... 44% 20.4M 7s 118100K .......... .......... .......... .......... .......... 44% 18.4M 7s 118150K .......... .......... .......... .......... .......... 44% 3.07M 7s 118200K .......... .......... .......... .......... .......... 44% 121M 7s 118250K .......... .......... .......... .......... .......... 44% 11.9M 7s 118300K .......... .......... .......... .......... .......... 44% 59.1M 7s 118350K .......... .......... .......... .......... .......... 44% 186M 7s 118400K .......... .......... .......... .......... .......... 44% 159M 7s 118450K .......... .......... .......... .......... .......... 44% 85.2M 7s 118500K .......... .......... .......... .......... .......... 44% 301M 7s 118550K .......... .......... .......... .......... .......... 44% 311M 7s 118600K .......... .......... .......... .......... .......... 44% 286M 7s 118650K .......... .......... .......... .......... .......... 44% 4.46M 7s 118700K .......... .......... .......... .......... .......... 44% 108M 7s 118750K .......... .......... .......... .......... .......... 44% 5.17M 7s 118800K .......... .......... .......... .......... .......... 44% 28.2M 7s 118850K .......... .......... .......... .......... .......... 44% 92.7M 7s 118900K .......... .......... .......... .......... .......... 44% 204M 7s 118950K .......... .......... .......... .......... .......... 44% 190M 7s 119000K .......... .......... .......... .......... .......... 44% 208M 7s 119050K .......... .......... .......... .......... .......... 44% 215M 7s 119100K .......... .......... .......... .......... .......... 44% 6.59M 7s 119150K .......... .......... .......... .......... .......... 44% 26.0M 7s 119200K .......... .......... .......... .......... .......... 44% 68.2M 7s 119250K .......... .......... .......... .......... .......... 44% 2.82M 7s 119300K .......... .......... .......... .......... .......... 44% 3.12M 7s 119350K .......... .......... .......... .......... .......... 44% 99.9M 7s 119400K 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.......... .......... 45% 176M 7s 120750K .......... .......... .......... .......... .......... 45% 7.50M 7s 120800K .......... .......... .......... .......... .......... 45% 42.9M 7s 120850K .......... .......... .......... .......... .......... 45% 7.06M 7s 120900K .......... .......... .......... .......... .......... 45% 172M 7s 120950K .......... .......... .......... .......... .......... 45% 8.30M 7s 121000K .......... .......... .......... .......... .......... 45% 166M 7s 121050K .......... .......... .......... .......... .......... 45% 161M 7s 121100K .......... .......... .......... .......... .......... 45% 7.34M 7s 121150K .......... .......... .......... .......... .......... 45% 164M 7s 121200K .......... .......... .......... .......... .......... 45% 6.09M 7s 121250K .......... .......... .......... .......... .......... 45% 82.1M 7s 121300K .......... .......... .......... .......... .......... 45% 8.47M 7s 121350K .......... .......... .......... .......... .......... 45% 248M 7s 121400K .......... .......... .......... .......... .......... 45% 6.16M 7s 121450K .......... .......... .......... .......... .......... 45% 110M 7s 121500K .......... .......... .......... .......... .......... 45% 8.38M 7s 121550K .......... .......... .......... .......... .......... 45% 236M 7s 121600K .......... .......... .......... .......... .......... 45% 7.66M 7s 121650K .......... .......... .......... .......... .......... 45% 73.8M 7s 121700K .......... .......... .......... .......... .......... 45% 203M 7s 121750K .......... .......... .......... .......... .......... 45% 5.80M 7s 121800K .......... .......... .......... .......... .......... 45% 180M 7s 121850K .......... .......... .......... .......... .......... 45% 4.64M 7s 121900K .......... .......... .......... .......... .......... 45% 261M 7s 121950K .......... .......... .......... .......... .......... 45% 9.40M 7s 122000K .......... .......... .......... .......... .......... 45% 323M 7s 122050K .......... .......... .......... .......... .......... 45% 9.09M 7s 122100K .......... .......... .......... .......... .......... 45% 179M 7s 122150K .......... .......... .......... .......... .......... 45% 138M 7s 122200K .......... .......... .......... .......... .......... 46% 4.82M 7s 122250K .......... .......... .......... .......... .......... 46% 219M 7s 122300K .......... .......... .......... .......... .......... 46% 5.91M 7s 122350K .......... .......... .......... .......... .......... 46% 161M 7s 122400K .......... .......... .......... .......... .......... 46% 7.97M 7s 122450K .......... .......... .......... .......... .......... 46% 196M 7s 122500K .......... .......... .......... .......... .......... 46% 239M 7s 122550K .......... .......... .......... .......... .......... 46% 7.66M 7s 122600K .......... .......... .......... .......... .......... 46% 235M 7s 122650K .......... .......... .......... .......... .......... 46% 10.9M 7s 122700K .......... .......... .......... .......... .......... 46% 192M 7s 122750K .......... .......... .......... .......... .......... 46% 7.92M 7s 122800K .......... .......... .......... .......... .......... 46% 205M 7s 122850K .......... .......... .......... .......... .......... 46% 85.1M 7s 122900K .......... .......... .......... .......... .......... 46% 4.86M 7s 122950K .......... .......... .......... .......... .......... 46% 85.5M 7s 123000K .......... .......... .......... .......... .......... 46% 6.83M 7s 123050K .......... .......... .......... .......... .......... 46% 191M 7s 123100K .......... .......... .......... .......... .......... 46% 9.36M 7s 123150K .......... .......... .......... .......... .......... 46% 135M 7s 123200K .......... .......... .......... .......... .......... 46% 112M 7s 123250K .......... .......... .......... .......... .......... 46% 10.3M 7s 123300K .......... .......... .......... .......... .......... 46% 8.74M 7s 123350K .......... 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3.22M 7s 126000K .......... .......... .......... .......... .......... 47% 185M 7s 126050K .......... .......... .......... .......... .......... 47% 199M 7s 126100K .......... .......... .......... .......... .......... 47% 4.40M 7s 126150K .......... .......... .......... .......... .......... 47% 204M 7s 126200K .......... .......... .......... .......... .......... 47% 80.8M 7s 126250K .......... .......... .......... .......... .......... 47% 5.56M 7s 126300K .......... .......... .......... .......... .......... 47% 115M 7s 126350K .......... .......... .......... .......... .......... 47% 147M 7s 126400K .......... .......... .......... .......... .......... 47% 5.36M 7s 126450K .......... .......... .......... .......... .......... 47% 181M 7s 126500K .......... .......... .......... .......... .......... 47% 148M 7s 126550K .......... .......... .......... .......... .......... 47% 5.38M 7s 126600K .......... .......... .......... .......... .......... 47% 124M 7s 126650K 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164M 6s 138550K .......... .......... .......... .......... .......... 52% 279M 6s 138600K .......... .......... .......... .......... .......... 52% 4.16M 6s 138650K .......... .......... .......... .......... .......... 52% 129M 6s 138700K .......... .......... .......... .......... .......... 52% 113M 6s 138750K .......... .......... .......... .......... .......... 52% 174M 6s 138800K .......... .......... .......... .......... .......... 52% 4.08M 6s 138850K .......... .......... .......... .......... .......... 52% 122M 6s 138900K .......... .......... .......... .......... .......... 52% 161M 6s 138950K .......... .......... .......... .......... .......... 52% 15.3M 6s 139000K .......... .......... .......... .......... .......... 52% 3.94M 6s 139050K .......... .......... .......... .......... .......... 52% 31.6M 6s 139100K .......... .......... .......... .......... .......... 52% 118M 6s 139150K .......... .......... .......... .......... .......... 52% 163M 6s 139200K 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5s 181550K .......... .......... .......... .......... .......... 68% 2.58M 5s 181600K .......... .......... .......... .......... .......... 68% 141M 5s 181650K .......... .......... .......... .......... .......... 68% 123M 5s 181700K .......... .......... .......... .......... .......... 68% 144M 5s 181750K .......... .......... .......... .......... .......... 68% 128M 5s 181800K .......... .......... .......... .......... .......... 68% 241M 5s 181850K .......... .......... .......... .......... .......... 68% 282M 5s 181900K .......... .......... .......... .......... .......... 68% 2.65M 5s 181950K .......... .......... .......... .......... .......... 68% 183M 5s 182000K .......... .......... .......... .......... .......... 68% 273M 5s 182050K .......... .......... .......... .......... .......... 68% 222M 5s 182100K .......... .......... .......... .......... .......... 68% 151M 5s 182150K .......... .......... .......... .......... .......... 68% 337M 5s 182200K .......... 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.......... .......... .......... .......... .......... 73% 9.13M 4s 194800K .......... .......... .......... .......... .......... 73% 15.0M 4s 194850K .......... .......... .......... .......... .......... 73% 8.19M 4s 194900K .......... .......... .......... .......... .......... 73% 12.2M 4s 194950K .......... .......... .......... .......... .......... 73% 6.05M 4s 195000K .......... .......... .......... .......... .......... 73% 11.8M 4s 195050K .......... .......... .......... .......... .......... 73% 10.4M 4s 195100K .......... .......... .......... .......... .......... 73% 11.5M 4s 195150K .......... .......... .......... .......... .......... 73% 9.79M 4s 195200K .......... .......... .......... .......... .......... 73% 7.14M 4s 195250K .......... .......... .......... .......... .......... 73% 17.5M 4s 195300K .......... .......... .......... .......... .......... 73% 15.0M 4s 195350K .......... .......... .......... .......... .......... 73% 14.5M 4s 195400K .......... 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74% 17.5M 4s 198050K .......... .......... .......... .......... .......... 74% 15.6M 4s 198100K .......... .......... .......... .......... .......... 74% 8.45M 4s 198150K .......... .......... .......... .......... .......... 74% 14.8M 4s 198200K .......... .......... .......... .......... .......... 74% 17.2M 4s 198250K .......... .......... .......... .......... .......... 74% 16.0M 4s 198300K .......... .......... .......... .......... .......... 74% 16.7M 4s 198350K .......... .......... .......... .......... .......... 74% 13.9M 4s 198400K .......... .......... .......... .......... .......... 74% 11.4M 4s 198450K .......... .......... .......... .......... .......... 74% 5.61M 4s 198500K .......... .......... .......... .......... .......... 74% 220M 4s 198550K .......... .......... .......... .......... .......... 74% 12.2M 4s 198600K .......... .......... .......... .......... .......... 74% 18.0M 4s 198650K .......... .......... .......... .......... .......... 74% 12.8M 4s 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4.63M 3s 211200K .......... .......... .......... .......... .......... 79% 167M 3s 211250K .......... .......... .......... .......... .......... 79% 6.57M 3s 211300K .......... .......... .......... .......... .......... 79% 195M 3s 211350K .......... .......... .......... .......... .......... 79% 4.41M 3s 211400K .......... .......... .......... .......... .......... 79% 198M 3s 211450K .......... .......... .......... .......... .......... 79% 4.36M 3s 211500K .......... .......... .......... .......... .......... 79% 210M 3s 211550K .......... .......... .......... .......... .......... 79% 5.44M 3s 211600K .......... .......... .......... .......... .......... 79% 161M 3s 211650K .......... .......... .......... .......... .......... 79% 4.55M 3s 211700K .......... .......... .......... .......... .......... 79% 173M 3s 211750K .......... .......... .......... .......... .......... 79% 3.87M 3s 211800K .......... .......... .......... .......... .......... 79% 191M 3s 211850K 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3s 219100K .......... .......... .......... .......... .......... 82% 1.87M 3s 219150K .......... .......... .......... .......... .......... 82% 89.1M 3s 219200K .......... .......... .......... .......... .......... 82% 5.74M 3s 219250K .......... .......... .......... .......... .......... 82% 171M 3s 219300K .......... .......... .......... .......... .......... 82% 129M 3s 219350K .......... .......... .......... .......... .......... 82% 3.74M 3s 219400K .......... .......... .......... .......... .......... 82% 148M 3s 219450K .......... .......... .......... .......... .......... 82% 4.21M 3s 219500K .......... .......... .......... .......... .......... 82% 70.5M 3s 219550K .......... .......... .......... .......... .......... 82% 205M 3s 219600K .......... .......... .......... .......... .......... 82% 3.73M 3s 219650K .......... .......... .......... .......... .......... 82% 185M 3s 219700K .......... .......... .......... .......... .......... 82% 116M 3s 219750K 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.......... .......... 83% 62.3M 3s 221750K .......... .......... .......... .......... .......... 83% 7.71M 3s 221800K .......... .......... .......... .......... .......... 83% 187M 3s 221850K .......... .......... .......... .......... .......... 83% 174M 3s 221900K .......... .......... .......... .......... .......... 83% 4.77M 3s 221950K .......... .......... .......... .......... .......... 83% 173M 3s 222000K .......... .......... .......... .......... .......... 83% 216M 3s 222050K .......... .......... .......... .......... .......... 83% 1.70M 3s 222100K .......... .......... .......... .......... .......... 83% 42.1M 3s 222150K .......... .......... .......... .......... .......... 83% 212M 3s 222200K .......... .......... .......... .......... .......... 83% 3.64M 3s 222250K .......... .......... .......... .......... .......... 83% 214M 3s 222300K .......... .......... .......... .......... .......... 83% 174M 3s 222350K .......... .......... .......... .......... .......... 83% 4.21M 3s 222400K .......... .......... .......... .......... .......... 83% 210M 3s 222450K .......... .......... .......... .......... .......... 83% 174M 3s 222500K .......... .......... .......... .......... .......... 83% 3.54M 3s 222550K .......... .......... .......... .......... .......... 83% 164M 3s 222600K .......... .......... .......... .......... .......... 83% 157M 3s 222650K .......... .......... .......... .......... .......... 83% 207M 3s 222700K .......... .......... .......... .......... .......... 83% 3.30M 3s 222750K .......... .......... .......... .......... .......... 83% 228M 3s 222800K .......... .......... .......... .......... .......... 83% 141M 3s 222850K .......... .......... .......... .......... .......... 83% 3.42M 3s 222900K .......... .......... .......... .......... .......... 83% 203M 3s 222950K .......... .......... .......... .......... .......... 83% 77.6M 3s 223000K .......... .......... .......... .......... .......... 83% 3.93M 3s 223050K .......... .......... .......... .......... .......... 83% 143M 3s 223100K .......... .......... .......... .......... .......... 83% 133M 3s 223150K .......... .......... .......... .......... .......... 83% 3.71M 3s 223200K .......... .......... .......... .......... .......... 84% 105M 3s 223250K .......... .......... .......... .......... .......... 84% 14.9M 3s 223300K .......... .......... .......... .......... .......... 84% 212M 3s 223350K .......... .......... .......... .......... .......... 84% 7.46M 3s 223400K .......... .......... .......... .......... .......... 84% 244M 3s 223450K .......... .......... .......... .......... .......... 84% 88.3M 3s 223500K .......... .......... .......... .......... .......... 84% 8.12M 3s 223550K .......... .......... .......... .......... .......... 84% 212M 3s 223600K .......... .......... .......... .......... .......... 84% 142M 3s 223650K .......... .......... .......... .......... .......... 84% 3.04M 3s 223700K .......... .......... .......... .......... .......... 84% 88.1M 3s 223750K .......... .......... .......... .......... .......... 84% 97.7M 3s 223800K .......... .......... .......... .......... .......... 84% 196M 3s 223850K .......... .......... .......... .......... .......... 84% 3.81M 3s 223900K .......... .......... .......... .......... .......... 84% 189M 3s 223950K .......... .......... .......... .......... .......... 84% 63.2M 3s 224000K .......... .......... .......... .......... .......... 84% 4.11M 3s 224050K .......... .......... .......... .......... .......... 84% 182M 3s 224100K .......... .......... .......... .......... .......... 84% 113M 3s 224150K .......... .......... .......... .......... .......... 84% 5.15M 3s 224200K .......... .......... .......... .......... .......... 84% 137M 3s 224250K .......... .......... .......... .......... .......... 84% 119M 3s 224300K .......... .......... .......... .......... .......... 84% 189M 3s 224350K .......... .......... .......... .......... .......... 84% 2.97M 3s 224400K .......... .......... .......... .......... .......... 84% 163M 3s 224450K .......... .......... .......... .......... .......... 84% 125M 3s 224500K .......... .......... .......... .......... .......... 84% 3.91M 3s 224550K .......... .......... .......... .......... .......... 84% 162M 3s 224600K .......... .......... .......... .......... .......... 84% 121M 3s 224650K .......... .......... .......... .......... .......... 84% 2.68M 3s 224700K .......... .......... .......... .......... .......... 84% 126M 3s 224750K .......... .......... .......... .......... .......... 84% 187M 3s 224800K .......... .......... .......... .......... .......... 84% 203M 2s 224850K .......... .......... .......... .......... .......... 84% 3.53M 2s 224900K .......... .......... .......... .......... .......... 84% 130M 2s 224950K .......... .......... .......... .......... .......... 84% 100M 2s 225000K .......... .......... .......... .......... .......... 84% 2.98M 2s 225050K .......... .......... .......... .......... .......... 84% 241M 2s 225100K .......... .......... .......... .......... .......... 84% 94.8M 2s 225150K .......... .......... .......... .......... .......... 84% 100M 2s 225200K .......... .......... .......... .......... .......... 84% 3.53M 2s 225250K .......... .......... .......... .......... .......... 84% 3.18M 2s 225300K .......... .......... .......... .......... .......... 84% 133M 2s 225350K .......... .......... .......... .......... .......... 84% 5.15M 2s 225400K .......... .......... .......... .......... .......... 84% 81.5M 2s 225450K .......... .......... .......... .......... .......... 84% 131M 2s 225500K .......... .......... .......... .......... .......... 84% 205M 2s 225550K .......... .......... .......... .......... .......... 84% 3.92M 2s 225600K .......... .......... .......... .......... .......... 84% 103M 2s 225650K .......... .......... .......... .......... .......... 84% 138M 2s 225700K .......... .......... .......... .......... .......... 84% 4.27M 2s 225750K .......... .......... .......... .......... .......... 84% 116M 2s 225800K .......... .......... .......... .......... .......... 84% 131M 2s 225850K .......... .......... .......... .......... .......... 85% 7.36M 2s 225900K .......... .......... .......... .......... .......... 85% 108M 2s 225950K .......... .......... .......... .......... .......... 85% 148M 2s 226000K .......... .......... .......... .......... .......... 85% 77.6M 2s 226050K .......... .......... .......... .......... .......... 85% 5.22M 2s 226100K .......... .......... .......... .......... .......... 85% 83.8M 2s 226150K .......... .......... .......... .......... .......... 85% 227M 2s 226200K .......... .......... .......... .......... .......... 85% 3.90M 2s 226250K .......... .......... .......... .......... .......... 85% 148M 2s 226300K .......... .......... .......... .......... .......... 85% 90.3M 2s 226350K .......... .......... .......... .......... .......... 85% 9.49M 2s 226400K .......... .......... .......... .......... .......... 85% 3.21M 2s 226450K .......... .......... .......... .......... .......... 85% 182M 2s 226500K .......... .......... .......... .......... .......... 85% 189M 2s 226550K .......... .......... .......... .......... .......... 85% 250M 2s 226600K .......... .......... .......... .......... .......... 85% 3.79M 2s 226650K .......... .......... .......... .......... .......... 85% 168M 2s 226700K .......... .......... .......... .......... .......... 85% 102M 2s 226750K .......... .......... .......... .......... .......... 85% 3.73M 2s 226800K .......... .......... .......... .......... .......... 85% 223M 2s 226850K .......... .......... .......... .......... .......... 85% 113M 2s 226900K .......... .......... .......... .......... .......... 85% 128M 2s 226950K .......... .......... .......... .......... .......... 85% 3.67M 2s 227000K .......... .......... .......... .......... .......... 85% 229M 2s 227050K .......... .......... .......... .......... .......... 85% 243M 2s 227100K .......... .......... .......... .......... .......... 85% 3.72M 2s 227150K .......... .......... .......... .......... .......... 85% 208M 2s 227200K .......... .......... .......... .......... .......... 85% 60.7M 2s 227250K .......... .......... .......... .......... .......... 85% 201M 2s 227300K .......... .......... .......... .......... .......... 85% 2.82M 2s 227350K .......... .......... .......... .......... .......... 85% 158M 2s 227400K .......... .......... .......... .......... .......... 85% 153M 2s 227450K .......... .......... .......... .......... .......... 85% 3.82M 2s 227500K .......... .......... .......... .......... .......... 85% 6.88M 2s 227550K .......... .......... .......... .......... .......... 85% 17.7M 2s 227600K .......... .......... .......... .......... .......... 85% 15.2M 2s 227650K .......... .......... .......... .......... .......... 85% 5.28M 2s 227700K .......... .......... .......... .......... .......... 85% 59.7M 2s 227750K .......... .......... .......... .......... .......... 85% 11.5M 2s 227800K .......... .......... .......... .......... .......... 85% 26.7M 2s 227850K .......... .......... .......... .......... .......... 85% 3.45M 2s 227900K .......... .......... .......... .......... .......... 85% 120M 2s 227950K .......... .......... .......... .......... .......... 85% 34.8M 2s 228000K .......... .......... .......... .......... .......... 85% 19.8M 2s 228050K .......... .......... .......... .......... .......... 85% 2.60M 2s 228100K .......... .......... .......... .......... .......... 85% 96.1M 2s 228150K .......... .......... .......... .......... .......... 85% 169M 2s 228200K .......... .......... .......... .......... .......... 85% 3.15M 2s 228250K .......... .......... .......... .......... .......... 85% 119M 2s 228300K .......... .......... 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21.8M 2s 230300K .......... .......... .......... .......... .......... 86% 159M 2s 230350K .......... .......... .......... .......... .......... 86% 4.23M 2s 230400K .......... .......... .......... .......... .......... 86% 33.1M 2s 230450K .......... .......... .......... .......... .......... 86% 151M 2s 230500K .......... .......... .......... .......... .......... 86% 3.46M 2s 230550K .......... .......... .......... .......... .......... 86% 118M 2s 230600K .......... .......... .......... .......... .......... 86% 110M 2s 230650K .......... .......... .......... .......... .......... 86% 3.34M 2s 230700K .......... .......... .......... .......... .......... 86% 146M 2s 230750K .......... .......... .......... .......... .......... 86% 156M 2s 230800K .......... .......... .......... .......... .......... 86% 3.10M 2s 230850K .......... .......... .......... .......... .......... 86% 141M 2s 230900K .......... .......... .......... .......... .......... 86% 3.18M 2s 230950K 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.......... .......... 87% 37.4M 2s 232950K .......... .......... .......... .......... .......... 87% 2.36M 2s 233000K .......... .......... .......... .......... .......... 87% 191M 2s 233050K .......... .......... .......... .......... .......... 87% 8.31M 2s 233100K .......... .......... .......... .......... .......... 87% 4.28M 2s 233150K .......... .......... .......... .......... .......... 87% 174M 2s 233200K .......... .......... .......... .......... .......... 87% 105M 2s 233250K .......... .......... .......... .......... .......... 87% 2.62M 2s 233300K .......... .......... .......... .......... .......... 87% 160M 2s 233350K .......... .......... .......... .......... .......... 87% 194M 2s 233400K .......... .......... .......... .......... .......... 87% 2.58M 2s 233450K .......... .......... .......... .......... .......... 87% 109M 2s 233500K .......... .......... .......... .......... .......... 87% 249M 2s 233550K .......... .......... .......... .......... 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6.69M 2s 234250K .......... .......... .......... .......... .......... 88% 133M 2s 234300K .......... .......... .......... .......... .......... 88% 212M 2s 234350K .......... .......... .......... .......... .......... 88% 7.56M 2s 234400K .......... .......... .......... .......... .......... 88% 35.0M 2s 234450K .......... .......... .......... .......... .......... 88% 19.4M 2s 234500K .......... .......... .......... .......... .......... 88% 3.41M 2s 234550K .......... .......... .......... .......... .......... 88% 231M 2s 234600K .......... .......... .......... .......... .......... 88% 148M 2s 234650K .......... .......... .......... .......... .......... 88% 2.32M 2s 234700K .......... .......... .......... .......... .......... 88% 182M 2s 234750K .......... .......... .......... .......... .......... 88% 294M 2s 234800K .......... .......... .......... .......... .......... 88% 287M 2s 234850K .......... .......... .......... .......... .......... 88% 3.70M 2s 234900K 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.......... .......... .......... 88% 7.03M 2s 236250K .......... .......... .......... .......... .......... 88% 149M 2s 236300K .......... .......... .......... .......... .......... 88% 146M 2s 236350K .......... .......... .......... .......... .......... 88% 5.35M 2s 236400K .......... .......... .......... .......... .......... 88% 164M 2s 236450K .......... .......... .......... .......... .......... 88% 6.45M 2s 236500K .......... .......... .......... .......... .......... 89% 95.9M 2s 236550K .......... .......... .......... .......... .......... 89% 132M 2s 236600K .......... .......... .......... .......... .......... 89% 3.56M 2s 236650K .......... .......... .......... .......... .......... 89% 220M 2s 236700K .......... .......... .......... .......... .......... 89% 228M 2s 236750K .......... .......... .......... .......... .......... 89% 5.57M 2s 236800K .......... .......... .......... .......... .......... 89% 178M 2s 236850K .......... .......... .......... 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.......... 89% 233M 2s 237550K .......... .......... .......... .......... .......... 89% 1.62M 2s 237600K .......... .......... .......... .......... .......... 89% 5.80M 2s 237650K .......... .......... .......... .......... .......... 89% 271M 2s 237700K .......... .......... .......... .......... .......... 89% 2.85M 2s 237750K .......... .......... .......... .......... .......... 89% 165M 2s 237800K .......... .......... .......... .......... .......... 89% 200M 2s 237850K .......... .......... .......... .......... .......... 89% 4.23M 2s 237900K .......... .......... .......... .......... .......... 89% 203M 2s 237950K .......... .......... .......... .......... .......... 89% 3.51M 2s 238000K .......... .......... .......... .......... .......... 89% 289M 2s 238050K .......... .......... .......... .......... .......... 89% 257M 2s 238100K .......... .......... .......... .......... .......... 89% 3.09M 2s 238150K .......... .......... .......... .......... .......... 89% 230M 2s 238200K .......... .......... .......... .......... .......... 89% 4.64M 2s 238250K .......... .......... .......... .......... .......... 89% 210M 2s 238300K .......... .......... .......... .......... .......... 89% 159M 2s 238350K .......... .......... .......... .......... .......... 89% 3.55M 2s 238400K .......... .......... .......... .......... .......... 89% 108M 2s 238450K .......... .......... .......... .......... .......... 89% 4.60M 2s 238500K .......... .......... .......... .......... .......... 89% 228M 2s 238550K .......... .......... .......... .......... .......... 89% 169M 2s 238600K .......... .......... .......... .......... .......... 89% 9.14M 2s 238650K .......... .......... .......... .......... .......... 89% 100M 2s 238700K .......... .......... .......... .......... .......... 89% 203M 2s 238750K .......... .......... .......... .......... .......... 89% 9.44M 2s 238800K .......... .......... .......... .......... .......... 89% 204M 2s 238850K .......... .......... .......... .......... .......... 89% 3.76M 2s 238900K .......... .......... .......... .......... .......... 89% 197M 2s 238950K .......... .......... .......... .......... .......... 89% 193M 2s 239000K .......... .......... .......... .......... .......... 89% 3.29M 2s 239050K .......... .......... .......... .......... .......... 89% 222M 2s 239100K .......... .......... .......... .......... .......... 89% 2.35M 2s 239150K .......... .......... .......... .......... .......... 90% 203M 2s 239200K .......... .......... .......... .......... .......... 90% 189M 2s 239250K .......... .......... .......... .......... .......... 90% 3.72M 2s 239300K .......... .......... .......... .......... .......... 90% 183M 2s 239350K .......... .......... .......... .......... .......... 90% 182M 2s 239400K .......... .......... .......... .......... .......... 90% 4.02M 2s 239450K .......... .......... .......... .......... .......... 90% 183M 2s 239500K .......... 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2s 242150K .......... .......... .......... .......... .......... 91% 209M 2s 242200K .......... .......... .......... .......... .......... 91% 125M 2s 242250K .......... .......... .......... .......... .......... 91% 2.67M 2s 242300K .......... .......... .......... .......... .......... 91% 163M 2s 242350K .......... .......... .......... .......... .......... 91% 169M 2s 242400K .......... .......... .......... .......... .......... 91% 3.00M 1s 242450K .......... .......... .......... .......... .......... 91% 178M 1s 242500K .......... .......... .......... .......... .......... 91% 97.5M 1s 242550K .......... .......... .......... .......... .......... 91% 2.50M 1s 242600K .......... .......... .......... .......... .......... 91% 135M 1s 242650K .......... .......... .......... .......... .......... 91% 696K 1s 242700K .......... .......... .......... .......... .......... 91% 4.84M 1s 242750K .......... .......... .......... .......... .......... 91% 99.2M 1s 242800K 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1s 246100K .......... .......... .......... .......... .......... 92% 190M 1s 246150K .......... .......... .......... .......... .......... 92% 180M 1s 246200K .......... .......... .......... .......... .......... 92% 3.34M 1s 246250K .......... .......... .......... .......... .......... 92% 11.0M 1s 246300K .......... .......... .......... .......... .......... 92% 192M 1s 246350K .......... .......... .......... .......... .......... 92% 3.00M 1s 246400K .......... .......... .......... .......... .......... 92% 97.5M 1s 246450K .......... .......... .......... .......... .......... 92% 146M 1s 246500K .......... .......... .......... .......... .......... 92% 190M 1s 246550K .......... .......... .......... .......... .......... 92% 3.20M 1s 246600K .......... .......... .......... .......... .......... 92% 110M 1s 246650K .......... .......... .......... .......... .......... 92% 210M 1s 246700K .......... .......... .......... .......... .......... 92% 3.12M 1s 246750K 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/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/config/ + ./makeEnv ESP runtime AutoConfigurator CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 with contents: bin include lib share Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python found! Info: Python header /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11/Python.h found! Info: Python library /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin/libpython3.11.dylib found! ESP_ARCH = DARWIN64 ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad EFCOMP = gfortran CARCH = DARWIN64 CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 CASARCH = . CASREV = 7.7 PYTHONINC= /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 PYTHONLIB= -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 + source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESPenv.sh ++ export ESP_ARCH=DARWIN64 ++ ESP_ARCH=DARWIN64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 ++ export CASARCH=. ++ CASARCH=. ++ export CASREV=7.7 ++ CASREV=7.7 ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/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:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONINC=/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 ++ PYTHONINC=/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 ++ export 'PYTHONLIB=-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11' ++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11' ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ export AFLR_ARCH=MacOSX-x86-64 ++ AFLR_ARCH=MacOSX-x86-64 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ export CAPS_GLYPH= ++ CAPS_GLYPH= ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/SLUGS/Slugs.html' ++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/SLUGS/Slugs.html' ++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESP/ESP.html' ++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESP/ESP.html' ++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/wvClient/wv.html' ++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/wvClient/wv.html' + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src + make (cd EGADS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64 rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64 cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64 touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/always_inline.h clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsGeom.cpp -o ./egadsGeom.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsHLevel.cpp -o ./egadsHLevel.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsTopo.cpp -o ./egadsTopo.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsCopy.cpp -o ./egadsCopy.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsSpline.cpp -o ./egadsSpline.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsIO.cpp -o ./egadsIO.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsSplineFit.cpp -o ./egadsSplineFit.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsSkinning.cpp -o ./egadsSkinning.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \ -I. egadsTessSens.cpp -o ./egadsTessSens.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsBase.c -o ./egadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o ./egadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsTess.c -o ./egadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsTris.c -o ./egadsTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o ./egadsQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsFit.c -o ./egadsFit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o ./egadsRobust.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o ./egadsSBO.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap prmCfit.c -o ./prmCfit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap prmGrid.c -o ./prmGrid.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap prmUV.c -o ./prmUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsExport.c -o ./egadsExport.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o ./egadsEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o ./egadsSolids.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include ../util/emp.c \ -o ./emp.o clang++ -g -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 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \ ../util/evaluate.c -o ./evaluate.o clang++ -g -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 -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \ ../util/rational.c -o ./rational.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../util \ ../util/regQuads.c -o ./regQuads.o clang++ -g -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp ./SurrealD1 SurrealD1_test_suite Complete! clang++ -g -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp ./SurrealD4 SurrealD4_test_suite Complete! clang++ -g -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp ./SurrealS1 SurrealS1_test_suite Complete! clang++ -g -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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 uvmap/main/uvmap.c -Iuvmap \ -o ./uvmap.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_add.c -o ./uvmap_add.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_message.c -o ./uvmap_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_read.c -o ./uvmap_read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_test.c -o ./uvmap_test.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_version.c -o ./uvmap_version.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_write.c -o ./uvmap_write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 egadsUVmap.c -Iuvmap \ -o ./egadsUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a clang -g -o ./uvmap.exe ./uvmap.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib (cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \ egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.7 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a (cd .; \ ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsBase.c -o ./fgadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsMemory.c -o ./fgadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsAttrs.c -o ./fgadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTess.c -o ./fgadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsHLevel.c -o ./fgadsHLevel.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsGeom.c -o ./fgadsGeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTopo.c -o ./fgadsTopo.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a *** EGADS Build Complete! *** (cd EGADS/lite; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteBase.c -o ./liteBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteMemory.c -o ./liteMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteGeom.c -o ./liteGeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteTopo.c -o ./liteTopo.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteAttrs.c -o ./liteAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteImport.c -o ./liteImport.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \ liteString.c -o ./liteString.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o ./liteTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o ./liteTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src \ ../src/egadsQuads.c -o ./liteQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o ./liteTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 ../src/egadsRobust.c \ -o ./egadsRobust.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DDARWIN64 -I../include ../util/emp.c \ -o ./emp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o ./evaLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE ../util/rational.c \ -o ./ratLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I../util \ ../util/regQuads.c -o ./liteRegQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o ./liteEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o ./liteUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib (cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib \ liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \ egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \ liteEffect.o liteUVmap.o \ -install_name '@rpath/libegadslite.dylib' \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \ liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \ emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \ liteUVmap.o ; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a (cd wvServer; make) clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 map.cpp -o ./map.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include base64-decode.c -o ./base64-decode.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include handshake.c -o ./handshake.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include client-handshake.c -o ./client-handshake.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include md5.c -o ./md5.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include parsers.c -o ./parsers.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension.c -o ./extension.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include sha-1.c -o ./sha-1.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include server.c -o ./server.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include wv.c -o ./wv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include browserMessage.c -o ./browserMessage.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fwv.c -o ./fwv.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \ ./fwv.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \ -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -o ./servertest.o clang++ -g -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib (cd .; clang++ -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib \ base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \ -install_name '@rpath/libwsserver.dylib' \ -compatibility_version 7.7 \ -current_version 1.0.25 ) (cd EGADS/examples; make -f egads2cart.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include egads2cart.c \ -o ./egads2cart.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm (cd EGADS/examples; make -f vCurvature.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vCurvature.c -o ./vCurvature.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vCurvature ./vCurvature.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib (cd EGADS/examples; make -f vGeom.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vGeom.c -o ./vGeom.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib (cd EGADS/examples; make -f vTess.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vTess.c -o ./vTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include ../util/retessFaces.c \ -o ./retessFaces.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib (cd OpenCSM; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udp.c -o ./udp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. tim.c -o ./tim.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25 clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so ./udpWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J . touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm -Wl,-w clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c (cd Slugs; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Fitter.c \ -o ./Fitter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. RedBlackTree.c \ -o ./RedBlackTree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Tessellate.c \ -o ./Tessellate.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \ ./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads \ -lpthread -lz -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads \ -lpthread -lz -lm (cd CAPS; make) /bin/cp Cart3D/OSX64_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libc3dio.a /bin/cp Cart3D/OSX64_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libCart3D.a /bin/cp Executables/DARWIN64/avl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/avl /bin/cp Executables/DARWIN64/pplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/pplot /bin/cp Executables/DARWIN64/pxplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/pxplot /bin/cp Executables/DARWIN64/xfoil /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/xfoil /bin/cp Executables/DARWIN64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mastros.exe /bin/cp Executables/DARWIN64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ASTRO.D01 /bin/cp Executables/DARWIN64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ASTRO.IDX /bin/cp Executables/DARWIN64/mses /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mses /bin/cp Executables/DARWIN64/mset /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mset /bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include /bin/cp udunits/DARWIN64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib /bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libudunits2.dylib /bin/cp Libraries/DARWIN64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr2AIM.so /bin/cp Libraries/DARWIN64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr3AIM.so /bin/cp Libraries/DARWIN64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr4AIM.so (cd CAPS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../include \ -I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o ./aimTransferUtil.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../include \ aimMesh.c -o ./aimMesh.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \ ./aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsBase.c -o ./capsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsBound.c -o ./capsBound.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsValue.c -o ./capsValue.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 printObject.c -o ./printObject.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib (cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \ -install_name '@rpath/libcaps.dylib' \ -compatibility_version 1.0.25 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include testingAIM.c \ -o ./testingAIM.o rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include testingWriter.c \ -o ./testingWriter.o rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include phaseUtil.c \ -o ./phaseUtil.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm (cd ../CAPSexamples; make) (make -C cCAPS -f aeroelastic_SU2.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o clang -g -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include avlTest.c -o ./avlTest.o clang -g -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include awaveTest.c -o ./awaveTest.o clang -g -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include frictionTest.c -o ./frictionTest.o clang -g -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o clang -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o clang -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o clang -g -o ./aeroelasticTest ./aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmTest.c -o ./hsmTest.o clang -g -o ./hsmTest ./hsmTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o clang -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o clang -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o clang -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include interferenceTest.c \ -o ./interferenceTest.o clang -g -o ./interferenceTest ./interferenceTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include msesTest.c -o ./msesTest.o clang -g -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include mystranTest.c -o ./mystranTest.o clang -g -o ./mystranTest ./mystranTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o clang -g -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl (cd CAPS/aim; make) /Library/Developer/CommandLineTools/usr/bin/make -C utils clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a /Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a(attrUtils.o) has no symbols mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmUtils.h /Library/Developer/CommandLineTools/usr/bin/make -C abaqus clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \ abaqusAIM.c -o ./abaqusAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \ abaqusUtils.c -o ./abaqusUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \ -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o echo "Building Abaqus with Python" Building Abaqus with Python clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -lm -ldl -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin /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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosAIM.c \ -o ./astrosAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosUtils.c \ -o ./astrosUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosCards.c \ -o ./astrosCards.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C avl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C awave clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils awaveAIM.c \ -o ./awaveAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C cart3d clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \ cart3dAIM.c -o ./cart3dAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \ writeTrix.c -o ./writeTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D \ surfTrix.c -o ./surfTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -pedantic -I./xddm -I. \ `xml2-config --cflags` ./xddm/xddm.c \ -o ./xddm.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bodyTess.c -o ./bodyTess.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \ ./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/ \ -lc3dio -lCart3D -ldl -lxml2 -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include cart3dTest.c \ -o ./cart3dTest.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I./xddm \ -I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \ ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lxml2 -lm /Library/Developer/CommandLineTools/usr/bin/make -C cbaero clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o clang -g -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C cgt clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include egads2cgt.c \ -o ./egads2cgt.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aflr4egads.c \ -o ./aflr4egads.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C custom make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C delaundo clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils delaundoAIM.c \ -o ./delaundoAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C egadsTess clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils egadsTessAIM.c \ -o ./egadsTessAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C friction clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils frictionAIM.c \ -o ./frictionAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o gfortran -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/friction ./friction.o -Wl,-w -static-libgfortran -static-libgcc /Library/Developer/CommandLineTools/usr/bin/make -C fun3d clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \ -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \ fun3dUtils.c -o ./fun3dUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \ -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o Building FUN3D with Python clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \ ./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -lm -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin /Library/Developer/CommandLineTools/usr/bin/make -C hsm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmAIM.c \ -o src/hsmAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmUtils.c \ -o src/hsmUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmAdj.c \ -o src/hsmAdj.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.7 \ -o src/rcm.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 rcm/genrcmi.cpp -DREVISION=7.7 \ -o src/genrcmi.o /Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o /Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o /Library/Developer/CommandLineTools/usr/bin/make -C src cross.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o /Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o /Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o /Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so \ src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \ src/rcm.o src/genrcmi.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C interference clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include interferenceAIM.c \ -o ./interferenceAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. cloudFns.c \ -o ./cloudFns.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so \ ./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C masstran clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils masstranAIM.cpp \ -o ./masstranAIM.o clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bstlWriter.c \ -o ./bstlWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bvtkWriter.c \ -o ./bvtkWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C fastWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fastWriter.c \ -o ./fastWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libmeshbWriter.c \ -o ./libmeshbWriter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C stlWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include stlWriter.c \ -o ./stlWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include su2Writer.c \ -o ./su2Writer.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include tecplotWriter.c \ -o ./tecplotWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include ugridWriter.c \ -o ./ugridWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vtkWriter.c \ -o ./vtkWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C mses clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C mystran clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils mystranAIM.c \ -o ./mystranAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils mystranUtils.c \ -o ./mystranUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C nastran clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils nastranAIM.c \ -o ./nastranAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C plato Not compiling platoAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C pointwise clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils pointwiseAIM.c \ -o ./pointwiseAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hashElement.c \ -o ./hashElement.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -lpthread /Library/Developer/CommandLineTools/usr/bin/make -C refine clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \ -o ./refineAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 \ -I../meshWriter/libmeshbWriter/libMeshb/sources \ ../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C sierraSD Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C sierraSM Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C skeleton clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils skeletonAIM.c \ -o ./skeletonAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C spinnaker make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C su2 clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \ -o ./su2AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2Utils.c \ -o ./su2Utils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_4_Cardinal.c \ -o ./su2_4_Cardinal.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_5_Raven.c \ -o ./su2_5_Raven.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_6_Falcon.c \ -o ./su2_6_Falcon.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_7_Blackbird.c \ -o ./su2_7_Blackbird.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_801_Harrier.c \ -o ./su2_801_Harrier.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C tacs clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils tacsAIM.c \ -o ./tacsAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 /Library/Developer/CommandLineTools/usr/bin/make -C tetgen clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils tetgenAIM.cpp \ -o ./tetgenAIM.o clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \ -DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o clang++ -g -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 -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 -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \ ./tetgen_Interface.o ./tetgen.o \ ./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tsfoil clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \ tsfoilAIM.c -o ./tsfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \ xfoilAIM.c -o ./xfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C zaero clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl (cd OpenCSM; make -f serveESP.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 timPyscript.c -o ./timPyscript.o touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pyscript.so rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pyscript.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin *** Build Completed! *** + export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data + CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin ++ uname -a + [[ Darwin macys-VM 20.6.0 Darwin Kernel Version 20.6.0: Thu Sep 29 20:15:11 PDT 2022; root:xnu-7195.141.42~1/RELEASE_X86_64 x86_64 == *\D\a\r\w\i\n* ]] + sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/Verification.sh + bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/Verification.sh + expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/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 0m0.362s user 0m0.023s sys 0m0.011s + set +x ============================================= ESP verification case 01 passed (as expected) ============================================= + expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/demo2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/demo2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.227s user 0m0.273s sys 0m0.029s + set +x ============================================= ESP verification case 02 passed (as expected) ============================================= + expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m2.358s user 0m3.409s sys 0m0.638s + set +x ============================================= ESP verification case 03 passed (as expected) ============================================= + expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.599s user 0m0.678s sys 0m0.050s + set +x ============================================= ESP verification case 04 passed (as expected) ============================================= + expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.419s user 0m0.641s sys 0m0.031s + set +x ============================================= ESP verification case 05 passed (as expected) ============================================= + expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.482s user 0m0.707s sys 0m0.030s + set +x ============================================= ESP verification case 06 passed (as expected) ============================================= + expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m2.917s user 0m4.647s sys 0m0.529s + set +x ============================================= ESP verification case 07 passed (as expected) ============================================= + expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/myPlane + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/myPlane WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/verify_7.7.0/myPlane.vfy", so verification is being skipped ==> serveESP completed successfully with 12 warnings and no verification data real 0m26.805s user 0m40.826s sys 0m1.559s + set +x ============================================= ESP verification case 08 passed (as expected) ============================================= + expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/bottle + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/bottle WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.467s user 0m0.604s sys 0m0.029s + set +x ============================================= ESP verification case 09 passed (as expected) ============================================= + expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/wingMultiModel + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/wingMultiModel WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/wingMultiModel.vfy", so verification is being skipped ==> serveESP completed successfully with 4 warnings and no verification data real 0m36.578s user 1m5.510s sys 0m7.164s + set +x ============================================= ESP verification case 10 passed (as expected) ============================================= + expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/bullet + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/bullet WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/bullet.vfy", so verification is being skipped WARNING:: 8 _hist and/or __trace__ attributes removed WARNING:: 8 _hist and/or __trace__ attributes removed ==> serveESP completed successfully with 1 warnings and no verification data real 0m0.403s user 0m0.241s sys 0m0.024s + set +x ============================================= ESP verification case 11 passed (as expected) ============================================= + expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/connect5 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/connect5 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.482s user 0m0.712s sys 0m0.015s + set +x ============================================= ESP verification case 12 passed (as expected) ============================================= + expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/group2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/group2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.145s user 0m0.196s sys 0m0.013s + set +x ============================================= ESP verification case 13 passed (as expected) ============================================= + expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/csm3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/csm3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/csm3.vfy", so verification is being skipped nnode=8 nedge=12 nface=6 nnode=8 nedge=12 nface=6 nnode=16 nedge=24 nface=10 nnode=8 nedge=12 nface=6 ==> serveESP completed successfully with no verification data real 0m0.473s user 0m0.463s sys 0m0.017s + set +x ============================================= ESP verification case 14 passed (as expected) ============================================= + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP/testEGADS + make test python --version Python 3.11.5 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 2.865s OK + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP/testOCSM + source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/test_pyOCSM.sh ++ set -x ++ python -u test_pyOCSM.py -skipHelp real 0m5.704s user 0m8.825s sys 0m0.208s ++ set +x ================================================= test_pyOCSM.py passed (as expected) ================================================= + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP/testCAPS + make test python --version Python 3.11.5 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 21.135s OK WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/ + make test python --version Python 3.11.5 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.064 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.007 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 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 = 0.024 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4122 6020 AFLR2 GG : Nodes, Faces = 5812 9400 AFLR2 GG : Nodes, Faces = 7299 12374 AFLR2 GG : Nodes, Faces = 8574 14924 AFLR2 GG : Nodes, Faces = 9729 17234 AFLR2 GG : Nodes, Faces = 10787 19350 AFLR2 GG : Nodes, Faces = 11767 21310 AFLR2 GG : Nodes, Faces = 12683 23142 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 14278 26332 AFLR2 GG : Nodes, Faces = 14999 27774 AFLR2 GG : Nodes, Faces = 15682 29140 AFLR2 GG : Nodes, Faces = 16312 30400 AFLR2 GG : Nodes, Faces = 16899 31574 AFLR2 GG : Nodes, Faces = 17451 32678 AFLR2 GG : Nodes, Faces = 17959 33694 AFLR2 GG : Nodes, Faces = 18443 34662 AFLR2 GG : Nodes, Faces = 18877 35530 AFLR2 GG : Nodes, Faces = 19283 36342 AFLR2 GG : Nodes, Faces = 19650 37076 AFLR2 GG : Nodes, Faces = 19994 37764 AFLR2 GG : Nodes, Faces = 20325 38426 AFLR2 GG : Nodes, Faces = 20638 39052 AFLR2 GG : Nodes, Faces = 20940 39656 AFLR2 GG : Nodes, Faces = 21240 40256 AFLR2 GG : Nodes, Faces = 21523 40822 AFLR2 GG : Nodes, Faces = 21792 41360 AFLR2 GG : Nodes, Faces = 22053 41882 AFLR2 GG : Nodes, Faces = 22305 42386 AFLR2 GG : Nodes, Faces = 22521 42818 AFLR2 GG : Nodes, Faces = 22696 43168 AFLR2 GG : Nodes, Faces = 22829 43434 AFLR2 GG : Nodes, Faces = 22953 43682 AFLR2 GG : Nodes, Faces = 23050 43876 AFLR2 GG : Nodes, Faces = 23110 43996 AFLR2 GG : Nodes, Faces = 23139 44054 AFLR2 GG : Nodes, Faces = 23157 44090 AFLR2 GG : Nodes, Faces = 23175 44126 AFLR2 GG : Nodes, Faces = 23183 44142 AFLR2 GG : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.056 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.005 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23187 Number of elements = 46374 Number of tris = 44150 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.061 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 0.025 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4122 6020 AFLR2 GG : Nodes, Faces = 5812 9400 AFLR2 GG : Nodes, Faces = 7299 12374 AFLR2 GG : Nodes, Faces = 8574 14924 AFLR2 GG : Nodes, Faces = 9729 17234 AFLR2 GG : Nodes, Faces = 10787 19350 AFLR2 GG : Nodes, Faces = 11767 21310 AFLR2 GG : Nodes, Faces = 12683 23142 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 14278 26332 AFLR2 GG : Nodes, Faces = 14999 27774 AFLR2 GG : Nodes, Faces = 15682 29140 AFLR2 GG : Nodes, Faces = 16312 30400 AFLR2 GG : Nodes, Faces = 16899 31574 AFLR2 GG : Nodes, Faces = 17451 32678 AFLR2 GG : Nodes, Faces = 17959 33694 AFLR2 GG : Nodes, Faces = 18443 34662 AFLR2 GG : Nodes, Faces = 18877 35530 AFLR2 GG : Nodes, Faces = 19283 36342 AFLR2 GG : Nodes, Faces = 19650 37076 AFLR2 GG : Nodes, Faces = 19994 37764 AFLR2 GG : Nodes, Faces = 20325 38426 AFLR2 GG : Nodes, Faces = 20638 39052 AFLR2 GG : Nodes, Faces = 20940 39656 AFLR2 GG : Nodes, Faces = 21240 40256 AFLR2 GG : Nodes, Faces = 21523 40822 AFLR2 GG : Nodes, Faces = 21792 41360 AFLR2 GG : Nodes, Faces = 22053 41882 AFLR2 GG : Nodes, Faces = 22305 42386 AFLR2 GG : Nodes, Faces = 22521 42818 AFLR2 GG : Nodes, Faces = 22696 43168 AFLR2 GG : Nodes, Faces = 22829 43434 AFLR2 GG : Nodes, Faces = 22953 43682 AFLR2 GG : Nodes, Faces = 23050 43876 AFLR2 GG : Nodes, Faces = 23110 43996 AFLR2 GG : Nodes, Faces = 23139 44054 AFLR2 GG : Nodes, Faces = 23157 44090 AFLR2 GG : Nodes, Faces = 23175 44126 AFLR2 GG : Nodes, Faces = 23183 44142 AFLR2 GG : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.056 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.005 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23187 Number of elements = 46374 Number of tris = 44150 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 0.023 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.060 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 161 274 AFLR2 GG : Nodes, Faces = 171 294 AFLR2 GG : Nodes, Faces = 181 314 AFLR2 GG : Nodes, Faces = 187 326 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 0.001 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 = 0.010 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.002 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4705 Number of elements = 9410 Number of tris = 9066 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing FAST file .... Finished writing FAST file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.011 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 = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 0.001 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 = 0.011 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 = 0.005 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:62031) 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1189 Number of elements = 6249 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4917 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 6237 Number of elements = 34620 Number of triangles = 4438 Number of quadrilatarals = 0 Number of tetrahedrals = 30182 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 13613 Number of elements = 76414 Number of triangles = 8142 Number of quadrilatarals = 0 Number of tetrahedrals = 68272 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 41618 Number of elements = 236483 Number of triangles = 19838 Number of quadrilatarals = 0 Number of tetrahedrals = 216645 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 4369 Number of elements = 24223 Number of triangles = 3016 Number of quadrilatarals = 0 Number of tetrahedrals = 21207 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 11007 Number of elements = 60837 Number of triangles = 8632 Number of quadrilatarals = 0 Number of tetrahedrals = 52205 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 10474 Number of elements = 58678 Number of triangles = 6352 Number of quadrilatarals = 0 Number of tetrahedrals = 52326 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 88507 Number of elements = 497504 Number of triangles = 51750 Number of quadrilatarals = 0 Number of tetrahedrals = 445754 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:62031) 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16456 Number of elements = 93635 Number of triangles = 7926 Number of quadrilatarals = 0 Number of tetrahedrals = 85709 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2589 Number of elements = 13809 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11051 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3654 Number of elements = 19800 Number of triangles = 3394 Number of quadrilatarals = 0 Number of tetrahedrals = 16406 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5456 Number of elements = 30308 Number of triangles = 3656 Number of quadrilatarals = 0 Number of tetrahedrals = 26652 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4694 Number of elements = 25935 Number of triangles = 3326 Number of quadrilatarals = 0 Number of tetrahedrals = 22609 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5554 Number of elements = 30862 Number of triangles = 3756 Number of quadrilatarals = 0 Number of tetrahedrals = 27106 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2260 Number of elements = 12133 Number of triangles = 2222 Number of quadrilatarals = 0 Number of tetrahedrals = 9911 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2392 Number of elements = 12577 Number of triangles = 2666 Number of quadrilatarals = 0 Number of tetrahedrals = 9911 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3341 Number of elements = 18069 Number of triangles = 3110 Number of quadrilatarals = 0 Number of tetrahedrals = 14959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3606 Number of elements = 18961 Number of triangles = 4002 Number of quadrilatarals = 0 Number of tetrahedrals = 14959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4414 Number of elements = 23974 Number of triangles = 3998 Number of quadrilatarals = 0 Number of tetrahedrals = 19976 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4811 Number of elements = 25310 Number of triangles = 5334 Number of quadrilatarals = 0 Number of tetrahedrals = 19976 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 4): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 4): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 4): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 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 4 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 4): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5490 Number of elements = 29891 Number of triangles = 4886 Number of quadrilatarals = 0 Number of tetrahedrals = 25005 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6019 Number of elements = 31671 Number of triangles = 6666 Number of quadrilatarals = 0 Number of tetrahedrals = 25005 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 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 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 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 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6542 Number of elements = 35667 Number of triangles = 5774 Number of quadrilatarals = 0 Number of tetrahedrals = 29893 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7203 Number of elements = 37891 Number of triangles = 7998 Number of quadrilatarals = 0 Number of tetrahedrals = 29893 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 6): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 6): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 6): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 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 4 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 6): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 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 5 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 6): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 6): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7601 Number of elements = 41489 Number of triangles = 6662 Number of quadrilatarals = 0 Number of tetrahedrals = 34827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8394 Number of elements = 44157 Number of triangles = 9330 Number of quadrilatarals = 0 Number of tetrahedrals = 34827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 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 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 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 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 1191 Number of elements = 6266 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4934 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19800 Number of elements = 109798 Number of triangles = 15540 Number of quadrilatarals = 0 Number of tetrahedrals = 94258 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 8 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 9 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 10 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 11 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 12 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 13 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 14 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 15 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 16 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 17 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 18 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 19 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22741 Number of elements = 119570 Number of triangles = 25312 Number of quadrilatarals = 0 Number of tetrahedrals = 94258 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 19): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 19): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 19): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 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 4 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 19): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 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 5 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 19): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 19): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 19): Number of nodes = 1191 Number of elements = 6266 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4934 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 8 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 8 (of 19): Number of nodes = 1193 Number of elements = 6272 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4940 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 9 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 9 (of 19): Number of nodes = 1176 Number of elements = 6165 Number of triangles = 1330 Number of quadrilatarals = 0 Number of tetrahedrals = 4835 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 10 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 10 (of 19): Number of nodes = 1203 Number of elements = 6314 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4982 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 11 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 11 (of 19): Number of nodes = 1192 Number of elements = 6269 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4937 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 12 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 12 (of 19): Number of nodes = 1192 Number of elements = 6269 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4937 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 13 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 13 (of 19): Number of nodes = 1198 Number of elements = 6296 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4964 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 14 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 14 (of 19): Number of nodes = 1223 Number of elements = 6443 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5111 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 15 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 15 (of 19): Number of nodes = 1184 Number of elements = 6224 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4892 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 16 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 16 (of 19): Number of nodes = 1195 Number of elements = 6287 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4955 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 17 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 17 (of 19): Number of nodes = 1197 Number of elements = 6311 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4979 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 18 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 18 (of 19): Number of nodes = 1203 Number of elements = 6310 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4978 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 19 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 19 (of 19): Number of nodes = 1191 Number of elements = 6253 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4921 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8857 Number of elements = 49191 Number of triangles = 6284 Number of quadrilatarals = 0 Number of tetrahedrals = 42907 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8989 Number of elements = 49635 Number of triangles = 6728 Number of quadrilatarals = 0 Number of tetrahedrals = 42907 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 7796 Number of elements = 43368 Number of triangles = 5396 Number of quadrilatarals = 0 Number of tetrahedrals = 37972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1193 Number of elements = 6267 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4935 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9944 Number of elements = 55193 Number of triangles = 7174 Number of quadrilatarals = 0 Number of tetrahedrals = 48019 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10218 Number of elements = 56081 Number of triangles = 8062 Number of quadrilatarals = 0 Number of tetrahedrals = 48019 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7818 Number of elements = 43469 Number of triangles = 5398 Number of quadrilatarals = 0 Number of tetrahedrals = 38071 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1202 Number of elements = 6320 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4988 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1198 Number of elements = 6292 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4960 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9609 Number of elements = 53228 Number of triangles = 6994 Number of quadrilatarals = 0 Number of tetrahedrals = 46234 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9829 Number of elements = 53956 Number of triangles = 7722 Number of quadrilatarals = 0 Number of tetrahedrals = 46234 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7789 Number of elements = 43295 Number of triangles = 5394 Number of quadrilatarals = 0 Number of tetrahedrals = 37901 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1186 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 854 Number of elements = 4431 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3435 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9348 Number of elements = 51734 Number of triangles = 6812 Number of quadrilatarals = 0 Number of tetrahedrals = 44922 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9531 Number of elements = 52330 Number of triangles = 7408 Number of quadrilatarals = 0 Number of tetrahedrals = 44922 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7804 Number of elements = 43358 Number of triangles = 5386 Number of quadrilatarals = 0 Number of tetrahedrals = 37972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1200 Number of elements = 6311 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4979 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2661 Number of triangles = 690 Number of quadrilatarals = 0 Number of tetrahedrals = 1971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9183 Number of elements = 50871 Number of triangles = 6632 Number of quadrilatarals = 0 Number of tetrahedrals = 44239 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9322 Number of elements = 51307 Number of triangles = 7068 Number of quadrilatarals = 0 Number of tetrahedrals = 44239 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7927 Number of elements = 44116 Number of triangles = 5382 Number of quadrilatarals = 0 Number of tetrahedrals = 38734 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 868 Number of elements = 4530 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3534 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2661 Number of triangles = 690 Number of quadrilatarals = 0 Number of tetrahedrals = 1971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10181 Number of elements = 56797 Number of triangles = 6782 Number of quadrilatarals = 0 Number of tetrahedrals = 50015 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10671 Number of elements = 58561 Number of triangles = 8546 Number of quadrilatarals = 0 Number of tetrahedrals = 50015 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7741 Number of elements = 43010 Number of triangles = 5362 Number of quadrilatarals = 0 Number of tetrahedrals = 37648 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 2692 Number of elements = 14435 Number of triangles = 2800 Number of quadrilatarals = 0 Number of tetrahedrals = 11635 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 238 Number of elements = 1116 Number of triangles = 384 Number of quadrilatarals = 0 Number of tetrahedrals = 732 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1500 Number of elements = 7757 Number of triangles = 1986 Number of quadrilatarals = 0 Number of tetrahedrals = 5771 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1564 Number of elements = 7881 Number of triangles = 2110 Number of quadrilatarals = 0 Number of tetrahedrals = 5771 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1160 Number of elements = 6087 Number of triangles = 1308 Number of quadrilatarals = 0 Number of tetrahedrals = 4779 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 360 Number of elements = 1635 Number of triangles = 718 Number of quadrilatarals = 0 Number of tetrahedrals = 917 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 44 Number of elements = 159 Number of triangles = 84 Number of quadrilatarals = 0 Number of tetrahedrals = 75 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5075 Number of elements = 27761 Number of triangles = 4072 Number of quadrilatarals = 0 Number of tetrahedrals = 23689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5221 Number of elements = 28313 Number of triangles = 4624 Number of quadrilatarals = 0 Number of tetrahedrals = 23689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 4882 Number of elements = 26790 Number of triangles = 4040 Number of quadrilatarals = 0 Number of tetrahedrals = 22750 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 339 Number of elements = 1523 Number of triangles = 584 Number of quadrilatarals = 0 Number of tetrahedrals = 939 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 32776 Number of elements = 189806 Number of triangles = 8496 Number of quadrilatarals = 0 Number of tetrahedrals = 181310 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 36115 Number of elements = 203130 Number of triangles = 21820 Number of quadrilatarals = 0 Number of tetrahedrals = 181310 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 28584 Number of elements = 162362 Number of triangles = 15158 Number of quadrilatarals = 0 Number of tetrahedrals = 147204 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1425 Number of elements = 7592 Number of triangles = 1456 Number of quadrilatarals = 0 Number of tetrahedrals = 6136 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 4138 Number of elements = 22901 Number of triangles = 2938 Number of quadrilatarals = 0 Number of tetrahedrals = 19963 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 711 Number of elements = 3685 Number of triangles = 844 Number of quadrilatarals = 0 Number of tetrahedrals = 2841 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1257 Number of elements = 6590 Number of triangles = 1424 Number of quadrilatarals = 0 Number of tetrahedrals = 5166 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16639 Number of elements = 94369 Number of triangles = 8800 Number of quadrilatarals = 0 Number of tetrahedrals = 85569 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 18563 Number of elements = 101745 Number of triangles = 16176 Number of quadrilatarals = 0 Number of tetrahedrals = 85569 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 12009 Number of elements = 67436 Number of triangles = 7140 Number of quadrilatarals = 0 Number of tetrahedrals = 60296 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 6554 Number of elements = 34309 Number of triangles = 9036 Number of quadrilatarals = 0 Number of tetrahedrals = 25273 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4989 Number of elements = 27641 Number of triangles = 3462 Number of quadrilatarals = 0 Number of tetrahedrals = 24179 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6401 Number of elements = 35742 Number of triangles = 4048 Number of quadrilatarals = 0 Number of tetrahedrals = 31694 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 59702 Number of elements = 348382 Number of triangles = 12928 Number of quadrilatarals = 0 Number of tetrahedrals = 335454 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 58332 Number of elements = 339688 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 327260 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 59702 Number of elements = 347882 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 335454 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:62031) 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:62031) 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:62031) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) 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:62031) 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:62031) 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:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) 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:62031) 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:62031) ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) 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:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 44 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 3 Surface 2: Number of points found for aero-spline = 6 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 8 automatic connections were made for capsConnect Rib_Root (node id 1) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL 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 IEEE_DENORMAL 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 IEEE_DENORMAL 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 IEEE_DENORMAL 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) ... skipped 'No flowCart executable' test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable' test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable' test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable' test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable' test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... 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_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... 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:62031) 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 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 70000BE97000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 70000BE97000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, 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 70000BE97000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 70000BE97000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 113BA0E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 113BA0E00 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 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 70000BE97000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 70000BE97000 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 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 70000BE97000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 70000BE97000 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:62031) 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:62031) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) 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:62031) 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:62031) 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:62031) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) 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:62031) 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:62031) 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:62031) 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:62031) 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:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_egadsTess.TestEGADS.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 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 - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.249704 Creating surface mesh ... Surface mesh seconds: 0.054895 Recovering boundaries... Boundary recovery seconds: 0.164117 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.07545 Recovering Delaunayness... Delaunay recovery seconds: 0.080501 Refining mesh... 18972 insertions, added 13254 points, 701278 tetrahedra in queue. 6317 insertions, added 2883 points, 614952 tetrahedra in queue. 8421 insertions, added 2047 points, 103425 tetrahedra in queue. Refinement seconds: 3.57427 Smoothing vertices... Mesh smoothing seconds: 2.9638 Improving mesh... Mesh improvement seconds: 0.057487 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.022234 Total running seconds: 7.24348 Statistics: Input points: 14233 Input facets: 28454 Input segments: 42681 Input holes: 2 Input regions: 0 Mesh points: 33078 Mesh tetrahedra: 159812 Mesh faces: 333851 Mesh faces on exterior boundary: 28454 Mesh faces on input facets: 28454 Mesh edges on input segments: 42681 Steiner points inside domain: 18845 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 = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 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 - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.1918 Creating surface mesh ... Surface mesh seconds: 0.03724 Recovering boundaries... Boundary recovery seconds: 0.126092 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.058387 Recovering Delaunayness... Delaunay recovery seconds: 0.073362 Refining mesh... 18972 insertions, added 13254 points, 701278 tetrahedra in queue. 6317 insertions, added 2883 points, 614952 tetrahedra in queue. 8421 insertions, added 2047 points, 103425 tetrahedra in queue. Refinement seconds: 2.59891 Smoothing vertices... Mesh smoothing seconds: 2.74815 Improving mesh... Mesh improvement seconds: 0.070417 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.025812 Total running seconds: 5.93105 Statistics: Input points: 14233 Input facets: 28454 Input segments: 42681 Input holes: 2 Input regions: 0 Mesh points: 33078 Mesh tetrahedra: 159812 Mesh faces: 333851 Mesh faces on exterior boundary: 28454 Mesh faces on input facets: 28454 Mesh edges on input segments: 42681 Steiner points inside domain: 18845 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. ok test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found! Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 - 5079, elements - 10146 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 - 5079, elements - 10146 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 - 14233, elements - 28454 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 = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 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 = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 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 = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 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 = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 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 = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 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 = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 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 = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 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 = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 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 = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 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 = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 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 = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 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 = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 0.001 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 225 Number of elements = 450 Number of tris = 396 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1602 Number of elements = 8758 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7518 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2600 Number of elements = 13864 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11106 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1071 Number of elements = 5705 Number of triangles = 998 Number of quadrilatarals = 0 Number of tetrahedrals = 4707 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 15544 Number of elements = 89331 Number of triangles = 4632 Number of quadrilatarals = 0 Number of tetrahedrals = 84699 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1602 Number of elements = 8758 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7518 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 438 Number of elements = 2179 Number of triangles = 644 Number of quadrilatarals = 0 Number of tetrahedrals = 1535 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 ok test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 936 Number of elements = 4999 Number of triangles = 758 Number of quadrilatarals = 0 Number of tetrahedrals = 4241 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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS 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 22.6.0 x86_64 AFLR3 : Compile Date 11/01/23 @ 12:19PM 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 = 0.012 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 25021 AFLR3 IG : Nodes, Elements = 4984 34304 AFLR3 IG : Nodes, Elements = 6227 43518 AFLR3 IG : Nodes, Elements = 6227 43440 AFLR3 IG : Nodes, Elements = 6227 43474 AFLR3 IG : Nodes, Elements = 6227 43437 AFLR3 IG : Nodes, Elements = 6220 26107 AFLR3 IG : Nodes, Elements = 6220 26133 AFLR3 IG : Nodes, Elements = 6220 21538 AFLR3 IG : Nodes, Elements = 6220 19141 AFLR3 : CPU Time = 0.134 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 6220 19141 AFLR3 GG : Nodes, Elements = 9092 27970 AFLR3 GG : Nodes, Elements = 9092 39349 AFLR3 GG : Nodes, Elements = 9092 36380 AFLR3 GG : Nodes, Elements = 9092 34923 AFLR3 GG : Nodes, Elements = 11659 42981 AFLR3 GG : Nodes, Elements = 11659 53807 AFLR3 GG : Nodes, Elements = 11659 50702 AFLR3 GG : Nodes, Elements = 11659 49815 AFLR3 GG : Nodes, Elements = 14477 58553 AFLR3 GG : Nodes, Elements = 14477 70855 AFLR3 GG : Nodes, Elements = 14477 67465 AFLR3 GG : Nodes, Elements = 14477 66533 AFLR3 GG : Nodes, Elements = 17443 75634 AFLR3 GG : Nodes, Elements = 17443 88707 AFLR3 GG : Nodes, Elements = 17443 85026 AFLR3 GG : Nodes, Elements = 17443 84166 AFLR3 GG : Nodes, Elements = 20625 93912 AFLR3 GG : Nodes, Elements = 20625 107483 AFLR3 GG : Nodes, Elements = 20625 103837 AFLR3 GG : Nodes, Elements = 20625 103014 AFLR3 GG : Nodes, Elements = 23983 113245 AFLR3 GG : Nodes, Elements = 23983 127691 AFLR3 GG : Nodes, Elements = 23983 123762 AFLR3 GG : Nodes, Elements = 23983 122939 AFLR3 GG : Nodes, Elements = 27471 133562 AFLR3 GG : Nodes, Elements = 27471 148246 AFLR3 GG : Nodes, Elements = 27471 144367 AFLR3 GG : Nodes, Elements = 27471 143483 AFLR3 GG : Nodes, Elements = 31049 154330 AFLR3 GG : Nodes, Elements = 31049 169629 AFLR3 GG : Nodes, Elements = 31049 165573 AFLR3 GG : Nodes, Elements = 31049 164719 AFLR3 GG : Nodes, Elements = 34642 175591 AFLR3 GG : Nodes, Elements = 34642 190772 AFLR3 GG : Nodes, Elements = 34642 186857 AFLR3 GG : Nodes, Elements = 34642 186049 AFLR3 GG : Nodes, Elements = 38204 196811 AFLR3 GG : Nodes, Elements = 38204 211769 AFLR3 GG : Nodes, Elements = 38204 208011 AFLR3 GG : Nodes, Elements = 38204 207203 AFLR3 GG : Nodes, Elements = 41735 217867 AFLR3 GG : Nodes, Elements = 41735 232734 AFLR3 GG : Nodes, Elements = 41735 228893 AFLR3 GG : Nodes, Elements = 41735 228199 AFLR3 GG : Nodes, Elements = 45118 238407 AFLR3 GG : Nodes, Elements = 45118 252771 AFLR3 GG : Nodes, Elements = 45118 249083 AFLR3 GG : Nodes, Elements = 45118 248399 AFLR3 GG : Nodes, Elements = 48432 258383 AFLR3 GG : Nodes, Elements = 48432 272398 AFLR3 GG : Nodes, Elements = 48432 268767 AFLR3 GG : Nodes, Elements = 48432 268040 AFLR3 GG : Nodes, Elements = 51632 277673 AFLR3 GG : Nodes, Elements = 51632 291124 AFLR3 GG : Nodes, Elements = 51632 287737 AFLR3 GG : Nodes, Elements = 51632 287138 AFLR3 GG : Nodes, Elements = 54742 296489 AFLR3 GG : Nodes, Elements = 54742 309545 AFLR3 GG : Nodes, Elements = 54742 306294 AFLR3 GG : Nodes, Elements = 54742 305700 AFLR3 GG : Nodes, Elements = 57753 314750 AFLR3 GG : Nodes, Elements = 57753 327393 AFLR3 GG : Nodes, Elements = 57753 324205 AFLR3 GG : Nodes, Elements = 57753 323671 AFLR3 GG : Nodes, Elements = 60589 332185 AFLR3 GG : Nodes, Elements = 60589 344195 AFLR3 GG : Nodes, Elements = 60589 341132 AFLR3 GG : Nodes, Elements = 60589 340678 AFLR3 GG : Nodes, Elements = 63303 348823 AFLR3 GG : Nodes, Elements = 63303 360078 AFLR3 GG : Nodes, Elements = 63303 357259 AFLR3 GG : Nodes, Elements = 63303 356861 AFLR3 GG : Nodes, Elements = 65821 364418 AFLR3 GG : Nodes, Elements = 65821 375019 AFLR3 GG : Nodes, Elements = 65821 372315 AFLR3 GG : Nodes, Elements = 65821 371973 AFLR3 GG : Nodes, Elements = 68056 378682 AFLR3 GG : Nodes, Elements = 68056 387933 AFLR3 GG : Nodes, Elements = 68056 385584 AFLR3 GG : Nodes, Elements = 68056 385301 AFLR3 GG : Nodes, Elements = 69951 390988 AFLR3 GG : Nodes, Elements = 69951 398948 AFLR3 GG : Nodes, Elements = 69951 396934 AFLR3 GG : Nodes, Elements = 69951 396704 AFLR3 GG : Nodes, Elements = 71446 401190 AFLR3 GG : Nodes, Elements = 71446 407532 AFLR3 GG : Nodes, Elements = 71446 405836 AFLR3 GG : Nodes, Elements = 71446 405665 AFLR3 GG : Nodes, Elements = 72588 409091 AFLR3 GG : Nodes, Elements = 72588 414051 AFLR3 GG : Nodes, Elements = 72588 412698 AFLR3 GG : Nodes, Elements = 72588 412555 AFLR3 GG : Nodes, Elements = 73412 415028 AFLR3 GG : Nodes, Elements = 73412 418465 AFLR3 GG : Nodes, Elements = 73412 417560 AFLR3 GG : Nodes, Elements = 73412 417491 AFLR3 GG : Nodes, Elements = 73970 419165 AFLR3 GG : Nodes, Elements = 73970 421515 AFLR3 GG : Nodes, Elements = 73970 420850 AFLR3 GG : Nodes, Elements = 73970 420801 AFLR3 GG : Nodes, Elements = 74329 421878 AFLR3 GG : Nodes, Elements = 74329 423409 AFLR3 GG : Nodes, Elements = 74329 422967 AFLR3 GG : Nodes, Elements = 74329 422934 AFLR3 GG : Nodes, Elements = 74527 423528 AFLR3 GG : Nodes, Elements = 74527 424406 AFLR3 GG : Nodes, Elements = 74527 424145 AFLR3 GG : Nodes, Elements = 74527 424123 AFLR3 GG : Nodes, Elements = 74619 424399 AFLR3 GG : Nodes, Elements = 74619 424805 AFLR3 GG : Nodes, Elements = 74619 424686 AFLR3 GG : Nodes, Elements = 74619 424681 AFLR3 GG : Nodes, Elements = 74657 424795 AFLR3 GG : Nodes, Elements = 74657 424951 AFLR3 GG : Nodes, Elements = 74657 424897 AFLR3 GG : Nodes, Elements = 74672 424942 AFLR3 GG : Nodes, Elements = 74672 425006 AFLR3 GG : Nodes, Elements = 74672 424985 AFLR3 GG : Nodes, Elements = 74672 424986 AFLR3 GG : Nodes, Elements = 74673 424989 AFLR3 GG : Nodes, Elements = 74673 424992 AFLR3 GG : Nodes, Elements = 74673 424991 AFLR3 GG : Nodes, Elements = 74696 425060 AFLR3 GG : Nodes, Elements = 74696 425133 AFLR3 GG : Nodes, Elements = 74696 425114 AFLR3 GG : Nodes, Elements = 74696 425117 AFLR3 GG : Nodes, Elements = 74700 425129 AFLR3 GG : Nodes, Elements = 74700 425145 AFLR3 GG : Nodes, Elements = 74700 425140 AFLR3 GG : Nodes, Elements = 74702 425146 AFLR3 GG : Nodes, Elements = 74702 425155 AFLR3 GG : Nodes, Elements = 74702 425152 AFLR3 GG : Nodes, Elements = 74702 425150 AFLR3 : CPU Time = 3.537 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 74702 425150 AFLR3 QI : Nodes, Elements = 73200 416638 AFLR3 QI : Nodes, Elements = 72976 415359 AFLR3 QI : Nodes, Elements = 72961 415273 AFLR3 QI : Nodes, Elements = 72960 415266 AFLR3 QI : Nodes, Elements = 72960 419161 AFLR3 QI : Nodes, Elements = 72960 415035 AFLR3 QI : Nodes, Elements = 72960 414621 AFLR3 QI : Nodes, Elements = 72960 415001 AFLR3 QI : Nodes, Elements = 72960 414373 AFLR3 QI : Nodes, Elements = 72960 414178 AFLR3 QI : Nodes, Elements = 72960 414472 AFLR3 QI : Nodes, Elements = 72960 414145 AFLR3 QI : Nodes, Elements = 72960 414045 AFLR3 QI : Nodes, Elements = 72960 414288 AFLR3 QI : Nodes, Elements = 72960 414039 AFLR3 QI : Nodes, Elements = 72960 413980 AFLR3 QI : Nodes, Elements = 72960 414224 AFLR3 QI : Nodes, Elements = 72960 413989 AFLR3 QI : Nodes, Elements = 72960 413938 AFLR3 QI : Nodes, Elements = 72966 413964 AFLR3 QI : Nodes, Elements = 72966 414196 AFLR3 QI : Nodes, Elements = 72966 413985 AFLR3 QI : Nodes, Elements = 72966 413966 AFLR3 QI : Nodes, Elements = 72966 414195 AFLR3 QI : Nodes, Elements = 72966 413976 AFLR3 QI : Nodes, Elements = 72966 413935 AFLR3 : CPU Time = 1.263 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 72966 413935 AFLR3 QRG: Nodes, Elements = 72978 413998 AFLR3 QRG: Nodes, Elements = 72988 414052 AFLR3 QRG: Nodes, Elements = 72990 414061 AFLR3 QRG: Nodes, Elements = 72991 414065 AFLR3 QRG: Nodes, Elements = 72990 414059 AFLR3 QRG: Nodes, Elements = 72998 414101 AFLR3 QRG: Nodes, Elements = 72998 414099 AFLR3 QRG: Nodes, Elements = 73000 414112 AFLR3 QRG: Nodes, Elements = 73007 414152 AFLR3 : CPU Time = 0.052 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 414152 UG3 : Min, Max Ang = 1.137 170.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 61 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 414152 UG3 : Min Vol = 6.36e-10 UG3 : Average Vol = 5.12 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 = 414152 UG3 : Min, Max Q = 0.0734 1 UG3 : Average Q = 0.894 UG3 : No. Q< 0.1 = 29 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 5.472 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 414152 UG3 : Min, Max Ang = 1.137 170.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 61 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 414152 UG3 : Min Vol = 6.36e-10 UG3 : Average Vol = 5.12 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 = 414152 UG3 : Min, Max Q = 0.223 1 UG3 : Average Q = 0.859 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 7.7.0 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 = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 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:62031) 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) 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 70000BE97000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 70000BE97000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! 113BA0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, 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 = 294 Number of elements = 584 Number of triangle elements = 584 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 = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4192 Total number of elements = 8364 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 - 294, elements - 584 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 - 488, elements - 972 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 - 294, elements - 584 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 - 488, elements - 972 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 - 4192, elements - 8364 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 = 174 Number of elements = 344 Number of triangle elements = 344 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 = 2321 Total number of elements = 4606 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 - 174, elements - 344 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 - 174, elements - 344 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 = 444 Number of elements = 884 Number of triangle elements = 884 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 = 966 Total number of elements = 1928 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 444, elements - 884 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 - 444, elements - 884 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 - 9601, elements - 19194 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 - 9601, elements - 19194 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 - 9601, elements - 19194 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 - 9601, elements - 19194 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 - 9601, elements - 19194 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 - 7173, elements - 14338 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 = 9601 Number of elements = 19194 Number of triangle elements = 19194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9601 Total number of elements = 19194 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok test_Output (test_zaero.TestZAERO.test_Output) ... ok test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1220 Number of elements = 2680 Number of triangle elements = 2680 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1221 Total number of elements = 2680 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1220 Number of elements = 2680 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 2680 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1221 Combined Number of elements = 2681 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2680 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - Rib_Root Property name - Rib_Root_Point Property name - Ribs Property name - Skin Property name - Spar1 Property name - Spar2 Done getting FEA properties Updating mesh element types based on properties input 'Smart_Restart' is ON Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting vortex lattice control surface data VLM control surface name - CntrlLE VLM control surface name - CntrlTE Done getting vortex lattice control surface data Getting FEA vortex lattice mesh Getting ZAERO UAIC Configurations....... Number of UAIC Configurations - 2 UAIC Configuration: climb, id = 1 - Mach Number : 0.200000 - Reduced Freq: [0.020000, ... , 0.250000] UAIC Configuration: cruise, id = 2 - Mach Number : 0.700000 - Reduced Freq: [0.040000, ... , 0.350000] Getting ZAERO Analysis Subcases....... Number of Analysis Subcases - 2 Analysis Subcase: FlutterCruise, id = 1 - Discipline : flutter - UAIC : cruise Analysis Subcase: Trim, id = 2 - Discipline : Trim - UAIC : climb Getting ZAERO Trim Variables....... Number of Trim Variables - 2 Trim Variable: ANGLEA - Label : ALPHA - Value : free Trim Variable: URDD3 - Label : NZ - Value : 1.0 Updating StaticAeroelastic subcase: Trim - vectorToCG -> [0.345898, 1.652951, -0.041403] - weight -> 476456.149985 - weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523] ok ---------------------------------------------------------------------- Ran 144 tests in 542.489s OK (skipped=15) + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/7.7/DARWIN64/ESP_venv/bin/python ================================================= Running.... MINIMAL PyTests ================================================= + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 0.0006119078685748102 CYtot -6.295467348382128e-15 CZtot -0.3012861394885953 Cltot -4.784258926526785e-14 Cmtot -0.1945055953450382 Cntot -2.338191252215186e-15 Cl'tot -4.787610967125373e-14 Cn'tot -1.502866821492718e-15 CLtot 0.3012509314150635 CDtot 0.004646353488232475 CDvis 0.0 CLff 0.3009503023520388 CYff -7.723329422293541e-15 CDind 0.004646353488232475 CDff 0.004968969500907922 e 0.9669902146157789 StripForces Wing cl = [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.3101221284189, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422921, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408] Wing cd = [-0.004234137763162, -0.004494543653192, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946409, 0.000511459807839, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080993, -0.0007386538944077, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653162, -0.004234137764545] real 0m1.353s user 0m0.540s sys 0m0.517s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Cl = [1.05475230553347, 1.36488869373699, 1.5660721427216, 2.03059709348412, 1.97271083121139, 1.87307153172667, 1.7605047576018] Cd = [0.0131991208677172, 0.0166540240605863, 0.0200551482562954, 0.0458671341943513, 0.07542560093961, 0.099446917447585, 0.127479430989108] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.496044115314418, 0.46137773204142, 0.442376568201556, 0.361251636297643, 0.276104140853528, 0.214381239319783, 0.132988264746104] real 0m3.182s user 0m2.690s sys 0m0.199s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Cl = 0.37837932402995744 Cd = 0.0077758580442312715 Cm = 0.005262576090327783 real 0m2.412s user 0m2.121s sys 0m0.269s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 0m0.658s user 0m0.422s sys 0m0.211s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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. Cl = 0.933417 Cd = 0.000284 Cd Wave = 0.0 Cm = -0.203436 Cp _Critcal = -1.303869 real 0m0.602s user 0m0.424s sys 0m0.168s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt delaundo_PyTest.py test; + python -u delaundo_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 0m0.680s user 0m0.603s sys 0m0.289s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_PyTest.py test; + python -u egadsTess_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 0m5.499s user 0m10.482s sys 0m2.011s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr2_PyTest.py test; + python -u aflr2_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 0.001 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 = 0.019 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 = 0.008 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 0m0.671s user 0m0.707s sys 0m0.282s + 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/7.7/DARWIN64/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/7.7/DARWIN64/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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 150173 Number of elements = 449915 Number of triangles = 14380 Number of quadrilatarals = 0 Number of tetrahedrals = 214483 Number of pyramids = 425 Number of prisms = 220627 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m12.805s user 0m11.699s sys 0m0.628s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tetgen_PyTest.py test; + python -u tetgen_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 = 267 Number of elements = 530 Number of triangle elements = 530 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3139 Total number of elements = 6266 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 - 3139, elements - 6266 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.023999 Creating surface mesh ... Surface mesh seconds: 0.007076 Recovering boundaries... Boundary recovery seconds: 0.063323 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.008801 Suppressing Steiner points ... Steiner suppression seconds: 2.9e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.010215 Refining mesh... 4188 insertions, added 2137 points, 127272 tetrahedra in queue. 1394 insertions, added 414 points, 131442 tetrahedra in queue. 1858 insertions, added 464 points, 129858 tetrahedra in queue. 2477 insertions, added 450 points, 111812 tetrahedra in queue. 3302 insertions, added 490 points, 67833 tetrahedra in queue. 4401 insertions, added 401 points, 112 tetrahedra in queue. Refinement seconds: 0.662663 Smoothing vertices... Mesh smoothing seconds: 0.367369 Improving mesh... Mesh improvement seconds: 0.010249 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00366 Total running seconds: 1.15776 Statistics: Input points: 3139 Input facets: 6266 Input segments: 9399 Input holes: 2 Input regions: 0 Mesh points: 7895 Mesh tetrahedra: 38676 Mesh faces: 80485 Mesh faces on exterior boundary: 6266 Mesh faces on input facets: 6266 Mesh edges on input segments: 9399 Steiner points inside domain: 4756 Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file real 0m5.604s user 0m5.544s sys 0m0.334s + 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/7.7/DARWIN64/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/7.7/DARWIN64/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 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM 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 = 0.014 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| 7.6995e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 7.4023e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.1402e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.0304e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.1217e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 7.1808e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 7.1434e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 7.0832e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 7.0100e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 6.9811e-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 0m2.282s user 0m1.859s sys 0m0.607s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'astros_ThreeBar_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedForce Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards real 0m0.707s user 0m0.545s sys 0m0.274s + 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/7.7/DARWIN64/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/7.7/DARWIN64/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 IEEE_DENORMAL real 0m1.006s user 0m0.731s sys 0m0.371s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 3.428666259747 Mass 5383.006027803 Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11] CG [1.222256036874, 0.1634981473778, -4.234574416087e-11] Ixx 22133.97306033 Iyy 23448.30046709 Izz 1389.213122582 Ixy 164.2055275657 Ixz -7.454849830627e-06 Iyz 1.707682983295e-06 I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06] II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]] real 0m4.341s user 0m6.917s sys 0m2.470s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + python -u hsm_SingleLoadCase_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 81 Number of elements = 96 Elemental Tria3 = 0 Elemental Quad4 = 64 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 32 ->HSMSOL Matrix Non-zero Entries = 5741 Converging HSM equation system ... iter dr dd dp rlx max 1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00) 1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00) 2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00) 2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00) 4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00) 5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00) 6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00) 7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00) Converging n vectors ... it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 ) it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 ) Converging e1,e2 vectors ... it = 1 de = 0.691E-03 rlx = 1.000 ( 45 ) it = 2 de = 0.404E-04 rlx = 1.000 ( 9 ) it = 3 de = 0.142E-07 rlx = 1.000 ( 46 ) it = 4 de = 0.521E-11 rlx = 1.000 ( 62 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat real 0m0.776s user 0m0.612s sys 0m0.161s + 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/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt ../corsairlite/qp.py test; + python -u ../corsairlite/qp.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 0m23.052s user 0m1.684s sys 0m0.286s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: abaqus awave Cart3D Mystran ================================================= All tests pass! ================================================= ================================================= + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64 + mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/test/plugs + cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/test/plugs + find /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs -name 'plugs0*.csm' + sort -f + awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/data/plugs/plugsFailure.txt + cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/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 51856 -rw-r--r-- 1 jenkins staff 1.2M May 22 11:22 ASTRO.D01 -rw-r--r-- 1 jenkins staff 277K May 22 11:22 ASTRO.IDX -rwxr-xr-x 1 jenkins staff 131K May 22 11:22 ESPxddm -rwxr-xr-x 1 jenkins staff 229K May 22 11:22 Slugs -rwxr-xr-x 1 jenkins staff 102K May 22 11:22 TestFit -rwxr-xr-x 1 jenkins staff 1.8M May 22 11:22 avl -rwxr-xr-x 1 jenkins staff 50K May 22 11:22 cart3dTest -rwxr-xr-x 1 jenkins staff 50K May 22 11:20 egads2cart -rwxr-xr-x 1 jenkins staff 86K May 22 11:22 egads2cgt -rwxr-xr-x 1 jenkins staff 383K May 22 11:22 friction -rwxr-xr-x 1 jenkins staff 8.9M May 22 11:22 mastros.exe -rwxr-xr-x 1 jenkins staff 2.2M May 22 11:22 mses -rwxr-xr-x 1 jenkins staff 2.5M May 22 11:22 mset -rwxr-xr-x 1 jenkins staff 51K May 22 11:22 phaseUtil -rw-r--r-- 1 jenkins staff 1.6K May 22 11:24 pod.egads -rw-r--r-- 1 jenkins staff 0B May 22 11:24 port7681.jrnl -rwxr-xr-x 1 jenkins staff 1.2M May 22 11:22 pplot -rwxr-xr-x 1 jenkins staff 1.2M May 22 11:22 pxplot -rwxr-xr-x 1 jenkins staff 84K May 22 11:21 sensCSM -rwxr-xr-x 1 jenkins staff 224K May 22 11:21 serveCSM -rwxr-xr-x 1 jenkins staff 192K May 22 11:21 serveESP -rwxr-xr-x 1 jenkins staff 68K May 22 11:20 vCurvature -rwxr-xr-x 1 jenkins staff 51K May 22 11:20 vGeom -rwxr-xr-x 1 jenkins staff 52K May 22 11:20 vTess -rwxr-xr-x 1 jenkins staff 2.3M May 22 11:20 vTesstatic -rw-r--r-- 1 jenkins staff 195K May 22 11:24 wingMultiModel.bdf -rwxr-xr-x 1 jenkins staff 1.8M May 22 11:22 xfoil ( 1 / 4 ) data/Plugs/plugs0a.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/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/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m8.152s user 0m7.233s sys 0m0.441s ++ set +x data/Plugs/plugs0a passed (as expected) -------------------------------------------------------------------------------------------------- ( 2 / 4 ) data/Plugs/plugs0b.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/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/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m6.943s user 0m8.495s sys 0m0.079s ++ set +x data/Plugs/plugs0b passed (as expected) -------------------------------------------------------------------------------------------------- ( 3 / 4 ) data/Plugs/plugs0c.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/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/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m19.606s user 0m29.488s sys 0m0.166s ++ set +x data/Plugs/plugs0c passed (as expected) -------------------------------------------------------------------------------------------------- ( 4 / 4 ) data/Plugs/plugs0d.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/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/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m19.412s user 0m29.309s sys 0m0.160s ++ set +x data/Plugs/plugs0d passed (as expected) -------------------------------------------------------------------------------------------------- [Execution node] check if [macys_VM] is in [[viggen]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [macys_VM] 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/7.7/DARWIN64') [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/7.7/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64') [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/7.7/DARWIN64') [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/7.7/DARWIN64') [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/7.7/DARWIN64') [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=7.7,ESP_ARCH=DARWIN64,buildnode=macys_VM #717'. [Checks API] No suitable checks publisher found. [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] done Finished: SUCCESS