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Started by upstream project "ESP_Beta" build number 702 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 '2024-04-03T12:23:18.495 -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 2475 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 '2024-04-03T12:23:18.495 -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 851 No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [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/jenkins16028674907120801210.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=7.6 ++ OCCTREF=7.6 ++ AFLR_VERSION=11.5.9 ++ SU2_VERSION=8.0.0 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.34.0 ++ export PYTHON_VERSION=3.11.6 ++ PYTHON_VERSION=3.11.6 ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ [[ 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 ++ [[ 7.6 != '' ]] ++ [[ '' != '' ]] ++ [[ 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_11.5.9 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9 ++ [[ 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-3.34.0-MacOS ++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/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 ]] ++ 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 5902ms 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==69.1.1, wheel==0.42.0 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-3.31.1-py3-none-any.whl Collecting networkx>=2.0 (from openmdao) Using cached networkx-3.2.1-py3-none-any.whl.metadata (5.2 kB) Requirement already satisfied: numpy in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4) Collecting scipy (from openmdao) Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB) Collecting requests (from openmdao) Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB) Collecting packaging (from openmdao) Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB) Collecting charset-normalizer<4,>=2 (from requests->openmdao) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (33 kB) Collecting idna<4,>=2.5 (from requests->openmdao) Using cached idna-3.6-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-3.2.1-py3-none-any.whl (1.6 MB) Using cached packaging-24.0-py3-none-any.whl (53 kB) Using cached requests-2.31.0-py3-none-any.whl (62 kB) Using cached scipy-1.13.0-cp311-cp311-macosx_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-3.6-py3-none-any.whl (61 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-3.6 networkx-3.2.1 openmdao-3.31.1 packaging-24.0 requests-2.31.0 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-3.8.3-cp311-cp311-macosx_10_12_x86_64.whl.metadata (5.8 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-4.50.0-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<2,>=1.21 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4) Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.0) Collecting pillow>=8 (from matplotlib) Using cached pillow-10.3.0-cp311-cp311-macosx_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-3.8.3-cp311-cp311-macosx_10_12_x86_64.whl (7.6 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-4.50.0-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-4.50.0 kiwisolver-1.4.5 matplotlib-3.8.3 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 --2024-04-03 12:24:38-- 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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.......... .......... .......... .......... 1% 276M 67s 4750K .......... .......... .......... .......... .......... 1% 351M 67s 4800K .......... .......... .......... .......... .......... 1% 346M 66s 4850K .......... .......... .......... .......... .......... 1% 300M 65s 4900K .......... .......... .......... .......... .......... 1% 346M 65s 4950K .......... .......... .......... .......... .......... 1% 303M 64s 5000K .......... .......... .......... .......... .......... 1% 351M 63s 5050K .......... .......... .......... .......... .......... 1% 341M 63s 5100K .......... .......... .......... .......... .......... 1% 287K 71s 5150K .......... .......... .......... .......... .......... 1% 127M 70s 5200K .......... .......... .......... .......... .......... 1% 102M 69s 5250K .......... .......... .......... .......... .......... 2% 83.5M 69s 5300K .......... .......... .......... .......... .......... 2% 181M 68s 5350K .......... .......... .......... .......... .......... 2% 155M 68s 5400K .......... .......... .......... .......... .......... 2% 313M 67s 5450K .......... .......... .......... .......... .......... 2% 221M 66s 5500K .......... .......... .......... .......... .......... 2% 270M 66s 5550K .......... .......... .......... .......... .......... 2% 281M 65s 5600K .......... .......... .......... .......... .......... 2% 187M 65s 5650K .......... .......... .......... .......... .......... 2% 268M 64s 5700K .......... .......... .......... .......... .......... 2% 137M 63s 5750K .......... .......... .......... .......... .......... 2% 221M 63s 5800K .......... .......... .......... .......... .......... 2% 250M 62s 5850K .......... .......... .......... .......... .......... 2% 62.2K 97s 5900K .......... .......... .......... .......... .......... 2% 248M 96s 5950K .......... .......... .......... .......... .......... 2% 133M 95s 6000K .......... .......... .......... .......... .......... 2% 189M 95s 6050K .......... .......... .......... .......... .......... 2% 156M 94s 6100K .......... .......... .......... .......... .......... 2% 135M 93s 6150K .......... .......... .......... .......... .......... 2% 268M 92s 6200K .......... .......... .......... .......... .......... 2% 257M 91s 6250K .......... .......... .......... .......... .......... 2% 294M 91s 6300K .......... .......... .......... .......... .......... 2% 238M 90s 6350K .......... .......... .......... .......... .......... 2% 143M 89s 6400K .......... .......... .......... .......... .......... 2% 223M 89s 6450K .......... .......... .......... .......... .......... 2% 254M 88s 6500K .......... .......... .......... .......... .......... 2% 250M 87s 6550K .......... .......... .......... .......... .......... 2% 264M 87s 6600K .......... .......... .......... .......... .......... 2% 254M 86s 6650K .......... .......... .......... .......... .......... 2% 265M 85s 6700K .......... .......... .......... .......... .......... 2% 257M 85s 6750K .......... .......... .......... .......... .......... 2% 267M 84s 6800K .......... .......... .......... .......... .......... 2% 260M 83s 6850K .......... .......... .......... .......... .......... 2% 274M 83s 6900K .......... .......... .......... .......... .......... 2% 289M 82s 6950K .......... .......... .......... .......... .......... 2% 258M 82s 7000K .......... .......... .......... .......... .......... 2% 2.58M 82s 7050K .......... .......... .......... .......... .......... 2% 126M 81s 7100K .......... .......... .......... .......... .......... 2% 222M 81s 7150K .......... .......... .......... .......... .......... 2% 317M 80s 7200K .......... .......... .......... .......... .......... 2% 134M 79s 7250K .......... .......... .......... .......... .......... 2% 270M 79s 7300K .......... .......... .......... .......... .......... 2% 161M 78s 7350K .......... .......... .......... .......... .......... 2% 220M 78s 7400K .......... .......... .......... .......... .......... 2% 273M 77s 7450K .......... .......... .......... .......... .......... 2% 233M 77s 7500K .......... .......... .......... .......... .......... 2% 274M 76s 7550K .......... .......... .......... .......... .......... 2% 271M 76s 7600K .......... .......... .......... .......... .......... 2% 207M 75s 7650K .......... .......... .......... .......... .......... 2% 160M 75s 7700K .......... .......... .......... .......... .......... 2% 179M 74s 7750K .......... .......... .......... .......... .......... 2% 233M 74s 7800K .......... .......... .......... .......... .......... 2% 296M 73s 7850K .......... .......... .......... .......... .......... 2% 258M 73s 7900K .......... .......... .......... .......... .......... 3% 223M 72s 7950K .......... .......... .......... .......... .......... 3% 184M 72s 8000K .......... .......... .......... .......... .......... 3% 213M 71s 8050K .......... .......... .......... .......... .......... 3% 216M 71s 8100K .......... .......... .......... .......... .......... 3% 234M 70s 8150K .......... .......... .......... .......... .......... 3% 16.4M 70s 8200K .......... .......... .......... .......... .......... 3% 5.67M 70s 8250K .......... .......... .......... .......... .......... 3% 108M 70s 8300K .......... .......... .......... .......... .......... 3% 44.9M 69s 8350K .......... .......... .......... .......... .......... 3% 245M 69s 8400K .......... .......... .......... .......... .......... 3% 160M 68s 8450K .......... .......... .......... .......... .......... 3% 227M 68s 8500K .......... .......... .......... .......... .......... 3% 292M 68s 8550K .......... .......... .......... .......... .......... 3% 301M 67s 8600K .......... .......... .......... .......... .......... 3% 257M 67s 8650K .......... .......... .......... .......... .......... 3% 242M 66s 8700K .......... .......... .......... .......... .......... 3% 263M 66s 8750K .......... .......... .......... .......... .......... 3% 261M 66s 8800K .......... .......... .......... .......... .......... 3% 276M 65s 8850K .......... .......... .......... .......... .......... 3% 218M 65s 8900K .......... .......... .......... .......... .......... 3% 300M 64s 8950K .......... .......... .......... .......... .......... 3% 276M 64s 9000K .......... .......... .......... .......... .......... 3% 267M 64s 9050K .......... .......... .......... .......... .......... 3% 284M 63s 9100K .......... .......... .......... .......... .......... 3% 277M 63s 9150K .......... .......... .......... .......... .......... 3% 298M 63s 9200K .......... .......... .......... .......... .......... 3% 6.97M 62s 9250K .......... .......... .......... .......... .......... 3% 192M 62s 9300K .......... .......... .......... .......... .......... 3% 214M 62s 9350K .......... .......... .......... .......... .......... 3% 4.17M 62s 9400K .......... .......... .......... .......... .......... 3% 176M 61s 9450K .......... .......... .......... .......... .......... 3% 112M 61s 9500K .......... .......... .......... .......... .......... 3% 188M 61s 9550K .......... .......... .......... .......... .......... 3% 328M 60s 9600K .......... .......... .......... .......... .......... 3% 249M 60s 9650K .......... .......... .......... .......... .......... 3% 317M 60s 9700K .......... .......... .......... .......... .......... 3% 292M 60s 9750K .......... .......... .......... .......... .......... 3% 172M 59s 9800K .......... .......... .......... .......... .......... 3% 126M 59s 9850K .......... .......... .......... .......... .......... 3% 2.57M 59s 9900K .......... .......... .......... .......... .......... 3% 226M 59s 9950K .......... .......... .......... .......... .......... 3% 198M 58s 10000K .......... .......... .......... .......... .......... 3% 252M 58s 10050K .......... .......... .......... .......... .......... 3% 231M 58s 10100K .......... .......... .......... .......... .......... 3% 107M 58s 10150K .......... .......... .......... .......... .......... 3% 301M 57s 10200K .......... .......... .......... .......... .......... 3% 28.6M 57s 10250K .......... .......... .......... .......... .......... 3% 219M 57s 10300K .......... .......... .......... .......... .......... 3% 249M 57s 10350K .......... .......... .......... .......... .......... 3% 157M 56s 10400K .......... .......... .......... .......... .......... 3% 180M 56s 10450K .......... .......... .......... .......... .......... 3% 31.5M 56s 10500K .......... .......... .......... .......... .......... 3% 175M 55s 10550K .......... .......... .......... .......... .......... 4% 247M 55s 10600K .......... .......... .......... .......... .......... 4% 187M 55s 10650K .......... .......... .......... .......... .......... 4% 191M 55s 10700K .......... .......... .......... .......... .......... 4% 122M 54s 10750K .......... .......... .......... .......... .......... 4% 244M 54s 10800K .......... .......... .......... .......... .......... 4% 291M 54s 10850K .......... .......... .......... .......... .......... 4% 225M 54s 10900K .......... .......... .......... .......... .......... 4% 267M 53s 10950K .......... .......... .......... .......... .......... 4% 148M 53s 11000K .......... .......... .......... .......... .......... 4% 153M 53s 11050K .......... .......... .......... .......... .......... 4% 254M 53s 11100K .......... .......... .......... .......... .......... 4% 245M 52s 11150K .......... .......... .......... .......... .......... 4% 250M 52s 11200K .......... .......... .......... .......... .......... 4% 237M 52s 11250K .......... .......... .......... .......... .......... 4% 2.14M 52s 11300K .......... .......... .......... .......... .......... 4% 229M 52s 11350K .......... .......... .......... .......... .......... 4% 120M 52s 11400K .......... .......... .......... .......... .......... 4% 174M 52s 11450K .......... .......... .......... .......... .......... 4% 164M 51s 11500K .......... .......... .......... .......... .......... 4% 317M 51s 11550K .......... .......... .......... .......... .......... 4% 184M 51s 11600K .......... .......... .......... .......... .......... 4% 253M 51s 11650K .......... .......... .......... .......... .......... 4% 221M 50s 11700K .......... .......... .......... .......... .......... 4% 225M 50s 11750K .......... .......... .......... .......... .......... 4% 249M 50s 11800K .......... .......... .......... .......... .......... 4% 267M 50s 11850K .......... .......... .......... .......... .......... 4% 235M 50s 11900K .......... .......... .......... .......... .......... 4% 250M 49s 11950K .......... .......... .......... .......... .......... 4% 219M 49s 12000K .......... .......... .......... .......... .......... 4% 212M 49s 12050K .......... .......... .......... .......... .......... 4% 291M 49s 12100K .......... .......... .......... .......... .......... 4% 222M 48s 12150K .......... .......... .......... .......... .......... 4% 231M 48s 12200K .......... .......... .......... .......... .......... 4% 182M 48s 12250K .......... .......... .......... .......... .......... 4% 11.0M 48s 12300K .......... .......... .......... .......... .......... 4% 162M 48s 12350K .......... .......... .......... .......... .......... 4% 218M 48s 12400K .......... .......... .......... .......... .......... 4% 144M 47s 12450K .......... .......... .......... .......... .......... 4% 210M 47s 12500K .......... .......... .......... .......... .......... 4% 298M 47s 12550K .......... .......... .......... .......... .......... 4% 178M 47s 12600K .......... .......... .......... .......... .......... 4% 176M 47s 12650K .......... .......... .......... .......... .......... 4% 239M 46s 12700K .......... .......... .......... .......... .......... 4% 196M 46s 12750K .......... .......... .......... .......... .......... 4% 273M 46s 12800K .......... .......... .......... .......... .......... 4% 223M 46s 12850K .......... .......... .......... .......... .......... 4% 163M 46s 12900K .......... .......... .......... .......... .......... 4% 230M 45s 12950K .......... .......... .......... .......... .......... 4% 164M 45s 13000K .......... .......... .......... .......... .......... 4% 205M 45s 13050K .......... .......... .......... .......... .......... 4% 137M 45s 13100K .......... .......... .......... .......... .......... 4% 248M 45s 13150K .......... .......... .......... .......... .......... 5% 265M 45s 13200K .......... .......... .......... .......... .......... 5% 134M 44s 13250K .......... .......... .......... .......... .......... 5% 228M 44s 13300K .......... .......... .......... .......... .......... 5% 4.32M 44s 13350K .......... .......... .......... .......... .......... 5% 78.1M 44s 13400K .......... .......... .......... .......... .......... 5% 183M 44s 13450K .......... .......... .......... .......... .......... 5% 178M 44s 13500K .......... .......... .......... .......... .......... 5% 147M 44s 13550K .......... .......... .......... .......... .......... 5% 271M 43s 13600K .......... .......... .......... .......... .......... 5% 110M 43s 13650K .......... .......... .......... .......... .......... 5% 82.9M 43s 13700K .......... .......... .......... .......... .......... 5% 154M 43s 13750K .......... .......... .......... .......... .......... 5% 253M 43s 13800K .......... .......... .......... .......... .......... 5% 307M 43s 13850K .......... .......... .......... .......... .......... 5% 257M 43s 13900K .......... .......... .......... .......... .......... 5% 7.52M 42s 13950K .......... .......... .......... .......... .......... 5% 129M 42s 14000K .......... .......... .......... .......... .......... 5% 225M 42s 14050K .......... .......... .......... .......... .......... 5% 204M 42s 14100K .......... .......... .......... .......... .......... 5% 203M 42s 14150K .......... .......... .......... .......... .......... 5% 300M 42s 14200K .......... .......... .......... .......... .......... 5% 207M 42s 14250K .......... .......... .......... .......... .......... 5% 253M 41s 14300K .......... .......... .......... .......... .......... 5% 8.71M 41s 14350K .......... .......... .......... .......... .......... 5% 90.9M 41s 14400K .......... .......... .......... .......... .......... 5% 103M 41s 14450K .......... .......... .......... .......... .......... 5% 124M 41s 14500K .......... .......... .......... .......... .......... 5% 149M 41s 14550K .......... .......... .......... .......... .......... 5% 249M 41s 14600K .......... .......... .......... .......... .......... 5% 152M 40s 14650K .......... .......... .......... .......... .......... 5% 125M 40s 14700K .......... .......... .......... .......... .......... 5% 161M 40s 14750K .......... .......... .......... .......... .......... 5% 205M 40s 14800K .......... .......... .......... .......... .......... 5% 237M 40s 14850K .......... .......... .......... .......... .......... 5% 215M 40s 14900K .......... .......... .......... .......... .......... 5% 220M 40s 14950K .......... .......... .......... .......... .......... 5% 167M 40s 15000K .......... .......... .......... .......... .......... 5% 235M 39s 15050K .......... .......... .......... .......... .......... 5% 159M 39s 15100K .......... .......... .......... .......... .......... 5% 130M 39s 15150K .......... .......... .......... .......... .......... 5% 147M 39s 15200K .......... .......... .......... .......... .......... 5% 196M 39s 15250K .......... .......... .......... .......... .......... 5% 260M 39s 15300K .......... .......... .......... .......... .......... 5% 273M 39s 15350K .......... .......... .......... .......... .......... 5% 2.21M 39s 15400K .......... .......... .......... .......... .......... 5% 211M 39s 15450K .......... .......... .......... .......... .......... 5% 191M 39s 15500K .......... .......... .......... .......... .......... 5% 6.70M 39s 15550K .......... .......... .......... .......... .......... 5% 94.6M 38s 15600K .......... .......... .......... .......... .......... 5% 244M 38s 15650K .......... .......... .......... .......... .......... 5% 194M 38s 15700K .......... .......... .......... .......... .......... 5% 244M 38s 15750K .......... .......... .......... .......... .......... 5% 226M 38s 15800K .......... .......... .......... .......... .......... 6% 300M 38s 15850K .......... .......... .......... .......... .......... 6% 230M 38s 15900K .......... .......... .......... .......... .......... 6% 237M 38s 15950K .......... .......... .......... .......... .......... 6% 211M 37s 16000K .......... .......... .......... .......... .......... 6% 264M 37s 16050K .......... .......... .......... .......... .......... 6% 286M 37s 16100K .......... .......... .......... .......... .......... 6% 216M 37s 16150K .......... .......... .......... .......... .......... 6% 286M 37s 16200K .......... .......... .......... .......... .......... 6% 245M 37s 16250K .......... .......... .......... .......... .......... 6% 284M 37s 16300K .......... .......... .......... .......... .......... 6% 273M 37s 16350K .......... .......... .......... .......... .......... 6% 3.60M 37s 16400K .......... .......... .......... .......... .......... 6% 186M 37s 16450K .......... .......... .......... .......... .......... 6% 146M 36s 16500K .......... .......... .......... .......... .......... 6% 152M 36s 16550K .......... .......... .......... .......... .......... 6% 138M 36s 16600K .......... .......... .......... .......... .......... 6% 217M 36s 16650K .......... .......... .......... .......... .......... 6% 179M 36s 16700K .......... .......... .......... .......... .......... 6% 196M 36s 16750K .......... .......... .......... .......... .......... 6% 214M 36s 16800K .......... .......... .......... .......... .......... 6% 243M 36s 16850K .......... .......... .......... .......... .......... 6% 102M 36s 16900K .......... .......... .......... .......... .......... 6% 189M 35s 16950K .......... .......... .......... .......... .......... 6% 176M 35s 17000K .......... .......... .......... .......... .......... 6% 169M 35s 17050K .......... .......... .......... .......... .......... 6% 155M 35s 17100K .......... .......... .......... .......... .......... 6% 3.78M 35s 17150K .......... .......... .......... .......... .......... 6% 140M 35s 17200K .......... .......... .......... .......... .......... 6% 203M 35s 17250K .......... .......... .......... .......... .......... 6% 126M 35s 17300K .......... .......... .......... .......... .......... 6% 204M 35s 17350K .......... .......... .......... .......... .......... 6% 194M 35s 17400K .......... .......... .......... .......... .......... 6% 3.53M 35s 17450K .......... .......... .......... .......... .......... 6% 89.3M 35s 17500K .......... .......... .......... .......... .......... 6% 163M 35s 17550K .......... .......... .......... .......... .......... 6% 170M 34s 17600K .......... .......... .......... .......... .......... 6% 144M 34s 17650K .......... .......... .......... .......... .......... 6% 242M 34s 17700K .......... .......... .......... .......... .......... 6% 227M 34s 17750K .......... .......... .......... .......... .......... 6% 279M 34s 17800K .......... .......... .......... .......... .......... 6% 281M 34s 17850K .......... .......... .......... .......... .......... 6% 230M 34s 17900K .......... .......... .......... .......... .......... 6% 250M 34s 17950K .......... .......... .......... .......... .......... 6% 215M 34s 18000K .......... .......... .......... .......... .......... 6% 244M 34s 18050K .......... .......... .......... .......... .......... 6% 247M 33s 18100K .......... .......... .......... .......... .......... 6% 241M 33s 18150K .......... .......... .......... .......... .......... 6% 264M 33s 18200K .......... .......... .......... .......... .......... 6% 252M 33s 18250K .......... .......... .......... .......... .......... 6% 248M 33s 18300K .......... .......... .......... .......... .......... 6% 268M 33s 18350K .......... .......... .......... .......... .......... 6% 241M 33s 18400K .......... .......... .......... .......... .......... 6% 67.0K 43s 18450K .......... .......... .......... .......... .......... 7% 90.6M 43s 18500K .......... .......... .......... .......... .......... 7% 154M 43s 18550K .......... .......... .......... .......... .......... 7% 149M 42s 18600K .......... .......... .......... .......... .......... 7% 177M 42s 18650K .......... .......... .......... .......... .......... 7% 214M 42s 18700K .......... .......... .......... .......... .......... 7% 95.7M 42s 18750K .......... .......... .......... .......... .......... 7% 248M 42s 18800K .......... .......... .......... .......... .......... 7% 223M 42s 18850K .......... .......... .......... .......... .......... 7% 202M 42s 18900K .......... .......... .......... .......... .......... 7% 300M 42s 18950K .......... .......... .......... .......... .......... 7% 228M 41s 19000K .......... .......... .......... .......... .......... 7% 265M 41s 19050K .......... .......... .......... .......... .......... 7% 286M 41s 19100K .......... .......... .......... .......... .......... 7% 231M 41s 19150K .......... .......... .......... .......... .......... 7% 241M 41s 19200K .......... .......... .......... .......... .......... 7% 191M 41s 19250K .......... .......... .......... .......... .......... 7% 219M 41s 19300K .......... .......... .......... .......... .......... 7% 140M 41s 19350K .......... .......... .......... .......... .......... 7% 139M 41s 19400K .......... .......... .......... .......... .......... 7% 279M 40s 19450K .......... .......... .......... .......... .......... 7% 13.6M 40s 19500K .......... .......... .......... .......... .......... 7% 103M 40s 19550K .......... .......... .......... .......... .......... 7% 113M 40s 19600K .......... .......... .......... .......... .......... 7% 131M 40s 19650K .......... .......... .......... .......... .......... 7% 253M 40s 19700K .......... .......... .......... .......... .......... 7% 149M 40s 19750K .......... .......... .......... .......... .......... 7% 170M 40s 19800K .......... .......... .......... .......... .......... 7% 215M 40s 19850K .......... .......... .......... .......... .......... 7% 163M 40s 19900K .......... .......... .......... .......... .......... 7% 228M 39s 19950K .......... .......... .......... .......... .......... 7% 177M 39s 20000K .......... .......... .......... .......... .......... 7% 204M 39s 20050K .......... .......... .......... .......... .......... 7% 138M 39s 20100K .......... .......... .......... .......... .......... 7% 183M 39s 20150K .......... .......... .......... .......... .......... 7% 218M 39s 20200K .......... .......... .......... .......... .......... 7% 244M 39s 20250K .......... .......... .......... .......... .......... 7% 219M 39s 20300K .......... .......... .......... .......... .......... 7% 211M 39s 20350K .......... .......... .......... .......... .......... 7% 219M 39s 20400K .......... .......... .......... .......... .......... 7% 277M 38s 20450K .......... .......... .......... .......... .......... 7% 54.9M 38s 20500K .......... .......... .......... .......... .......... 7% 126M 38s 20550K .......... .......... .......... .......... .......... 7% 102M 38s 20600K .......... .......... .......... .......... .......... 7% 104M 38s 20650K .......... .......... .......... .......... .......... 7% 147M 38s 20700K .......... .......... .......... .......... .......... 7% 102M 38s 20750K .......... .......... .......... .......... .......... 7% 139M 38s 20800K .......... .......... .......... .......... .......... 7% 222M 38s 20850K .......... .......... .......... .......... .......... 7% 100M 38s 20900K .......... .......... .......... .......... .......... 7% 220M 37s 20950K .......... .......... .......... .......... .......... 7% 260M 37s 21000K .......... .......... .......... .......... .......... 7% 260M 37s 21050K .......... .......... .......... .......... .......... 7% 237M 37s 21100K .......... .......... .......... .......... .......... 8% 177M 37s 21150K .......... .......... .......... .......... .......... 8% 252M 37s 21200K .......... .......... .......... .......... .......... 8% 292M 37s 21250K .......... .......... .......... .......... .......... 8% 346M 37s 21300K .......... .......... .......... .......... .......... 8% 351M 37s 21350K .......... .......... .......... .......... .......... 8% 301M 37s 21400K .......... .......... .......... .......... .......... 8% 273M 37s 21450K .......... .......... .......... .......... .......... 8% 301M 36s 21500K .......... .......... .......... .......... .......... 8% 62.3K 45s 21550K .......... .......... .......... .......... .......... 8% 135M 45s 21600K .......... .......... .......... .......... .......... 8% 58.4M 45s 21650K .......... .......... .......... .......... .......... 8% 140M 45s 21700K .......... .......... .......... .......... .......... 8% 82.8M 45s 21750K .......... .......... .......... .......... .......... 8% 138M 45s 21800K .......... .......... .......... .......... .......... 8% 145M 45s 21850K .......... .......... .......... .......... .......... 8% 184M 45s 21900K .......... .......... .......... .......... .......... 8% 162M 45s 21950K .......... .......... .......... .......... .......... 8% 152M 44s 22000K .......... .......... .......... .......... .......... 8% 160M 44s 22050K .......... .......... .......... .......... .......... 8% 217M 44s 22100K .......... .......... .......... .......... .......... 8% 154M 44s 22150K .......... .......... .......... .......... .......... 8% 162M 44s 22200K .......... .......... .......... .......... .......... 8% 135M 44s 22250K .......... .......... .......... .......... .......... 8% 138M 44s 22300K .......... .......... .......... .......... .......... 8% 54.3M 44s 22350K .......... .......... .......... .......... .......... 8% 61.2M 44s 22400K .......... .......... .......... .......... .......... 8% 172M 43s 22450K .......... .......... .......... .......... .......... 8% 91.4M 43s 22500K .......... .......... .......... .......... .......... 8% 9.98M 43s 22550K .......... .......... .......... .......... .......... 8% 28.2M 43s 22600K .......... .......... .......... .......... .......... 8% 21.9M 43s 22650K .......... .......... .......... .......... .......... 8% 24.0M 43s 22700K .......... .......... .......... .......... .......... 8% 20.6M 43s 22750K .......... .......... .......... .......... .......... 8% 22.6M 43s 22800K .......... .......... .......... .......... .......... 8% 20.7M 43s 22850K .......... .......... .......... .......... .......... 8% 72.7K 50s 22900K .......... .......... .......... .......... .......... 8% 158M 50s 22950K .......... .......... .......... .......... .......... 8% 211M 50s 23000K .......... .......... .......... .......... .......... 8% 221M 50s 23050K .......... .......... .......... .......... .......... 8% 216M 50s 23100K .......... .......... .......... .......... .......... 8% 115M 49s 23150K .......... .......... .......... .......... .......... 8% 243M 49s 23200K .......... .......... .......... .......... .......... 8% 164M 49s 23250K .......... .......... .......... .......... .......... 8% 154M 49s 23300K .......... .......... .......... .......... .......... 8% 184M 49s 23350K .......... .......... .......... .......... .......... 8% 2.60M 49s 23400K .......... .......... .......... .......... .......... 8% 99.6M 49s 23450K .......... .......... .......... .......... .......... 8% 108M 49s 23500K .......... .......... .......... .......... .......... 8% 9.58M 49s 23550K .......... .......... .......... .......... .......... 8% 77.1M 49s 23600K .......... .......... .......... .......... .......... 8% 95.7M 49s 23650K .......... .......... .......... .......... .......... 8% 145M 48s 23700K .......... .......... .......... .......... .......... 9% 125M 48s 23750K .......... .......... .......... .......... .......... 9% 140M 48s 23800K .......... .......... .......... .......... .......... 9% 109M 48s 23850K .......... .......... .......... .......... .......... 9% 142M 48s 23900K .......... .......... .......... .......... .......... 9% 17.1M 48s 23950K .......... .......... .......... .......... .......... 9% 154M 48s 24000K .......... .......... .......... .......... .......... 9% 271M 48s 24050K .......... .......... .......... .......... .......... 9% 289M 48s 24100K .......... .......... .......... .......... .......... 9% 157M 47s 24150K .......... .......... .......... .......... .......... 9% 11.2M 47s 24200K .......... .......... .......... .......... .......... 9% 152M 47s 24250K .......... .......... .......... .......... .......... 9% 223M 47s 24300K .......... .......... .......... .......... .......... 9% 192M 47s 24350K .......... .......... .......... .......... .......... 9% 166M 47s 24400K .......... .......... .......... .......... .......... 9% 11.3M 47s 24450K .......... .......... .......... .......... .......... 9% 82.6M 47s 24500K .......... .......... .......... .......... .......... 9% 241M 47s 24550K .......... .......... .......... .......... .......... 9% 20.4M 47s 24600K .......... .......... .......... .......... .......... 9% 121M 47s 24650K .......... .......... .......... .......... .......... 9% 5.56M 47s 24700K .......... .......... .......... .......... .......... 9% 228M 46s 24750K .......... .......... .......... .......... .......... 9% 10.5M 46s 24800K .......... .......... .......... .......... .......... 9% 200M 46s 24850K .......... .......... .......... .......... .......... 9% 177M 46s 24900K .......... .......... .......... .......... .......... 9% 258M 46s 24950K .......... .......... .......... .......... .......... 9% 186M 46s 25000K .......... .......... .......... .......... .......... 9% 14.2M 46s 25050K .......... .......... .......... .......... .......... 9% 137M 46s 25100K .......... .......... .......... .......... .......... 9% 128M 46s 25150K .......... .......... .......... .......... .......... 9% 222M 46s 25200K .......... .......... .......... .......... .......... 9% 257M 46s 25250K .......... .......... .......... .......... .......... 9% 13.5M 45s 25300K .......... .......... .......... .......... .......... 9% 11.7M 45s 25350K .......... .......... .......... .......... .......... 9% 182M 45s 25400K .......... .......... .......... .......... .......... 9% 284M 45s 25450K .......... .......... .......... .......... .......... 9% 183M 45s 25500K .......... .......... .......... .......... .......... 9% 274M 45s 25550K .......... .......... .......... .......... .......... 9% 9.09M 45s 25600K .......... .......... .......... .......... .......... 9% 96.9M 45s 25650K .......... .......... .......... .......... .......... 9% 122M 45s 25700K .......... .......... .......... .......... .......... 9% 152M 45s 25750K .......... .......... .......... .......... .......... 9% 21.0M 45s 25800K .......... .......... .......... .......... .......... 9% 177M 45s 25850K .......... .......... .......... .......... .......... 9% 17.1M 44s 25900K .......... .......... .......... .......... .......... 9% 271M 44s 25950K .......... .......... .......... .......... .......... 9% 16.1M 44s 26000K .......... .......... .......... .......... .......... 9% 208M 44s 26050K .......... .......... .......... .......... .......... 9% 14.0M 44s 26100K .......... .......... .......... .......... .......... 9% 16.8M 44s 26150K .......... .......... .......... .......... .......... 9% 206M 44s 26200K .......... .......... .......... .......... .......... 9% 15.6M 44s 26250K .......... .......... .......... .......... .......... 9% 265M 44s 26300K .......... .......... .......... .......... .......... 9% 15.6M 44s 26350K .......... .......... .......... .......... .......... 10% 82.6M 44s 26400K .......... .......... .......... .......... .......... 10% 15.7M 44s 26450K .......... .......... .......... .......... .......... 10% 167M 44s 26500K .......... .......... .......... .......... .......... 10% 16.2M 43s 26550K .......... .......... .......... .......... .......... 10% 264M 43s 26600K .......... .......... .......... .......... .......... 10% 14.4M 43s 26650K .......... .......... .......... .......... .......... 10% 139M 43s 26700K .......... .......... .......... .......... .......... 10% 14.3M 43s 26750K .......... .......... .......... .......... .......... 10% 305M 43s 26800K .......... .......... .......... .......... .......... 10% 12.0M 43s 26850K .......... .......... .......... .......... .......... 10% 178M 43s 26900K .......... .......... .......... .......... .......... 10% 13.8M 43s 26950K .......... .......... .......... .......... .......... 10% 95.4M 43s 27000K .......... .......... .......... .......... .......... 10% 13.9M 43s 27050K .......... .......... .......... .......... .......... 10% 148M 43s 27100K .......... .......... .......... .......... .......... 10% 12.3M 43s 27150K .......... .......... .......... .......... .......... 10% 296M 43s 27200K .......... .......... .......... .......... .......... 10% 13.7M 42s 27250K .......... .......... .......... .......... .......... 10% 175M 42s 27300K .......... .......... .......... .......... .......... 10% 14.0M 42s 27350K .......... .......... .......... .......... .......... 10% 228M 42s 27400K .......... .......... .......... .......... .......... 10% 12.8M 42s 27450K .......... .......... .......... .......... .......... 10% 82.9M 42s 27500K .......... .......... .......... .......... .......... 10% 14.9M 42s 27550K .......... .......... .......... .......... .......... 10% 168M 42s 27600K .......... .......... .......... .......... .......... 10% 86.7M 42s 27650K .......... .......... .......... .......... .......... 10% 14.0M 42s 27700K .......... .......... .......... .......... .......... 10% 249M 42s 27750K .......... .......... .......... .......... .......... 10% 12.6M 42s 27800K .......... .......... .......... .......... .......... 10% 263M 42s 27850K .......... .......... .......... .......... .......... 10% 9.02M 42s 27900K .......... .......... .......... .......... .......... 10% 282M 41s 27950K .......... .......... .......... .......... .......... 10% 12.1M 41s 28000K .......... .......... .......... .......... .......... 10% 166M 41s 28050K .......... .......... .......... .......... .......... 10% 12.8M 41s 28100K .......... .......... .......... .......... .......... 10% 166M 41s 28150K .......... .......... .......... .......... .......... 10% 13.1M 41s 28200K .......... .......... .......... .......... .......... 10% 166M 41s 28250K .......... .......... .......... .......... .......... 10% 14.4M 41s 28300K .......... .......... .......... .......... .......... 10% 161M 41s 28350K .......... .......... .......... .......... .......... 10% 179M 41s 28400K .......... .......... .......... .......... .......... 10% 14.8M 41s 28450K .......... .......... .......... .......... .......... 10% 117M 41s 28500K .......... .......... .......... .......... .......... 10% 15.2M 41s 28550K .......... .......... .......... .......... .......... 10% 93.4M 41s 28600K .......... .......... .......... .......... .......... 10% 14.4M 41s 28650K .......... .......... .......... .......... .......... 10% 718K 41s 28700K .......... .......... .......... .......... .......... 10% 11.5M 41s 28750K .......... .......... .......... .......... .......... 10% 176M 41s 28800K .......... .......... .......... .......... .......... 10% 147M 41s 28850K .......... .......... .......... .......... .......... 10% 13.7M 41s 28900K .......... 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.......... .......... .......... 11% 188M 40s 29600K .......... .......... .......... .......... .......... 11% 206M 40s 29650K .......... .......... .......... .......... .......... 11% 13.5M 40s 29700K .......... .......... .......... .......... .......... 11% 156M 40s 29750K .......... .......... .......... .......... .......... 11% 14.1M 40s 29800K .......... .......... .......... .......... .......... 11% 277M 40s 29850K .......... .......... .......... .......... .......... 11% 15.0M 40s 29900K .......... .......... .......... .......... .......... 11% 212M 39s 29950K .......... .......... .......... .......... .......... 11% 154M 39s 30000K .......... .......... .......... .......... .......... 11% 14.0M 39s 30050K .......... .......... .......... .......... .......... 11% 163M 39s 30100K .......... .......... .......... .......... .......... 11% 13.7M 39s 30150K .......... .......... .......... .......... .......... 11% 298M 39s 30200K .......... .......... .......... .......... .......... 11% 14.1M 39s 30250K .......... .......... .......... .......... .......... 11% 270M 39s 30300K .......... .......... .......... .......... .......... 11% 245M 39s 30350K .......... .......... .......... .......... .......... 11% 14.3M 39s 30400K .......... .......... .......... .......... .......... 11% 222M 39s 30450K .......... .......... .......... .......... .......... 11% 14.2M 39s 30500K .......... .......... .......... .......... .......... 11% 265M 39s 30550K .......... .......... .......... .......... .......... 11% 176M 39s 30600K .......... .......... .......... .......... .......... 11% 14.3M 39s 30650K .......... .......... .......... .......... .......... 11% 148M 39s 30700K .......... .......... .......... .......... .......... 11% 367K 40s 30750K .......... .......... .......... .......... .......... 11% 140M 39s 30800K .......... .......... .......... .......... .......... 11% 92.0M 39s 30850K .......... .......... .......... .......... .......... 11% 182M 39s 30900K .......... .......... .......... .......... .......... 11% 146M 39s 30950K .......... .......... .......... .......... .......... 11% 87.2M 39s 31000K .......... .......... .......... .......... .......... 11% 101M 39s 31050K .......... .......... .......... .......... .......... 11% 8.87M 39s 31100K .......... .......... .......... .......... .......... 11% 134M 39s 31150K .......... .......... .......... .......... .......... 11% 180M 39s 31200K .......... .......... .......... .......... .......... 11% 11.1M 39s 31250K .......... .......... .......... .......... .......... 11% 203M 39s 31300K .......... .......... .......... .......... .......... 11% 13.8M 39s 31350K .......... .......... .......... .......... .......... 11% 134M 39s 31400K .......... .......... .......... .......... .......... 11% 236M 39s 31450K .......... .......... .......... .......... .......... 11% 12.6M 39s 31500K .......... .......... .......... .......... .......... 11% 137M 39s 31550K .......... .......... .......... .......... .......... 11% 217M 38s 31600K .......... .......... .......... .......... .......... 11% 11.0M 38s 31650K .......... .......... .......... .......... .......... 12% 198M 38s 31700K .......... .......... .......... .......... .......... 12% 6.00M 38s 31750K .......... .......... .......... .......... .......... 12% 111M 38s 31800K .......... .......... .......... .......... .......... 12% 164M 38s 31850K .......... .......... .......... .......... .......... 12% 7.49M 38s 31900K .......... .......... .......... .......... .......... 12% 204M 38s 31950K .......... .......... .......... .......... .......... 12% 8.53M 38s 32000K .......... .......... .......... .......... .......... 12% 146M 38s 32050K .......... .......... .......... .......... .......... 12% 79.8M 38s 32100K .......... .......... .......... .......... .......... 12% 8.35M 38s 32150K .......... .......... .......... .......... .......... 12% 201M 38s 32200K .......... .......... .......... .......... .......... 12% 186M 38s 32250K .......... .......... .......... .......... .......... 12% 7.92M 38s 32300K .......... .......... .......... .......... .......... 12% 133M 38s 32350K .......... .......... .......... .......... .......... 12% 8.93M 38s 32400K .......... .......... .......... .......... .......... 12% 112M 38s 32450K .......... .......... .......... .......... .......... 12% 92.1M 38s 32500K .......... .......... .......... .......... .......... 12% 11.7M 38s 32550K .......... .......... .......... .......... .......... 12% 217M 38s 32600K .......... .......... .......... .......... .......... 12% 171M 37s 32650K .......... .......... .......... .......... .......... 12% 10.7M 37s 32700K .......... .......... .......... .......... .......... 12% 6.54M 37s 32750K .......... .......... .......... .......... .......... 12% 91.6M 37s 32800K .......... .......... .......... .......... .......... 12% 173M 37s 32850K .......... .......... .......... .......... .......... 12% 161M 37s 32900K .......... .......... .......... .......... .......... 12% 197M 37s 32950K .......... .......... .......... .......... .......... 12% 14.9M 37s 33000K .......... .......... .......... .......... .......... 12% 114M 37s 33050K .......... .......... .......... .......... .......... 12% 11.9M 37s 33100K .......... .......... .......... .......... .......... 12% 90.1M 37s 33150K .......... .......... .......... .......... .......... 12% 11.7M 37s 33200K .......... .......... .......... .......... .......... 12% 253M 37s 33250K .......... .......... .......... .......... .......... 12% 11.7M 37s 33300K .......... .......... .......... .......... .......... 12% 138M 37s 33350K .......... .......... .......... .......... .......... 12% 11.5M 37s 33400K .......... .......... .......... .......... .......... 12% 143M 37s 33450K .......... .......... .......... .......... .......... 12% 11.0M 37s 33500K .......... .......... 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.......... .......... 12% 245M 36s 34200K .......... .......... .......... .......... .......... 12% 11.1M 36s 34250K .......... .......... .......... .......... .......... 13% 183M 36s 34300K .......... .......... .......... .......... .......... 13% 11.1M 36s 34350K .......... .......... .......... .......... .......... 13% 113M 36s 34400K .......... .......... .......... .......... .......... 13% 10.9M 36s 34450K .......... .......... .......... .......... .......... 13% 97.7M 36s 34500K .......... .......... .......... .......... .......... 13% 11.3M 36s 34550K .......... .......... .......... .......... .......... 13% 140M 36s 34600K .......... .......... .......... .......... .......... 13% 11.1M 36s 34650K .......... .......... .......... .......... .......... 13% 213M 36s 34700K .......... .......... .......... .......... .......... 13% 10.4M 36s 34750K .......... .......... .......... .......... .......... 13% 128M 35s 34800K .......... .......... .......... .......... .......... 13% 1.26M 36s 34850K .......... .......... .......... .......... .......... 13% 9.82M 36s 34900K .......... .......... .......... .......... .......... 13% 260M 36s 34950K .......... .......... .......... .......... .......... 13% 9.14M 36s 35000K .......... .......... .......... .......... .......... 13% 226M 36s 35050K .......... .......... .......... .......... .......... 13% 10.6M 35s 35100K .......... .......... .......... .......... .......... 13% 117M 35s 35150K .......... .......... .......... .......... .......... 13% 10.1M 35s 35200K .......... .......... .......... .......... .......... 13% 165M 35s 35250K .......... .......... .......... .......... .......... 13% 10.2M 35s 35300K .......... .......... .......... .......... .......... 13% 112M 35s 35350K .......... .......... .......... .......... .......... 13% 10.3M 35s 35400K .......... .......... .......... .......... .......... 13% 113M 35s 35450K .......... .......... .......... .......... .......... 13% 9.11M 35s 35500K .......... .......... .......... .......... .......... 13% 140M 35s 35550K .......... .......... .......... .......... .......... 13% 210M 35s 35600K .......... .......... .......... .......... .......... 13% 10.0M 35s 35650K .......... .......... .......... .......... .......... 13% 124M 35s 35700K .......... .......... .......... .......... .......... 13% 9.48M 35s 35750K .......... .......... .......... .......... .......... 13% 158M 35s 35800K .......... .......... .......... .......... .......... 13% 9.50M 35s 35850K .......... .......... .......... .......... .......... 13% 198M 35s 35900K .......... .......... .......... .......... .......... 13% 229M 35s 35950K .......... .......... .......... .......... .......... 13% 9.31M 35s 36000K .......... .......... .......... .......... .......... 13% 174M 35s 36050K .......... .......... .......... .......... .......... 13% 9.97M 35s 36100K .......... .......... .......... .......... .......... 13% 105M 35s 36150K .......... .......... .......... .......... .......... 13% 9.25M 35s 36200K .......... .......... .......... .......... .......... 13% 75.7M 35s 36250K .......... .......... .......... .......... .......... 13% 9.40M 34s 36300K .......... .......... .......... .......... .......... 13% 106M 34s 36350K .......... .......... .......... .......... .......... 13% 97.7M 34s 36400K .......... .......... .......... .......... .......... 13% 9.32M 34s 36450K .......... .......... .......... .......... .......... 13% 178M 34s 36500K .......... .......... .......... .......... .......... 13% 9.29M 34s 36550K .......... .......... .......... .......... .......... 13% 90.9M 34s 36600K .......... .......... .......... .......... .......... 13% 9.90M 34s 36650K .......... .......... .......... .......... .......... 13% 180M 34s 36700K .......... .......... .......... .......... .......... 13% 217M 34s 36750K .......... .......... .......... .......... .......... 13% 9.22M 34s 36800K .......... 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.......... 14% 6.52M 33s 38800K .......... .......... .......... .......... .......... 14% 137M 33s 38850K .......... .......... .......... .......... .......... 14% 7.92M 33s 38900K .......... .......... .......... .......... .......... 14% 98.0M 33s 38950K .......... .......... .......... .......... .......... 14% 147M 32s 39000K .......... .......... .......... .......... .......... 14% 7.62M 32s 39050K .......... .......... .......... .......... .......... 14% 323M 32s 39100K .......... .......... .......... .......... .......... 14% 170M 32s 39150K .......... .......... .......... .......... .......... 14% 9.57M 32s 39200K .......... .......... .......... .......... .......... 14% 174M 32s 39250K .......... .......... .......... .......... .......... 14% 8.46M 32s 39300K .......... .......... .......... .......... .......... 14% 110M 32s 39350K .......... .......... .......... .......... .......... 14% 138M 32s 39400K .......... .......... .......... .......... .......... 14% 8.74M 32s 39450K .......... .......... .......... .......... .......... 14% 129M 32s 39500K .......... .......... .......... .......... .......... 14% 177M 32s 39550K .......... .......... .......... .......... .......... 15% 8.67M 32s 39600K .......... .......... .......... .......... .......... 15% 268M 32s 39650K .......... .......... .......... .......... .......... 15% 8.74M 32s 39700K .......... .......... .......... .......... .......... 15% 75.2M 32s 39750K .......... .......... .......... .......... .......... 15% 171M 32s 39800K .......... .......... .......... .......... .......... 15% 9.35M 32s 39850K .......... .......... .......... .......... .......... 15% 260M 32s 39900K .......... .......... .......... .......... .......... 15% 138M 32s 39950K .......... .......... .......... .......... .......... 15% 10.9M 32s 40000K .......... .......... .......... .......... .......... 15% 264M 32s 40050K .......... .......... .......... .......... .......... 15% 189M 32s 40100K 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18% 8.28M 26s 50000K .......... .......... .......... .......... .......... 18% 99.4M 26s 50050K .......... .......... .......... .......... .......... 18% 208M 26s 50100K .......... .......... .......... .......... .......... 19% 8.90M 26s 50150K .......... .......... .......... .......... .......... 19% 64.3M 26s 50200K .......... .......... .......... .......... .......... 19% 127M 26s 50250K .......... .......... .......... .......... .......... 19% 9.64M 26s 50300K .......... .......... .......... .......... .......... 19% 127M 26s 50350K .......... .......... .......... .......... .......... 19% 204M 26s 50400K .......... .......... .......... .......... .......... 19% 7.39M 26s 50450K .......... .......... .......... .......... .......... 19% 76.3M 26s 50500K .......... .......... .......... .......... .......... 19% 107M 26s 50550K .......... .......... .......... .......... .......... 19% 7.08M 26s 50600K .......... .......... .......... .......... .......... 19% 142M 26s 50650K .......... .......... .......... .......... .......... 19% 156M 26s 50700K .......... .......... .......... .......... .......... 19% 12.0M 26s 50750K .......... .......... .......... .......... .......... 19% 242M 26s 50800K .......... .......... .......... .......... .......... 19% 230M 26s 50850K .......... .......... .......... .......... .......... 19% 12.8M 26s 50900K .......... .......... .......... .......... .......... 19% 162M 26s 50950K .......... .......... .......... .......... .......... 19% 100M 26s 51000K .......... .......... .......... .......... .......... 19% 11.7M 26s 51050K .......... .......... .......... .......... .......... 19% 112M 26s 51100K .......... .......... .......... .......... .......... 19% 122M 26s 51150K .......... .......... .......... .......... .......... 19% 223M 26s 51200K .......... .......... .......... .......... .......... 19% 2.07M 26s 51250K .......... .......... .......... .......... .......... 19% 207M 26s 51300K .......... 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25s 61900K .......... .......... .......... .......... .......... 23% 9.84M 25s 61950K .......... .......... .......... .......... .......... 23% 187M 25s 62000K .......... .......... .......... .......... .......... 23% 141M 25s 62050K .......... .......... .......... .......... .......... 23% 11.6M 25s 62100K .......... .......... .......... .......... .......... 23% 183M 25s 62150K .......... .......... .......... .......... .......... 23% 185M 25s 62200K .......... .......... .......... .......... .......... 23% 13.8M 25s 62250K .......... .......... .......... .......... .......... 23% 150M 25s 62300K .......... .......... .......... .......... .......... 23% 188M 25s 62350K .......... .......... .......... .......... .......... 23% 13.4M 25s 62400K .......... .......... .......... .......... .......... 23% 134M 25s 62450K .......... .......... .......... .......... .......... 23% 13.0M 25s 62500K .......... .......... .......... .......... .......... 23% 139M 25s 62550K 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6.78M 23s 67200K .......... .......... .......... .......... .......... 25% 253M 23s 67250K .......... .......... .......... .......... .......... 25% 227M 23s 67300K .......... .......... .......... .......... .......... 25% 15.2M 23s 67350K .......... .......... .......... .......... .......... 25% 7.71M 23s 67400K .......... .......... .......... .......... .......... 25% 212M 23s 67450K .......... .......... .......... .......... .......... 25% 131M 23s 67500K .......... .......... .......... .......... .......... 25% 5.24M 23s 67550K .......... .......... .......... .......... .......... 25% 70.9M 23s 67600K .......... .......... .......... .......... .......... 25% 238M 23s 67650K .......... .......... .......... .......... .......... 25% 5.04M 23s 67700K .......... .......... .......... .......... .......... 25% 183M 23s 67750K .......... .......... .......... .......... .......... 25% 162M 23s 67800K .......... .......... .......... .......... .......... 25% 95.4M 23s 67850K 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.......... 34% 175M 17s 92300K .......... .......... .......... .......... .......... 35% 12.3M 17s 92350K .......... .......... .......... .......... .......... 35% 89.1M 17s 92400K .......... .......... .......... .......... .......... 35% 199M 17s 92450K .......... .......... .......... .......... .......... 35% 12.2M 17s 92500K .......... .......... .......... .......... .......... 35% 178M 17s 92550K .......... .......... .......... .......... .......... 35% 13.2M 17s 92600K .......... .......... .......... .......... .......... 35% 152M 17s 92650K .......... .......... .......... .......... .......... 35% 12.6M 17s 92700K .......... .......... .......... .......... .......... 35% 141M 17s 92750K .......... .......... .......... .......... .......... 35% 11.4M 17s 92800K .......... .......... .......... .......... .......... 35% 181M 17s 92850K .......... .......... .......... .......... .......... 35% 122M 17s 92900K .......... .......... .......... .......... .......... 35% 12.2M 17s 92950K .......... .......... .......... .......... .......... 35% 132M 17s 93000K .......... .......... .......... .......... .......... 35% 9.72M 17s 93050K .......... .......... .......... .......... .......... 35% 154M 17s 93100K .......... .......... .......... .......... .......... 35% 12.5M 17s 93150K .......... .......... .......... .......... .......... 35% 211K 18s 93200K .......... .......... .......... .......... .......... 35% 224M 18s 93250K .......... .......... .......... .......... .......... 35% 92.5M 17s 93300K .......... .......... .......... .......... .......... 35% 180M 17s 93350K .......... .......... .......... .......... .......... 35% 74.7M 17s 93400K .......... .......... .......... .......... .......... 35% 93.5M 17s 93450K .......... .......... .......... .......... .......... 35% 141M 17s 93500K .......... .......... .......... .......... .......... 35% 287M 17s 93550K .......... .......... .......... .......... .......... 35% 309M 17s 93600K .......... .......... .......... .......... .......... 35% 16.2M 17s 93650K .......... .......... .......... .......... .......... 35% 144M 17s 93700K .......... .......... .......... .......... .......... 35% 8.05M 17s 93750K .......... .......... .......... .......... .......... 35% 145M 17s 93800K .......... .......... .......... .......... .......... 35% 13.5M 17s 93850K .......... .......... .......... .......... .......... 35% 91.1M 17s 93900K .......... .......... .......... .......... .......... 35% 6.37M 17s 93950K .......... .......... .......... .......... .......... 35% 164M 17s 94000K .......... .......... .......... .......... .......... 35% 7.14M 17s 94050K .......... .......... .......... .......... .......... 35% 182M 17s 94100K .......... .......... .......... .......... .......... 35% 6.04M 17s 94150K .......... .......... .......... .......... .......... 35% 97.9M 17s 94200K .......... .......... .......... .......... .......... 35% 77.6M 17s 94250K .......... .......... .......... .......... .......... 35% 6.18M 17s 94300K .......... .......... .......... .......... .......... 35% 95.2M 17s 94350K .......... .......... .......... .......... .......... 35% 148M 17s 94400K .......... .......... .......... .......... .......... 35% 7.54M 17s 94450K .......... .......... .......... .......... .......... 35% 169M 17s 94500K .......... .......... .......... .......... .......... 35% 10.8M 17s 94550K .......... .......... .......... .......... .......... 35% 106M 17s 94600K .......... .......... .......... .......... .......... 35% 182M 17s 94650K .......... .......... .......... .......... .......... 35% 5.23M 17s 94700K .......... .......... .......... .......... .......... 35% 116M 17s 94750K .......... .......... .......... .......... .......... 35% 3.91M 17s 94800K .......... .......... .......... .......... .......... 35% 166M 17s 94850K .......... .......... .......... .......... .......... 35% 104M 17s 94900K .......... .......... .......... .......... .......... 35% 5.39M 17s 94950K .......... .......... .......... .......... .......... 36% 136M 17s 95000K .......... .......... .......... .......... .......... 36% 4.76M 17s 95050K .......... .......... .......... .......... .......... 36% 194M 17s 95100K .......... .......... .......... .......... .......... 36% 168M 17s 95150K .......... .......... .......... .......... .......... 36% 7.97M 17s 95200K .......... .......... .......... .......... .......... 36% 115M 17s 95250K .......... .......... .......... .......... .......... 36% 5.50M 17s 95300K .......... .......... .......... .......... .......... 36% 143M 17s 95350K .......... .......... .......... .......... .......... 36% 115M 17s 95400K .......... .......... .......... .......... .......... 36% 4.72M 17s 95450K .......... .......... .......... .......... .......... 36% 102M 17s 95500K .......... .......... .......... .......... .......... 36% 186M 17s 95550K .......... .......... .......... 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.......... 36% 4.33M 17s 96250K .......... .......... .......... .......... .......... 36% 227K 17s 96300K .......... .......... .......... .......... .......... 36% 104M 17s 96350K .......... .......... .......... .......... .......... 36% 127M 17s 96400K .......... .......... .......... .......... .......... 36% 177M 17s 96450K .......... .......... .......... .......... .......... 36% 141M 17s 96500K .......... .......... .......... .......... .......... 36% 134M 17s 96550K .......... .......... .......... .......... .......... 36% 92.5M 17s 96600K .......... .......... .......... .......... .......... 36% 141M 17s 96650K .......... .......... .......... .......... .......... 36% 214M 17s 96700K .......... .......... .......... .......... .......... 36% 4.48M 17s 96750K .......... .......... .......... .......... .......... 36% 161M 17s 96800K .......... .......... .......... .......... .......... 36% 150M 17s 96850K .......... .......... .......... .......... .......... 36% 6.43M 17s 96900K .......... .......... .......... .......... .......... 36% 157M 17s 96950K .......... .......... .......... .......... .......... 36% 20.6M 17s 97000K .......... .......... .......... .......... .......... 36% 10.3M 17s 97050K .......... .......... .......... .......... .......... 36% 190M 17s 97100K .......... .......... .......... .......... .......... 36% 25.3M 17s 97150K .......... .......... .......... .......... .......... 36% 6.82M 17s 97200K .......... .......... .......... .......... .......... 36% 144M 17s 97250K .......... .......... .......... .......... .......... 36% 80.7M 17s 97300K .......... .......... .......... .......... .......... 36% 6.54M 17s 97350K .......... .......... .......... .......... .......... 36% 141M 17s 97400K .......... .......... .......... .......... .......... 36% 252M 17s 97450K .......... .......... .......... .......... .......... 36% 5.96M 17s 97500K .......... .......... .......... .......... .......... 36% 71.9M 17s 97550K 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.......... 45% 6.65M 14s 119700K .......... .......... .......... .......... .......... 45% 81.7M 14s 119750K .......... .......... .......... .......... .......... 45% 77.4M 14s 119800K .......... .......... .......... .......... .......... 45% 6.43M 14s 119850K .......... .......... .......... .......... .......... 45% 167M 14s 119900K .......... .......... .......... .......... .......... 45% 115M 14s 119950K .......... .......... .......... .......... .......... 45% 6.09M 14s 120000K .......... .......... .......... .......... .......... 45% 119M 14s 120050K .......... .......... .......... .......... .......... 45% 115M 14s 120100K .......... .......... .......... .......... .......... 45% 9.83M 14s 120150K .......... .......... .......... .......... .......... 45% 164M 14s 120200K .......... .......... .......... .......... .......... 45% 86.1M 14s 120250K .......... .......... .......... .......... .......... 45% 11.3M 14s 120300K .......... .......... .......... .......... .......... 45% 99.9M 14s 120350K .......... .......... .......... .......... .......... 45% 116M 14s 120400K .......... .......... .......... .......... .......... 45% 10.7M 14s 120450K .......... .......... .......... .......... .......... 45% 197M 14s 120500K .......... .......... .......... .......... .......... 45% 201M 14s 120550K .......... .......... .......... .......... .......... 45% 10.2M 14s 120600K .......... .......... .......... .......... .......... 45% 105M 14s 120650K .......... .......... .......... .......... .......... 45% 113M 14s 120700K .......... .......... .......... .......... .......... 45% 9.96M 14s 120750K .......... .......... .......... .......... .......... 45% 212M 14s 120800K .......... .......... .......... .......... .......... 45% 110M 14s 120850K .......... .......... .......... .......... .......... 45% 11.0M 14s 120900K .......... .......... .......... .......... .......... 45% 138M 14s 120950K .......... .......... .......... .......... .......... 45% 171M 14s 121000K .......... .......... .......... .......... .......... 45% 10.4M 14s 121050K .......... .......... .......... .......... .......... 45% 165M 14s 121100K .......... .......... .......... .......... .......... 45% 151M 14s 121150K .......... .......... .......... .......... .......... 45% 9.66M 14s 121200K .......... .......... .......... .......... .......... 45% 133M 14s 121250K .......... .......... .......... .......... .......... 45% 190M 14s 121300K .......... .......... .......... .......... .......... 46% 9.85M 14s 121350K .......... .......... .......... .......... .......... 46% 164M 14s 121400K .......... .......... .......... .......... .......... 46% 204M 14s 121450K .......... .......... .......... .......... .......... 46% 9.44M 14s 121500K .......... .......... .......... .......... .......... 46% 214M 14s 121550K .......... .......... .......... .......... .......... 46% 121M 14s 121600K .......... .......... .......... .......... .......... 46% 9.93M 14s 121650K .......... .......... .......... .......... .......... 46% 125M 14s 121700K .......... .......... .......... .......... .......... 46% 92.8M 14s 121750K .......... .......... .......... .......... .......... 46% 10.2M 14s 121800K .......... .......... .......... .......... .......... 46% 182M 14s 121850K .......... .......... .......... .......... .......... 46% 84.3M 14s 121900K .......... .......... .......... .......... .......... 46% 11.1M 14s 121950K .......... .......... .......... .......... .......... 46% 122M 14s 122000K .......... .......... .......... .......... .......... 46% 126M 14s 122050K .......... .......... .......... .......... .......... 46% 9.84M 14s 122100K .......... .......... .......... .......... .......... 46% 117M 14s 122150K .......... .......... .......... .......... .......... 46% 95.2M 14s 122200K .......... .......... .......... .......... .......... 46% 9.42M 14s 122250K .......... .......... .......... .......... .......... 46% 180M 14s 122300K .......... .......... .......... .......... .......... 46% 127M 14s 122350K .......... .......... .......... .......... .......... 46% 10.1M 14s 122400K .......... .......... .......... .......... .......... 46% 166M 14s 122450K .......... .......... .......... .......... .......... 46% 199M 14s 122500K .......... .......... .......... .......... .......... 46% 9.43M 14s 122550K .......... .......... .......... .......... .......... 46% 128M 14s 122600K .......... .......... .......... .......... .......... 46% 106M 14s 122650K .......... .......... .......... .......... .......... 46% 9.84M 14s 122700K .......... .......... .......... .......... .......... 46% 85.8M 14s 122750K .......... .......... .......... .......... .......... 46% 122M 14s 122800K .......... .......... .......... .......... .......... 46% 89.4M 14s 122850K .......... .......... .......... .......... .......... 46% 343K 14s 122900K .......... .......... .......... .......... .......... 46% 119M 14s 122950K .......... .......... .......... .......... .......... 46% 135M 14s 123000K .......... .......... .......... .......... .......... 46% 120M 14s 123050K .......... .......... .......... .......... .......... 46% 163M 14s 123100K .......... .......... .......... .......... .......... 46% 176M 14s 123150K .......... .......... .......... .......... .......... 46% 261M 14s 123200K .......... .......... .......... .......... .......... 46% 254M 14s 123250K .......... .......... .......... .......... .......... 46% 289M 14s 123300K .......... .......... .......... .......... .......... 46% 261M 14s 123350K .......... .......... .......... .......... .......... 46% 5.13M 14s 123400K .......... .......... .......... .......... .......... 46% 183M 14s 123450K .......... .......... .......... .......... .......... 46% 184M 14s 123500K .......... .......... .......... .......... .......... 46% 5.92M 14s 123550K .......... .......... .......... .......... .......... 46% 133M 14s 123600K .......... .......... .......... .......... .......... 46% 99.4M 14s 123650K .......... .......... .......... .......... .......... 46% 10.4M 14s 123700K .......... .......... .......... .......... .......... 46% 121M 14s 123750K .......... .......... .......... .......... .......... 46% 153M 14s 123800K .......... .......... .......... .......... .......... 46% 86.9M 14s 123850K .......... .......... .......... .......... .......... 46% 10.1M 14s 123900K .......... .......... .......... .......... .......... 46% 116M 14s 123950K .......... .......... .......... .......... .......... 47% 107M 14s 124000K .......... .......... .......... .......... .......... 47% 10.1M 14s 124050K .......... .......... .......... .......... .......... 47% 122M 14s 124100K .......... .......... .......... .......... .......... 47% 120M 14s 124150K .......... .......... .......... .......... .......... 47% 9.14M 14s 124200K .......... .......... .......... .......... .......... 47% 147M 14s 124250K .......... .......... .......... .......... .......... 47% 146M 14s 124300K .......... .......... .......... .......... .......... 47% 9.90M 14s 124350K .......... .......... .......... .......... .......... 47% 154M 14s 124400K .......... .......... .......... .......... .......... 47% 196M 14s 124450K .......... .......... .......... .......... .......... 47% 161M 14s 124500K .......... .......... .......... .......... .......... 47% 9.12M 14s 124550K .......... .......... .......... .......... .......... 47% 174M 14s 124600K .......... .......... .......... .......... .......... 47% 116M 14s 124650K .......... .......... .......... .......... .......... 47% 7.18M 14s 124700K .......... .......... .......... .......... .......... 47% 168M 14s 124750K .......... .......... .......... .......... .......... 47% 173M 14s 124800K .......... .......... .......... .......... .......... 47% 106M 14s 124850K .......... .......... .......... .......... .......... 47% 6.40M 14s 124900K .......... .......... .......... .......... .......... 47% 81.5M 14s 124950K .......... .......... .......... .......... .......... 47% 119M 13s 125000K .......... .......... .......... .......... .......... 47% 7.79M 13s 125050K .......... .......... .......... .......... .......... 47% 170M 13s 125100K .......... .......... .......... .......... .......... 47% 120M 13s 125150K .......... .......... .......... .......... .......... 47% 8.64M 13s 125200K .......... .......... .......... .......... .......... 47% 115M 13s 125250K .......... .......... .......... .......... .......... 47% 149M 13s 125300K .......... .......... .......... .......... .......... 47% 211M 13s 125350K .......... .......... .......... .......... .......... 47% 8.28M 13s 125400K .......... .......... .......... .......... .......... 47% 107M 13s 125450K .......... .......... .......... .......... .......... 47% 88.6M 13s 125500K .......... .......... .......... .......... .......... 47% 8.29M 13s 125550K .......... .......... .......... .......... .......... 47% 289M 13s 125600K .......... .......... .......... .......... .......... 47% 142M 13s 125650K .......... .......... .......... .......... .......... 47% 118M 13s 125700K .......... .......... .......... .......... .......... 47% 7.44M 13s 125750K .......... .......... .......... .......... .......... 47% 109M 13s 125800K .......... .......... .......... .......... .......... 47% 168M 13s 125850K .......... .......... .......... .......... .......... 47% 8.56M 13s 125900K .......... .......... .......... .......... .......... 47% 122M 13s 125950K .......... .......... .......... .......... .......... 47% 308K 14s 126000K .......... .......... .......... .......... .......... 47% 126M 14s 126050K .......... .......... .......... .......... .......... 47% 140M 13s 126100K .......... .......... .......... .......... .......... 47% 207M 13s 126150K .......... .......... .......... .......... .......... 47% 205M 13s 126200K 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.......... .......... .......... 50% 230M 13s 134050K .......... .......... .......... .......... .......... 50% 3.65M 13s 134100K .......... .......... .......... .......... .......... 50% 43.6M 13s 134150K .......... .......... .......... .......... .......... 50% 198M 13s 134200K .......... .......... .......... .......... .......... 50% 203M 13s 134250K .......... .......... .......... .......... .......... 50% 3.96M 13s 134300K .......... .......... .......... .......... .......... 50% 98.0M 13s 134350K .......... .......... .......... .......... .......... 50% 127M 13s 134400K .......... .......... .......... .......... .......... 50% 121M 13s 134450K .......... .......... .......... .......... .......... 50% 3.66M 13s 134500K .......... .......... .......... .......... .......... 51% 113M 13s 134550K .......... .......... .......... .......... .......... 51% 319M 13s 134600K .......... .......... .......... .......... .......... 51% 254M 13s 134650K .......... .......... 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.......... .......... .......... 51% 2.82M 13s 135350K .......... .......... .......... .......... .......... 51% 95.4M 13s 135400K .......... .......... .......... .......... .......... 51% 162M 13s 135450K .......... .......... .......... .......... .......... 51% 106M 13s 135500K .......... .......... .......... .......... .......... 51% 3.01M 13s 135550K .......... .......... .......... .......... .......... 51% 158M 13s 135600K .......... .......... .......... .......... .......... 51% 70.7M 12s 135650K .......... .......... .......... .......... .......... 51% 156M 12s 135700K .......... .......... .......... .......... .......... 51% 3.47M 12s 135750K .......... .......... .......... .......... .......... 51% 198M 12s 135800K .......... .......... .......... .......... .......... 51% 233M 12s 135850K .......... .......... .......... .......... .......... 51% 99.2M 12s 135900K .......... .......... .......... .......... .......... 51% 210M 12s 135950K .......... .......... 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7s 179850K .......... .......... .......... .......... .......... 68% 20.5M 7s 179900K .......... .......... .......... .......... .......... 68% 21.1M 7s 179950K .......... .......... .......... .......... .......... 68% 189M 7s 180000K .......... .......... .......... .......... .......... 68% 20.0M 7s 180050K .......... .......... .......... .......... .......... 68% 243M 7s 180100K .......... .......... .......... .......... .......... 68% 16.9M 7s 180150K .......... .......... .......... .......... .......... 68% 17.8M 7s 180200K .......... .......... .......... .......... .......... 68% 111M 7s 180250K .......... .......... .......... .......... .......... 68% 17.3M 7s 180300K .......... .......... .......... .......... .......... 68% 18.7M 7s 180350K .......... .......... .......... .......... .......... 68% 148M 7s 180400K .......... .......... .......... .......... .......... 68% 17.7M 7s 180450K .......... .......... .......... .......... .......... 68% 16.2M 7s 180500K 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219950K .......... .......... .......... .......... .......... 83% 4.99M 4s 220000K .......... .......... .......... .......... .......... 83% 6.59M 4s 220050K .......... .......... .......... .......... .......... 83% 5.12M 4s 220100K .......... .......... .......... .......... .......... 83% 3.99M 4s 220150K .......... .......... .......... .......... .......... 83% 7.63M 4s 220200K .......... .......... .......... .......... .......... 83% 5.26M 4s 220250K .......... .......... .......... .......... .......... 83% 8.92M 4s 220300K .......... .......... .......... .......... .......... 83% 6.69M 4s 220350K .......... .......... .......... .......... .......... 83% 5.92M 4s 220400K .......... .......... .......... .......... .......... 83% 12.4M 4s 220450K .......... .......... .......... .......... .......... 83% 6.06M 4s 220500K .......... .......... .......... .......... .......... 83% 14.8M 4s 220550K .......... .......... .......... .......... .......... 83% 9.58M 4s 220600K 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.......... .......... .......... .......... 83% 8.66M 4s 221300K .......... .......... .......... .......... .......... 83% 6.60M 4s 221350K .......... .......... .......... .......... .......... 83% 7.35M 4s 221400K .......... .......... .......... .......... .......... 83% 7.95M 4s 221450K .......... .......... .......... .......... .......... 83% 11.5M 4s 221500K .......... .......... .......... .......... .......... 83% 6.35M 4s 221550K .......... .......... .......... .......... .......... 84% 6.44M 4s 221600K .......... .......... .......... .......... .......... 84% 12.2M 4s 221650K .......... .......... .......... .......... .......... 84% 6.98M 4s 221700K .......... .......... .......... .......... .......... 84% 14.1M 4s 221750K .......... .......... .......... .......... .......... 84% 5.63M 4s 221800K .......... .......... .......... .......... .......... 84% 14.4M 4s 221850K .......... .......... .......... .......... .......... 84% 13.5M 4s 221900K .......... .......... .......... .......... .......... 84% 13.3M 4s 221950K .......... .......... .......... .......... .......... 84% 7.99M 4s 222000K .......... .......... .......... .......... .......... 84% 15.6M 4s 222050K .......... .......... .......... .......... .......... 84% 17.0M 4s 222100K .......... .......... .......... .......... .......... 84% 15.3M 4s 222150K .......... .......... .......... .......... .......... 84% 12.9M 4s 222200K .......... .......... .......... .......... .......... 84% 13.2M 4s 222250K .......... .......... .......... .......... .......... 84% 14.1M 4s 222300K .......... .......... .......... .......... .......... 84% 5.97M 4s 222350K .......... .......... .......... .......... .......... 84% 12.0M 4s 222400K .......... .......... .......... .......... .......... 84% 12.8M 4s 222450K .......... .......... .......... .......... .......... 84% 9.71M 4s 222500K .......... .......... .......... .......... .......... 84% 8.14M 4s 222550K .......... .......... .......... .......... .......... 84% 7.40M 4s 222600K .......... .......... .......... .......... .......... 84% 6.39M 4s 222650K .......... .......... .......... .......... .......... 84% 6.49M 4s 222700K .......... .......... .......... .......... .......... 84% 4.23M 4s 222750K .......... .......... .......... .......... .......... 84% 132M 4s 222800K .......... .......... .......... .......... .......... 84% 6.24M 4s 222850K .......... .......... .......... .......... .......... 84% 5.39M 4s 222900K .......... .......... .......... .......... .......... 84% 8.19M 4s 222950K .......... .......... .......... .......... .......... 84% 5.05M 4s 223000K .......... .......... .......... .......... .......... 84% 7.16M 4s 223050K .......... .......... .......... .......... .......... 84% 11.3M 4s 223100K .......... .......... .......... .......... .......... 84% 6.83M 4s 223150K .......... .......... .......... .......... .......... 84% 6.22M 4s 223200K .......... .......... .......... .......... .......... 84% 1.27M 4s 223250K .......... .......... .......... .......... .......... 84% 10.0M 4s 223300K .......... .......... .......... .......... .......... 84% 17.1M 4s 223350K .......... .......... .......... .......... .......... 84% 12.3M 4s 223400K .......... .......... .......... .......... .......... 84% 11.7M 4s 223450K .......... .......... .......... .......... .......... 84% 10.2M 4s 223500K .......... .......... .......... .......... .......... 84% 20.2M 4s 223550K .......... .......... .......... .......... .......... 84% 8.10M 4s 223600K .......... .......... .......... .......... .......... 84% 15.4M 4s 223650K .......... .......... .......... .......... .......... 84% 17.4M 4s 223700K .......... .......... .......... .......... .......... 84% 4.64M 4s 223750K .......... .......... .......... .......... .......... 84% 38.4M 4s 223800K .......... .......... .......... .......... .......... 84% 13.3M 4s 223850K .......... .......... .......... .......... .......... 84% 7.45M 4s 223900K .......... .......... .......... .......... .......... 84% 9.83M 4s 223950K .......... .......... .......... .......... .......... 84% 7.33M 4s 224000K .......... .......... .......... .......... .......... 84% 8.99M 4s 224050K .......... .......... .......... .......... .......... 84% 8.80M 4s 224100K .......... .......... .......... .......... .......... 84% 7.62M 4s 224150K .......... .......... .......... .......... .......... 84% 4.44M 4s 224200K .......... .......... .......... .......... .......... 85% 18.7M 4s 224250K .......... .......... .......... .......... .......... 85% 8.88M 4s 224300K .......... .......... .......... .......... .......... 85% 9.28M 4s 224350K .......... .......... .......... .......... .......... 85% 8.84M 4s 224400K .......... .......... .......... .......... .......... 85% 8.52M 4s 224450K .......... .......... .......... .......... .......... 85% 8.45M 4s 224500K .......... .......... .......... .......... .......... 85% 8.37M 4s 224550K .......... .......... .......... .......... .......... 85% 5.60M 3s 224600K .......... .......... .......... .......... .......... 85% 16.5M 3s 224650K .......... .......... .......... .......... .......... 85% 12.6M 3s 224700K .......... .......... .......... .......... .......... 85% 7.25M 3s 224750K .......... .......... .......... .......... .......... 85% 16.7M 3s 224800K .......... .......... .......... .......... .......... 85% 12.3M 3s 224850K .......... .......... .......... .......... .......... 85% 7.49M 3s 224900K .......... .......... .......... .......... .......... 85% 14.4M 3s 224950K .......... .......... .......... .......... .......... 85% 7.20M 3s 225000K .......... .......... .......... .......... .......... 85% 11.5M 3s 225050K .......... .......... .......... .......... .......... 85% 9.01M 3s 225100K .......... .......... .......... .......... .......... 85% 17.6M 3s 225150K .......... .......... .......... .......... .......... 85% 7.45M 3s 225200K .......... .......... .......... .......... .......... 85% 19.0M 3s 225250K .......... .......... .......... .......... .......... 85% 10.2M 3s 225300K .......... .......... .......... .......... .......... 85% 8.17M 3s 225350K .......... .......... .......... .......... .......... 85% 15.0M 3s 225400K .......... .......... .......... .......... .......... 85% 9.10M 3s 225450K .......... .......... .......... .......... .......... 85% 9.95M 3s 225500K .......... .......... .......... .......... .......... 85% 13.0M 3s 225550K .......... .......... .......... .......... .......... 85% 11.8M 3s 225600K .......... .......... .......... .......... .......... 85% 6.34M 3s 225650K .......... .......... .......... .......... .......... 85% 18.1M 3s 225700K .......... .......... .......... .......... .......... 85% 11.9M 3s 225750K .......... .......... .......... .......... .......... 85% 11.5M 3s 225800K .......... .......... .......... .......... .......... 85% 19.7M 3s 225850K .......... .......... .......... .......... .......... 85% 9.36M 3s 225900K .......... .......... .......... .......... .......... 85% 9.28M 3s 225950K .......... .......... .......... .......... .......... 85% 18.3M 3s 226000K .......... .......... .......... .......... .......... 85% 10.3M 3s 226050K .......... .......... .......... .......... .......... 85% 6.88M 3s 226100K .......... .......... .......... .......... .......... 85% 12.7M 3s 226150K .......... .......... .......... .......... .......... 85% 11.9M 3s 226200K .......... .......... .......... .......... .......... 85% 6.72M 3s 226250K .......... .......... .......... .......... .......... 85% 15.8M 3s 226300K .......... .......... .......... .......... .......... 85% 2.65M 3s 226350K .......... .......... .......... .......... .......... 85% 7.24M 3s 226400K .......... .......... .......... .......... .......... 85% 105M 3s 226450K .......... .......... .......... .......... .......... 85% 10.4M 3s 226500K .......... .......... .......... .......... .......... 85% 19.2M 3s 226550K .......... .......... .......... .......... .......... 85% 21.7M 3s 226600K .......... .......... .......... .......... .......... 85% 8.37M 3s 226650K .......... .......... .......... .......... .......... 85% 10.8M 3s 226700K .......... .......... .......... .......... .......... 85% 9.09M 3s 226750K .......... .......... .......... .......... .......... 85% 16.2M 3s 226800K .......... .......... .......... .......... .......... 86% 15.8M 3s 226850K .......... .......... .......... .......... .......... 86% 7.30M 3s 226900K .......... .......... .......... .......... .......... 86% 9.28M 3s 226950K .......... .......... .......... .......... .......... 86% 6.06M 3s 227000K .......... .......... .......... .......... .......... 86% 19.7M 3s 227050K .......... .......... .......... .......... .......... 86% 7.62M 3s 227100K .......... .......... .......... .......... .......... 86% 9.52M 3s 227150K .......... .......... .......... .......... .......... 86% 14.2M 3s 227200K .......... .......... .......... .......... .......... 86% 6.58M 3s 227250K .......... .......... .......... .......... .......... 86% 11.1M 3s 227300K .......... .......... .......... .......... .......... 86% 6.16M 3s 227350K .......... .......... .......... .......... .......... 86% 4.05M 3s 227400K .......... .......... .......... .......... .......... 86% 13.7M 3s 227450K .......... .......... .......... .......... .......... 86% 7.17M 3s 227500K .......... .......... .......... .......... .......... 86% 16.6M 3s 227550K .......... .......... .......... .......... .......... 86% 8.40M 3s 227600K .......... .......... .......... .......... .......... 86% 8.57M 3s 227650K .......... .......... .......... .......... .......... 86% 8.30M 3s 227700K .......... .......... .......... .......... .......... 86% 8.62M 3s 227750K .......... .......... .......... .......... .......... 86% 17.5M 3s 227800K .......... .......... .......... .......... .......... 86% 15.8M 3s 227850K .......... .......... .......... .......... .......... 86% 5.38M 3s 227900K .......... .......... .......... .......... .......... 86% 13.0M 3s 227950K .......... .......... .......... .......... .......... 86% 6.46M 3s 228000K .......... .......... .......... .......... .......... 86% 10.6M 3s 228050K .......... .......... .......... .......... .......... 86% 12.3M 3s 228100K .......... .......... .......... .......... .......... 86% 5.51M 3s 228150K .......... .......... .......... .......... .......... 86% 9.99M 3s 228200K .......... .......... .......... .......... .......... 86% 11.1M 3s 228250K .......... .......... .......... .......... .......... 86% 13.1M 3s 228300K .......... .......... .......... .......... .......... 86% 13.7M 3s 228350K .......... .......... .......... .......... .......... 86% 11.6M 3s 228400K .......... .......... .......... .......... .......... 86% 6.56M 3s 228450K .......... .......... .......... .......... .......... 86% 7.27M 3s 228500K .......... .......... .......... .......... .......... 86% 77.4M 3s 228550K .......... .......... .......... .......... .......... 86% 8.73M 3s 228600K .......... .......... .......... .......... .......... 86% 14.5M 3s 228650K .......... .......... .......... .......... .......... 86% 8.56M 3s 228700K .......... .......... .......... .......... .......... 86% 17.4M 3s 228750K .......... .......... .......... .......... .......... 86% 8.07M 3s 228800K .......... .......... .......... .......... .......... 86% 15.7M 3s 228850K .......... .......... .......... .......... .......... 86% 7.03M 3s 228900K .......... .......... .......... .......... .......... 86% 5.16M 3s 228950K .......... .......... .......... .......... .......... 86% 85.4M 3s 229000K .......... .......... .......... .......... .......... 86% 17.3M 3s 229050K .......... .......... .......... .......... .......... 86% 16.6M 3s 229100K .......... .......... .......... .......... .......... 86% 9.38M 3s 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.......... .......... .......... .......... .......... 87% 7.17M 3s 229850K .......... .......... .......... .......... .......... 87% 11.7M 3s 229900K .......... .......... .......... .......... .......... 87% 12.4M 3s 229950K .......... .......... .......... .......... .......... 87% 12.8M 3s 230000K .......... .......... .......... .......... .......... 87% 9.18M 3s 230050K .......... .......... .......... .......... .......... 87% 9.63M 3s 230100K .......... .......... .......... .......... .......... 87% 7.30M 3s 230150K .......... .......... .......... .......... .......... 87% 8.78M 3s 230200K .......... .......... .......... .......... .......... 87% 7.14M 3s 230250K .......... .......... .......... .......... .......... 87% 7.19M 3s 230300K .......... .......... .......... .......... .......... 87% 8.77M 3s 230350K .......... .......... .......... .......... .......... 87% 9.50M 3s 230400K .......... .......... .......... .......... .......... 87% 6.78M 3s 230450K .......... .......... .......... .......... .......... 87% 7.63M 3s 230500K .......... .......... .......... .......... .......... 87% 7.86M 3s 230550K .......... .......... .......... .......... .......... 87% 8.23M 3s 230600K .......... .......... .......... .......... .......... 87% 8.48M 3s 230650K .......... .......... .......... .......... .......... 87% 7.70M 3s 230700K .......... .......... .......... .......... .......... 87% 5.47M 3s 230750K .......... .......... .......... .......... .......... 87% 7.81M 3s 230800K .......... .......... .......... .......... .......... 87% 4.14M 3s 230850K .......... .......... .......... .......... .......... 87% 7.42M 3s 230900K .......... .......... .......... .......... .......... 87% 6.47M 3s 230950K .......... .......... .......... .......... .......... 87% 7.28M 3s 231000K .......... .......... .......... .......... .......... 87% 4.49M 3s 231050K .......... .......... .......... .......... .......... 87% 5.93M 3s 231100K .......... .......... .......... .......... .......... 87% 7.15M 3s 231150K .......... .......... .......... .......... .......... 87% 6.11M 3s 231200K .......... .......... .......... .......... .......... 87% 6.86M 3s 231250K .......... .......... .......... .......... .......... 87% 11.4M 3s 231300K .......... .......... .......... .......... .......... 87% 6.47M 3s 231350K .......... .......... .......... .......... .......... 87% 5.61M 3s 231400K .......... .......... .......... .......... .......... 87% 10.9M 3s 231450K .......... .......... .......... .......... .......... 87% 5.57M 3s 231500K .......... .......... .......... .......... .......... 87% 10.5M 3s 231550K .......... .......... .......... .......... .......... 87% 4.43M 3s 231600K .......... .......... .......... .......... .......... 87% 143M 3s 231650K .......... .......... .......... .......... .......... 87% 7.86M 3s 231700K .......... .......... .......... .......... .......... 87% 7.04M 3s 231750K .......... .......... .......... 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.......... 88% 6.73M 3s 232450K .......... .......... .......... .......... .......... 88% 21.2M 3s 232500K .......... .......... .......... .......... .......... 88% 23.3M 3s 232550K .......... .......... .......... .......... .......... 88% 11.2M 3s 232600K .......... .......... .......... .......... .......... 88% 11.4M 3s 232650K .......... .......... .......... .......... .......... 88% 22.8M 3s 232700K .......... .......... .......... .......... .......... 88% 10.6M 3s 232750K .......... .......... .......... .......... .......... 88% 18.7M 3s 232800K .......... .......... .......... .......... .......... 88% 9.89M 3s 232850K .......... .......... .......... .......... .......... 88% 9.67M 3s 232900K .......... .......... .......... .......... .......... 88% 19.2M 3s 232950K .......... .......... .......... .......... .......... 88% 4.27M 3s 233000K .......... .......... .......... .......... .......... 88% 119M 3s 233050K .......... .......... .......... .......... .......... 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233750K .......... .......... .......... .......... .......... 88% 8.56M 3s 233800K .......... .......... .......... .......... .......... 88% 15.5M 3s 233850K .......... .......... .......... .......... .......... 88% 9.70M 3s 233900K .......... .......... .......... .......... .......... 88% 9.70M 3s 233950K .......... .......... .......... .......... .......... 88% 11.4M 3s 234000K .......... .......... .......... .......... .......... 88% 6.25M 3s 234050K .......... .......... .......... .......... .......... 88% 4.10M 3s 234100K .......... .......... .......... .......... .......... 88% 72.9M 3s 234150K .......... .......... .......... .......... .......... 88% 6.56M 3s 234200K .......... .......... .......... .......... .......... 88% 10.0M 3s 234250K .......... .......... .......... .......... .......... 88% 6.06M 3s 234300K .......... .......... .......... .......... .......... 88% 11.3M 3s 234350K .......... .......... .......... .......... .......... 88% 5.52M 3s 234400K .......... .......... .......... .......... .......... 88% 5.91M 3s 234450K .......... .......... .......... .......... .......... 88% 10.3M 3s 234500K .......... .......... .......... .......... .......... 88% 7.73M 3s 234550K .......... .......... .......... .......... .......... 88% 5.83M 3s 234600K .......... .......... .......... .......... .......... 88% 11.3M 3s 234650K .......... .......... .......... .......... .......... 88% 13.7M 3s 234700K .......... .......... .......... .......... .......... 88% 6.20M 3s 234750K .......... .......... .......... .......... .......... 89% 7.17M 3s 234800K .......... .......... .......... .......... .......... 89% 169M 3s 234850K .......... .......... .......... .......... .......... 89% 7.55M 3s 234900K .......... .......... .......... .......... .......... 89% 8.19M 3s 234950K .......... .......... .......... .......... .......... 89% 14.4M 3s 235000K .......... .......... .......... .......... .......... 89% 8.69M 3s 235050K .......... .......... .......... .......... .......... 89% 15.1M 3s 235100K .......... .......... .......... .......... .......... 89% 9.44M 3s 235150K .......... .......... .......... .......... .......... 89% 9.95M 3s 235200K .......... .......... .......... .......... .......... 89% 12.7M 3s 235250K .......... .......... .......... .......... .......... 89% 7.01M 3s 235300K .......... .......... .......... .......... .......... 89% 17.9M 3s 235350K .......... .......... .......... .......... .......... 89% 20.7M 3s 235400K .......... .......... .......... .......... .......... 89% 12.2M 3s 235450K .......... .......... .......... .......... .......... 89% 17.5M 3s 235500K .......... .......... .......... .......... .......... 89% 6.03M 3s 235550K .......... .......... .......... .......... .......... 89% 14.4M 3s 235600K .......... .......... .......... .......... .......... 89% 7.07M 3s 235650K .......... .......... .......... .......... .......... 89% 15.5M 3s 235700K .......... .......... .......... .......... .......... 89% 11.4M 3s 235750K .......... .......... .......... .......... .......... 89% 4.74M 3s 235800K .......... .......... .......... .......... .......... 89% 17.5M 3s 235850K .......... .......... .......... .......... .......... 89% 13.3M 3s 235900K .......... .......... .......... .......... .......... 89% 8.93M 3s 235950K .......... .......... .......... .......... .......... 89% 10.3M 2s 236000K .......... .......... .......... .......... .......... 89% 16.7M 2s 236050K .......... .......... .......... .......... .......... 89% 9.93M 2s 236100K .......... .......... .......... .......... .......... 89% 17.8M 2s 236150K .......... .......... .......... .......... .......... 89% 5.50M 2s 236200K .......... .......... .......... .......... .......... 89% 14.0M 2s 236250K .......... .......... .......... .......... .......... 89% 8.19M 2s 236300K .......... .......... .......... .......... .......... 89% 11.0M 2s 236350K .......... .......... .......... .......... .......... 89% 7.14M 2s 236400K .......... .......... .......... .......... .......... 89% 9.37M 2s 236450K .......... .......... .......... .......... .......... 89% 4.48M 2s 236500K .......... .......... .......... .......... .......... 89% 4.03M 2s 236550K .......... .......... .......... .......... .......... 89% 6.77M 2s 236600K .......... .......... .......... .......... .......... 89% 4.99M 2s 236650K .......... .......... .......... .......... .......... 89% 4.62M 2s 236700K .......... .......... .......... .......... .......... 89% 4.47M 2s 236750K .......... .......... .......... .......... .......... 89% 4.89M 2s 236800K .......... .......... .......... .......... .......... 89% 5.44M 2s 236850K .......... .......... .......... .......... .......... 89% 3.74M 2s 236900K .......... .......... .......... .......... .......... 89% 8.69M 2s 236950K .......... .......... .......... .......... .......... 89% 4.01M 2s 237000K .......... .......... .......... .......... .......... 89% 5.45M 2s 237050K .......... .......... .......... .......... .......... 89% 5.82M 2s 237100K .......... .......... .......... .......... .......... 89% 5.90M 2s 237150K .......... .......... .......... .......... .......... 89% 11.7M 2s 237200K .......... .......... .......... .......... .......... 89% 5.64M 2s 237250K .......... .......... .......... .......... .......... 89% 6.17M 2s 237300K .......... .......... .......... .......... .......... 89% 10.1M 2s 237350K .......... .......... .......... .......... .......... 90% 5.08M 2s 237400K .......... .......... .......... .......... .......... 90% 5.75M 2s 237450K .......... .......... .......... .......... .......... 90% 9.26M 2s 237500K .......... .......... .......... .......... .......... 90% 6.19M 2s 237550K .......... .......... .......... .......... .......... 90% 1.14M 2s 237600K .......... .......... .......... .......... .......... 90% 8.19M 2s 237650K .......... .......... .......... .......... .......... 90% 16.6M 2s 237700K .......... .......... .......... .......... .......... 90% 7.64M 2s 237750K .......... .......... .......... .......... .......... 90% 20.3M 2s 237800K .......... .......... .......... .......... .......... 90% 8.50M 2s 237850K .......... .......... .......... .......... .......... 90% 9.50M 2s 237900K .......... .......... .......... .......... .......... 90% 10.3M 2s 237950K .......... .......... .......... .......... .......... 90% 10.0M 2s 238000K .......... .......... .......... .......... .......... 90% 8.27M 2s 238050K .......... .......... .......... .......... .......... 90% 8.08M 2s 238100K .......... .......... .......... .......... .......... 90% 6.57M 2s 238150K .......... .......... .......... .......... .......... 90% 17.6M 2s 238200K .......... .......... .......... .......... .......... 90% 8.88M 2s 238250K .......... .......... .......... .......... .......... 90% 15.7M 2s 238300K .......... .......... .......... .......... .......... 90% 17.1M 2s 238350K .......... .......... .......... .......... .......... 90% 9.05M 2s 238400K .......... .......... .......... .......... .......... 90% 15.2M 2s 238450K .......... .......... .......... .......... .......... 90% 8.82M 2s 238500K .......... .......... .......... .......... .......... 90% 5.64M 2s 238550K .......... .......... .......... .......... .......... 90% 68.6M 2s 238600K .......... .......... .......... .......... .......... 90% 10.3M 2s 238650K .......... .......... .......... .......... .......... 90% 8.88M 2s 238700K .......... .......... .......... .......... .......... 90% 9.03M 2s 238750K .......... .......... .......... .......... .......... 90% 8.51M 2s 238800K .......... .......... .......... .......... .......... 90% 8.16M 2s 238850K .......... .......... .......... .......... .......... 90% 6.89M 2s 238900K .......... .......... .......... .......... .......... 90% 11.8M 2s 238950K .......... .......... .......... .......... .......... 90% 6.09M 2s 239000K .......... .......... .......... .......... .......... 90% 24.4M 2s 239050K .......... .......... .......... .......... .......... 90% 18.0M 2s 239100K .......... .......... .......... .......... .......... 90% 675K 2s 239150K .......... .......... .......... .......... .......... 90% 67.9M 2s 239200K .......... .......... .......... .......... .......... 90% 6.56M 2s 239250K .......... .......... .......... .......... .......... 90% 8.70M 2s 239300K .......... .......... .......... .......... .......... 90% 15.1M 2s 239350K .......... .......... .......... .......... .......... 90% 9.07M 2s 239400K .......... .......... .......... .......... .......... 90% 18.7M 2s 239450K .......... .......... .......... .......... .......... 90% 8.60M 2s 239500K .......... .......... .......... .......... .......... 90% 15.9M 2s 239550K .......... .......... .......... .......... .......... 90% 9.35M 2s 239600K .......... .......... .......... .......... .......... 90% 17.6M 2s 239650K .......... .......... .......... .......... .......... 90% 16.5M 2s 239700K .......... .......... .......... .......... .......... 90% 8.87M 2s 239750K .......... .......... .......... .......... .......... 90% 22.2M 2s 239800K .......... .......... .......... .......... .......... 90% 13.7M 2s 239850K .......... .......... .......... .......... .......... 90% 12.7M 2s 239900K .......... .......... .......... .......... .......... 90% 16.1M 2s 239950K .......... .......... .......... .......... .......... 90% 18.3M 2s 240000K .......... .......... .......... .......... .......... 91% 11.7M 2s 240050K .......... .......... .......... .......... .......... 91% 13.3M 2s 240100K .......... .......... .......... .......... .......... 91% 10.5M 2s 240150K .......... .......... .......... .......... .......... 91% 11.2M 2s 240200K .......... .......... .......... .......... .......... 91% 1.56M 2s 240250K .......... .......... .......... .......... .......... 91% 6.88M 2s 240300K .......... .......... .......... .......... .......... 91% 13.0M 2s 240350K .......... .......... .......... .......... .......... 91% 15.6M 2s 240400K .......... .......... .......... .......... .......... 91% 13.2M 2s 240450K .......... .......... .......... .......... .......... 91% 6.21M 2s 240500K .......... .......... .......... .......... .......... 91% 6.89M 2s 240550K .......... .......... .......... .......... .......... 91% 17.7M 2s 240600K .......... .......... .......... .......... .......... 91% 9.17M 2s 240650K .......... .......... .......... .......... .......... 91% 9.10M 2s 240700K .......... .......... .......... .......... .......... 91% 9.67M 2s 240750K .......... .......... .......... .......... .......... 91% 8.96M 2s 240800K .......... .......... .......... .......... .......... 91% 8.57M 2s 240850K .......... .......... .......... .......... .......... 91% 8.02M 2s 240900K .......... .......... .......... .......... .......... 91% 5.08M 2s 240950K .......... .......... .......... .......... .......... 91% 88.0M 2s 241000K .......... .......... .......... .......... .......... 91% 9.80M 2s 241050K .......... .......... .......... .......... .......... 91% 8.41M 2s 241100K .......... .......... .......... .......... .......... 91% 5.89M 2s 241150K .......... .......... .......... .......... .......... 91% 9.43M 2s 241200K .......... .......... .......... .......... .......... 91% 5.76M 2s 241250K .......... .......... .......... .......... .......... 91% 4.64M 2s 241300K .......... .......... .......... .......... .......... 91% 11.4M 2s 241350K .......... .......... .......... .......... .......... 91% 6.42M 2s 241400K .......... .......... .......... .......... .......... 91% 6.67M 2s 241450K .......... .......... .......... .......... .......... 91% 12.0M 2s 241500K .......... .......... .......... .......... .......... 91% 6.04M 2s 241550K .......... .......... .......... .......... .......... 91% 11.8M 2s 241600K .......... .......... .......... .......... .......... 91% 5.50M 2s 241650K .......... .......... .......... .......... .......... 91% 12.1M 2s 241700K .......... .......... .......... .......... .......... 91% 5.55M 2s 241750K .......... .......... .......... .......... .......... 91% 9.92M 2s 241800K .......... .......... .......... .......... .......... 91% 15.8M 2s 241850K .......... .......... .......... .......... .......... 91% 5.05M 2s 241900K .......... .......... .......... .......... .......... 91% 15.3M 2s 241950K .......... .......... .......... .......... .......... 91% 4.54M 2s 242000K .......... .......... .......... .......... .......... 91% 6.31M 2s 242050K .......... .......... .......... .......... .......... 91% 5.34M 2s 242100K .......... .......... .......... .......... .......... 91% 4.29M 2s 242150K .......... .......... .......... .......... .......... 91% 11.6M 2s 242200K .......... .......... .......... .......... .......... 91% 7.16M 2s 242250K .......... .......... .......... .......... .......... 91% 13.8M 2s 242300K .......... .......... .......... .......... .......... 91% 9.34M 2s 242350K .......... .......... .......... .......... .......... 91% 18.6M 2s 242400K .......... .......... .......... .......... .......... 91% 10.1M 2s 242450K .......... .......... .......... .......... .......... 91% 11.8M 2s 242500K .......... .......... .......... .......... .......... 91% 19.2M 2s 242550K .......... .......... .......... .......... .......... 91% 10.4M 2s 242600K .......... .......... .......... .......... .......... 91% 11.1M 2s 242650K .......... .......... .......... .......... .......... 92% 11.4M 2s 242700K .......... .......... .......... .......... .......... 92% 11.8M 2s 242750K .......... .......... .......... .......... .......... 92% 6.00M 2s 242800K .......... .......... .......... .......... .......... 92% 9.92M 2s 242850K .......... .......... .......... .......... .......... 92% 8.49M 2s 242900K .......... .......... .......... .......... .......... 92% 13.1M 2s 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.......... .......... .......... .......... .......... 92% 15.1M 2s 243650K .......... .......... .......... .......... .......... 92% 13.6M 2s 243700K .......... .......... .......... .......... .......... 92% 13.9M 2s 243750K .......... .......... .......... .......... .......... 92% 7.41M 2s 243800K .......... .......... .......... .......... .......... 92% 11.4M 2s 243850K .......... .......... .......... .......... .......... 92% 76.4M 2s 243900K .......... .......... .......... .......... .......... 92% 11.2M 2s 243950K .......... .......... .......... .......... .......... 92% 7.58M 2s 244000K .......... .......... .......... .......... .......... 92% 12.4M 2s 244050K .......... .......... .......... .......... .......... 92% 7.95M 2s 244100K .......... .......... .......... .......... .......... 92% 7.62M 2s 244150K .......... .......... .......... .......... .......... 92% 7.30M 2s 244200K .......... .......... .......... .......... .......... 92% 6.20M 2s 244250K .......... 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247550K .......... .......... .......... .......... .......... 93% 11.6M 1s 247600K .......... .......... .......... .......... .......... 93% 5.72M 1s 247650K .......... .......... .......... .......... .......... 93% 12.7M 1s 247700K .......... .......... .......... .......... .......... 93% 7.48M 1s 247750K .......... .......... .......... .......... .......... 93% 13.6M 1s 247800K .......... .......... .......... .......... .......... 93% 18.0M 1s 247850K .......... .......... .......... .......... .......... 93% 8.49M 1s 247900K .......... .......... .......... .......... .......... 94% 16.4M 1s 247950K .......... .......... .......... .......... .......... 94% 16.3M 1s 248000K .......... .......... .......... .......... .......... 94% 9.13M 1s 248050K .......... .......... .......... .......... .......... 94% 15.5M 1s 248100K .......... .......... .......... .......... .......... 94% 13.2M 1s 248150K .......... .......... .......... .......... .......... 94% 14.9M 1s 248200K .......... .......... .......... .......... .......... 94% 18.1M 1s 248250K .......... .......... .......... .......... .......... 94% 17.5M 1s 248300K .......... .......... .......... .......... .......... 94% 18.2M 1s 248350K .......... .......... .......... .......... .......... 94% 313K 1s 248400K .......... .......... .......... .......... .......... 94% 131M 1s 248450K .......... .......... .......... .......... .......... 94% 79.5M 1s 248500K .......... .......... .......... .......... .......... 94% 76.4M 1s 248550K .......... .......... .......... .......... .......... 94% 17.1M 1s 248600K .......... .......... .......... .......... .......... 94% 14.0M 1s 248650K .......... .......... .......... .......... .......... 94% 10.8M 1s 248700K .......... .......... .......... .......... .......... 94% 8.70M 1s 248750K .......... .......... .......... .......... .......... 94% 12.3M 1s 248800K .......... .......... .......... .......... .......... 94% 12.2M 1s 248850K .......... .......... .......... .......... .......... 94% 10.8M 1s 248900K .......... .......... .......... .......... .......... 94% 12.1M 1s 248950K .......... .......... .......... .......... .......... 94% 12.8M 1s 249000K .......... .......... .......... .......... .......... 94% 13.4M 1s 249050K .......... .......... .......... .......... .......... 94% 15.2M 1s 249100K .......... .......... .......... .......... .......... 94% 6.81M 1s 249150K .......... .......... .......... .......... .......... 94% 86.6M 1s 249200K .......... .......... .......... .......... .......... 94% 23.4M 1s 249250K .......... .......... .......... .......... .......... 94% 16.4M 1s 249300K .......... .......... .......... .......... .......... 94% 17.9M 1s 249350K .......... .......... .......... .......... .......... 94% 14.3M 1s 249400K .......... .......... .......... .......... .......... 94% 10.5M 1s 249450K .......... .......... .......... .......... .......... 94% 16.4M 1s 249500K .......... .......... .......... .......... .......... 94% 12.0M 1s 249550K .......... .......... .......... .......... .......... 94% 9.56M 1s 249600K .......... .......... .......... .......... .......... 94% 18.2M 1s 249650K .......... .......... .......... .......... .......... 94% 9.33M 1s 249700K .......... .......... .......... .......... .......... 94% 7.17M 1s 249750K .......... .......... .......... .......... .......... 94% 16.1M 1s 249800K .......... .......... .......... .......... .......... 94% 14.2M 1s 249850K .......... .......... .......... .......... .......... 94% 6.46M 1s 249900K .......... .......... .......... .......... .......... 94% 11.6M 1s 249950K .......... .......... .......... .......... .......... 94% 10.0M 1s 250000K .......... .......... .......... .......... .......... 94% 9.04M 1s 250050K .......... .......... .......... .......... .......... 94% 7.53M 1s 250100K .......... .......... .......... .......... .......... 94% 4.25M 1s 250150K .......... .......... .......... .......... .......... 94% 4.08M 1s 250200K .......... .......... .......... .......... .......... 94% 173M 1s 250250K .......... .......... .......... .......... .......... 94% 7.19M 1s 250300K .......... .......... .......... .......... .......... 94% 12.5M 1s 250350K .......... .......... .......... .......... .......... 94% 3.90M 1s 250400K .......... .......... .......... .......... .......... 94% 6.29M 1s 250450K .......... .......... .......... .......... .......... 94% 11.3M 1s 250500K .......... .......... .......... .......... .......... 94% 9.34M 1s 250550K .......... .......... .......... .......... .......... 95% 13.5M 1s 250600K .......... .......... .......... .......... .......... 95% 9.02M 1s 250650K .......... .......... .......... .......... .......... 95% 9.02M 1s 250700K .......... .......... .......... .......... .......... 95% 7.94M 1s 250750K .......... .......... .......... .......... .......... 95% 6.76M 1s 250800K .......... .......... .......... .......... .......... 95% 7.52M 1s 250850K .......... .......... .......... .......... .......... 95% 15.2M 1s 250900K .......... .......... .......... .......... .......... 95% 11.3M 1s 250950K .......... .......... .......... .......... .......... 95% 4.06M 1s 251000K .......... .......... .......... .......... .......... 95% 10.7M 1s 251050K .......... .......... .......... .......... .......... 95% 16.8M 1s 251100K .......... .......... .......... .......... .......... 95% 5.47M 1s 251150K .......... .......... .......... .......... .......... 95% 5.77M 1s 251200K .......... .......... .......... .......... .......... 95% 6.87M 1s 251250K .......... .......... .......... .......... .......... 95% 11.8M 1s 251300K .......... .......... .......... .......... .......... 95% 6.67M 1s 251350K .......... .......... .......... .......... .......... 95% 14.8M 1s 251400K .......... .......... .......... .......... .......... 95% 8.73M 1s 251450K .......... .......... .......... .......... .......... 95% 7.35M 1s 251500K .......... .......... .......... .......... .......... 95% 13.4M 1s 251550K .......... .......... .......... .......... .......... 95% 7.43M 1s 251600K .......... .......... .......... .......... .......... 95% 7.59M 1s 251650K .......... .......... .......... .......... .......... 95% 7.37M 1s 251700K .......... .......... .......... .......... .......... 95% 6.73M 1s 251750K .......... .......... .......... .......... .......... 95% 7.40M 1s 251800K .......... .......... .......... .......... .......... 95% 7.32M 1s 251850K .......... .......... .......... .......... .......... 95% 4.47M 1s 251900K .......... .......... .......... .......... .......... 95% 11.8M 1s 251950K .......... .......... .......... .......... .......... 95% 12.1M 1s 252000K .......... .......... .......... .......... .......... 95% 9.14M 1s 252050K .......... .......... .......... .......... .......... 95% 12.2M 1s 252100K .......... .......... .......... .......... .......... 95% 8.79M 1s 252150K .......... .......... .......... .......... .......... 95% 7.27M 1s 252200K .......... .......... .......... .......... .......... 95% 4.53M 1s 252250K .......... .......... .......... .......... .......... 95% 5.01M 1s 252300K .......... .......... .......... .......... .......... 95% 20.6M 1s 252350K .......... .......... .......... .......... .......... 95% 7.75M 1s 252400K .......... .......... .......... .......... .......... 95% 8.92M 1s 252450K .......... .......... .......... .......... .......... 95% 6.74M 1s 252500K .......... .......... .......... .......... .......... 95% 6.32M 1s 252550K .......... .......... .......... .......... .......... 95% 9.73M 1s 252600K .......... .......... .......... .......... .......... 95% 5.32M 1s 252650K .......... .......... .......... .......... .......... 95% 13.2M 1s 252700K .......... .......... .......... .......... .......... 95% 7.52M 1s 252750K .......... .......... .......... .......... .......... 95% 11.2M 1s 252800K .......... .......... .......... .......... .......... 95% 9.04M 1s 252850K .......... .......... .......... .......... .......... 95% 8.03M 1s 252900K .......... .......... .......... .......... .......... 95% 8.74M 1s 252950K .......... .......... .......... .......... .......... 95% 6.16M 1s 253000K .......... .......... .......... .......... .......... 95% 11.1M 1s 253050K .......... .......... .......... .......... .......... 95% 16.1M 1s 253100K .......... .......... .......... .......... .......... 95% 10.5M 1s 253150K .......... .......... .......... .......... .......... 95% 19.9M 1s 253200K .......... .......... .......... .......... .......... 96% 11.1M 1s 253250K .......... .......... .......... .......... .......... 96% 9.32M 1s 253300K .......... .......... .......... .......... .......... 96% 19.8M 1s 253350K .......... .......... .......... .......... .......... 96% 9.39M 1s 253400K .......... .......... .......... .......... .......... 96% 10.1M 1s 253450K .......... .......... .......... .......... .......... 96% 8.03M 1s 253500K .......... .......... .......... .......... .......... 96% 20.1M 1s 253550K .......... .......... .......... .......... .......... 96% 17.8M 1s 253600K .......... .......... .......... .......... .......... 96% 8.76M 1s 253650K .......... .......... .......... .......... .......... 96% 11.4M 1s 253700K .......... .......... .......... .......... .......... 96% 10.8M 1s 253750K .......... .......... .......... .......... .......... 96% 9.54M 1s 253800K .......... .......... .......... .......... .......... 96% 11.6M 1s 253850K .......... .......... .......... .......... .......... 96% 9.15M 1s 253900K .......... .......... .......... .......... .......... 96% 9.20M 1s 253950K .......... .......... .......... .......... .......... 96% 7.84M 1s 254000K .......... .......... .......... .......... .......... 96% 11.2M 1s 254050K .......... .......... .......... .......... .......... 96% 21.8M 1s 254100K .......... .......... .......... .......... .......... 96% 7.22M 1s 254150K .......... .......... .......... .......... .......... 96% 20.1M 1s 254200K .......... .......... .......... .......... .......... 96% 4.24M 1s 254250K .......... .......... .......... .......... .......... 96% 12.7M 1s 254300K .......... .......... .......... .......... .......... 96% 6.05M 1s 254350K .......... .......... .......... .......... .......... 96% 4.75M 1s 254400K .......... .......... .......... .......... .......... 96% 5.81M 1s 254450K .......... .......... .......... .......... .......... 96% 3.45M 1s 254500K .......... .......... .......... .......... .......... 96% 14.4M 1s 254550K .......... .......... .......... .......... .......... 96% 7.00M 1s 254600K .......... .......... .......... .......... .......... 96% 4.67M 1s 254650K .......... .......... .......... .......... .......... 96% 6.57M 1s 254700K .......... .......... .......... .......... .......... 96% 4.16M 1s 254750K .......... .......... .......... 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97% 31.2M 1s 256100K .......... .......... .......... .......... .......... 97% 13.2M 1s 256150K .......... .......... .......... .......... .......... 97% 7.22M 1s 256200K .......... .......... .......... .......... .......... 97% 12.0M 1s 256250K .......... .......... .......... .......... .......... 97% 10.6M 1s 256300K .......... .......... .......... .......... .......... 97% 9.01M 1s 256350K .......... .......... .......... .......... .......... 97% 6.84M 1s 256400K .......... .......... .......... .......... .......... 97% 13.9M 1s 256450K .......... .......... .......... .......... .......... 97% 9.90M 1s 256500K .......... .......... .......... .......... .......... 97% 13.0M 1s 256550K .......... .......... .......... .......... .......... 97% 17.9M 1s 256600K .......... .......... .......... .......... .......... 97% 19.7M 1s 256650K .......... .......... .......... .......... .......... 97% 17.1M 1s 256700K .......... .......... .......... .......... .......... 97% 17.5M 1s 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.......... .......... .......... .......... 97% 126M 1s 258100K .......... .......... .......... .......... .......... 97% 7.88M 1s 258150K .......... .......... .......... .......... .......... 97% 26.0M 1s 258200K .......... .......... .......... .......... .......... 97% 9.47M 1s 258250K .......... .......... .......... .......... .......... 97% 10.2M 1s 258300K .......... .......... .......... .......... .......... 97% 11.1M 1s 258350K .......... .......... .......... .......... .......... 97% 12.1M 0s 258400K .......... .......... .......... .......... .......... 97% 9.39M 0s 258450K .......... .......... .......... .......... .......... 98% 5.41M 0s 258500K .......... .......... .......... .......... .......... 98% 17.5M 0s 258550K .......... .......... .......... .......... .......... 98% 22.1M 0s 258600K .......... .......... .......... .......... .......... 98% 13.2M 0s 258650K .......... .......... .......... .......... .......... 98% 11.5M 0s 258700K .......... .......... 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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 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 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 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 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../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include \ -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_8_Harrier.c \ -o ./su2_8_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_8_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 (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:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:169]] ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)" ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:176]] ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)" ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:183]] iend must not be less than ibeg when evaluating "slice(e3,4,-1)" ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:384]] index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:402]] index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:418]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:434]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:442]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:450]] column index must be between 1 and 3 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:458]] column index must be between 1 and 3 --> catching signal -262 (illegal_pmtr_index) ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:1914]] signal 1 thrown by user --> catching signal 1 (UNKNOWN) ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions.csm:1924]] vertex and base must be different --> catching signal -225 (illegal_value) ==> serveESP completed successfully with no verification data real 0m0.934s user 0m0.028s sys 0m0.013s + 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 0m0.234s user 0m0.282s sys 0m0.031s + 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 0m2.318s user 0m3.356s sys 0m0.476s + 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 0m0.469s user 0m0.536s sys 0m0.035s + 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 0m0.367s user 0m0.554s sys 0m0.036s + 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 0m0.437s user 0m0.636s sys 0m0.028s + 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 0m3.485s user 0m4.669s sys 0m0.320s + 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 0m26.144s user 0m41.669s sys 0m1.469s + 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 0m0.519s user 0m0.707s sys 0m0.028s + 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 0m33.967s user 0m56.961s sys 0m5.611s + 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 0m0.271s user 0m0.198s sys 0m0.028s + 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 0m0.409s user 0m0.654s sys 0m0.014s + 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 0m0.121s user 0m0.168s sys 0m0.012s + 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 0m0.304s user 0m0.365s 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 2.159s 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 0m7.357s user 0m11.147s sys 0m0.323s ++ 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 41.227s 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 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1086 2174 AFLR2 IG : Nodes, Faces = 1087 2176 AFLR2 IG : Nodes, Faces = 1321 2644 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1421 2844 AFLR2 IG : Nodes, Faces = 1521 3044 AFLR2 IG : Nodes, Faces = 1621 3244 AFLR2 IG : Nodes, Faces = 1721 3444 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1821 3644 AFLR2 IG : Nodes, Faces = 1921 3844 AFLR2 IG : Nodes, Faces = 2021 4044 AFLR2 IG : Nodes, Faces = 2121 4244 AFLR2 IG : Nodes, Faces = 2221 4444 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.008 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4280 6316 AFLR2 GG : Nodes, Faces = 6142 10040 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9457 16670 AFLR2 GG : Nodes, Faces = 10755 19266 AFLR2 GG : Nodes, Faces = 11958 21672 AFLR2 GG : Nodes, Faces = 13085 23926 AFLR2 GG : Nodes, Faces = 14138 26032 AFLR2 GG : Nodes, Faces = 15126 28008 AFLR2 GG : Nodes, Faces = 16046 29848 AFLR2 GG : Nodes, Faces = 16885 31526 AFLR2 GG : Nodes, Faces = 17661 33078 AFLR2 GG : Nodes, Faces = 18384 34524 AFLR2 GG : Nodes, Faces = 19043 35842 AFLR2 GG : Nodes, Faces = 19652 37060 AFLR2 GG : Nodes, Faces = 20219 38194 AFLR2 GG : Nodes, Faces = 20752 39260 AFLR2 GG : Nodes, Faces = 21255 40266 AFLR2 GG : Nodes, Faces = 21709 41174 AFLR2 GG : Nodes, Faces = 22137 42030 AFLR2 GG : Nodes, Faces = 22527 42810 AFLR2 GG : Nodes, Faces = 22881 43518 AFLR2 GG : Nodes, Faces = 23170 44096 AFLR2 GG : Nodes, Faces = 23413 44582 AFLR2 GG : Nodes, Faces = 23626 45008 AFLR2 GG : Nodes, Faces = 23816 45388 AFLR2 GG : Nodes, Faces = 23971 45698 AFLR2 GG : Nodes, Faces = 24067 45890 AFLR2 GG : Nodes, Faces = 24162 46080 AFLR2 GG : Nodes, Faces = 24254 46264 AFLR2 GG : Nodes, Faces = 24329 46414 AFLR2 GG : Nodes, Faces = 24383 46522 AFLR2 GG : Nodes, Faces = 24422 46600 AFLR2 GG : Nodes, Faces = 24441 46638 AFLR2 GG : Nodes, Faces = 24449 46654 AFLR2 GG : Nodes, Faces = 24450 46656 AFLR2 : CPU Time = 0.064 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 24450 46656 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 24450 Number of elements = 48900 Number of tris = 46656 Number of quad = 0 Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 850 1702 AFLR2 IG : Nodes, Faces = 851 1704 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 1301 2604 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1401 2804 AFLR2 IG : Nodes, Faces = 1501 3004 AFLR2 IG : Nodes, Faces = 1601 3204 AFLR2 IG : Nodes, Faces = 1701 3404 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1801 3604 AFLR2 IG : Nodes, Faces = 1901 3804 AFLR2 IG : Nodes, Faces = 2001 4004 AFLR2 IG : Nodes, Faces = 2101 4204 AFLR2 IG : Nodes, Faces = 2201 4404 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.010 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4121 6018 AFLR2 GG : Nodes, Faces = 5676 9128 AFLR2 GG : Nodes, Faces = 6930 11636 AFLR2 GG : Nodes, Faces = 8008 13792 AFLR2 GG : Nodes, Faces = 8945 15666 AFLR2 GG : Nodes, Faces = 9742 17260 AFLR2 GG : Nodes, Faces = 10427 18630 AFLR2 GG : Nodes, Faces = 11007 19790 AFLR2 GG : Nodes, Faces = 11514 20804 AFLR2 GG : Nodes, Faces = 11940 21656 AFLR2 GG : Nodes, Faces = 12314 22404 AFLR2 GG : Nodes, Faces = 12630 23036 AFLR2 GG : Nodes, Faces = 12902 23580 AFLR2 GG : Nodes, Faces = 13117 24010 AFLR2 GG : Nodes, Faces = 13293 24362 AFLR2 GG : Nodes, Faces = 13417 24610 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 13581 24938 AFLR2 GG : Nodes, Faces = 13623 25022 AFLR2 GG : Nodes, Faces = 13649 25074 AFLR2 GG : Nodes, Faces = 13660 25096 AFLR2 GG : Nodes, Faces = 13664 25104 AFLR2 : CPU Time = 0.036 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 13664 25104 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 13664 Number of elements = 27328 Number of tris = 25104 Number of quad = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1086 2174 AFLR2 IG : Nodes, Faces = 1087 2176 AFLR2 IG : Nodes, Faces = 1321 2644 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1421 2844 AFLR2 IG : Nodes, Faces = 1521 3044 AFLR2 IG : Nodes, Faces = 1621 3244 AFLR2 IG : Nodes, Faces = 1721 3444 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1821 3644 AFLR2 IG : Nodes, Faces = 1921 3844 AFLR2 IG : Nodes, Faces = 2021 4044 AFLR2 IG : Nodes, Faces = 2121 4244 AFLR2 IG : Nodes, Faces = 2221 4444 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.009 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4280 6316 AFLR2 GG : Nodes, Faces = 6142 10040 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9457 16670 AFLR2 GG : Nodes, Faces = 10755 19266 AFLR2 GG : Nodes, Faces = 11958 21672 AFLR2 GG : Nodes, Faces = 13085 23926 AFLR2 GG : Nodes, Faces = 14138 26032 AFLR2 GG : Nodes, Faces = 15126 28008 AFLR2 GG : Nodes, Faces = 16046 29848 AFLR2 GG : Nodes, Faces = 16885 31526 AFLR2 GG : Nodes, Faces = 17661 33078 AFLR2 GG : Nodes, Faces = 18384 34524 AFLR2 GG : Nodes, Faces = 19043 35842 AFLR2 GG : Nodes, Faces = 19652 37060 AFLR2 GG : Nodes, Faces = 20219 38194 AFLR2 GG : Nodes, Faces = 20752 39260 AFLR2 GG : Nodes, Faces = 21255 40266 AFLR2 GG : Nodes, Faces = 21709 41174 AFLR2 GG : Nodes, Faces = 22137 42030 AFLR2 GG : Nodes, Faces = 22527 42810 AFLR2 GG : Nodes, Faces = 22881 43518 AFLR2 GG : Nodes, Faces = 23170 44096 AFLR2 GG : Nodes, Faces = 23413 44582 AFLR2 GG : Nodes, Faces = 23626 45008 AFLR2 GG : Nodes, Faces = 23816 45388 AFLR2 GG : Nodes, Faces = 23971 45698 AFLR2 GG : Nodes, Faces = 24067 45890 AFLR2 GG : Nodes, Faces = 24162 46080 AFLR2 GG : Nodes, Faces = 24254 46264 AFLR2 GG : Nodes, Faces = 24329 46414 AFLR2 GG : Nodes, Faces = 24383 46522 AFLR2 GG : Nodes, Faces = 24422 46600 AFLR2 GG : Nodes, Faces = 24441 46638 AFLR2 GG : Nodes, Faces = 24449 46654 AFLR2 GG : Nodes, Faces = 24450 46656 AFLR2 : CPU Time = 0.074 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 24450 46656 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 24450 Number of elements = 48900 Number of tris = 46656 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 850 1702 AFLR2 IG : Nodes, Faces = 851 1704 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 1301 2604 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1401 2804 AFLR2 IG : Nodes, Faces = 1501 3004 AFLR2 IG : Nodes, Faces = 1601 3204 AFLR2 IG : Nodes, Faces = 1701 3404 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1801 3604 AFLR2 IG : Nodes, Faces = 1901 3804 AFLR2 IG : Nodes, Faces = 2001 4004 AFLR2 IG : Nodes, Faces = 2101 4204 AFLR2 IG : Nodes, Faces = 2201 4404 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.008 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4121 6018 AFLR2 GG : Nodes, Faces = 5676 9128 AFLR2 GG : Nodes, Faces = 6930 11636 AFLR2 GG : Nodes, Faces = 8008 13792 AFLR2 GG : Nodes, Faces = 8945 15666 AFLR2 GG : Nodes, Faces = 9742 17260 AFLR2 GG : Nodes, Faces = 10427 18630 AFLR2 GG : Nodes, Faces = 11007 19790 AFLR2 GG : Nodes, Faces = 11514 20804 AFLR2 GG : Nodes, Faces = 11940 21656 AFLR2 GG : Nodes, Faces = 12314 22404 AFLR2 GG : Nodes, Faces = 12630 23036 AFLR2 GG : Nodes, Faces = 12902 23580 AFLR2 GG : Nodes, Faces = 13117 24010 AFLR2 GG : Nodes, Faces = 13293 24362 AFLR2 GG : Nodes, Faces = 13417 24610 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 13581 24938 AFLR2 GG : Nodes, Faces = 13623 25022 AFLR2 GG : Nodes, Faces = 13649 25074 AFLR2 GG : Nodes, Faces = 13660 25096 AFLR2 GG : Nodes, Faces = 13664 25104 AFLR2 : CPU Time = 0.032 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 13664 25104 AFLR2 : CPU Time = 0.003 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 13664 Number of elements = 27328 Number of tris = 25104 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 ok test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1086 2174 AFLR2 IG : Nodes, Faces = 1087 2176 AFLR2 IG : Nodes, Faces = 1321 2644 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1421 2844 AFLR2 IG : Nodes, Faces = 1521 3044 AFLR2 IG : Nodes, Faces = 1621 3244 AFLR2 IG : Nodes, Faces = 1721 3444 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1821 3644 AFLR2 IG : Nodes, Faces = 1921 3844 AFLR2 IG : Nodes, Faces = 2021 4044 AFLR2 IG : Nodes, Faces = 2121 4244 AFLR2 IG : Nodes, Faces = 2221 4444 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.012 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4280 6316 AFLR2 GG : Nodes, Faces = 6142 10040 AFLR2 GG : Nodes, Faces = 7878 13512 AFLR2 GG : Nodes, Faces = 9457 16670 AFLR2 GG : Nodes, Faces = 10755 19266 AFLR2 GG : Nodes, Faces = 11958 21672 AFLR2 GG : Nodes, Faces = 13085 23926 AFLR2 GG : Nodes, Faces = 14138 26032 AFLR2 GG : Nodes, Faces = 15126 28008 AFLR2 GG : Nodes, Faces = 16046 29848 AFLR2 GG : Nodes, Faces = 16885 31526 AFLR2 GG : Nodes, Faces = 17661 33078 AFLR2 GG : Nodes, Faces = 18384 34524 AFLR2 GG : Nodes, Faces = 19043 35842 AFLR2 GG : Nodes, Faces = 19652 37060 AFLR2 GG : Nodes, Faces = 20219 38194 AFLR2 GG : Nodes, Faces = 20752 39260 AFLR2 GG : Nodes, Faces = 21255 40266 AFLR2 GG : Nodes, Faces = 21709 41174 AFLR2 GG : Nodes, Faces = 22137 42030 AFLR2 GG : Nodes, Faces = 22527 42810 AFLR2 GG : Nodes, Faces = 22881 43518 AFLR2 GG : Nodes, Faces = 23170 44096 AFLR2 GG : Nodes, Faces = 23413 44582 AFLR2 GG : Nodes, Faces = 23626 45008 AFLR2 GG : Nodes, Faces = 23816 45388 AFLR2 GG : Nodes, Faces = 23971 45698 AFLR2 GG : Nodes, Faces = 24067 45890 AFLR2 GG : Nodes, Faces = 24162 46080 AFLR2 GG : Nodes, Faces = 24254 46264 AFLR2 GG : Nodes, Faces = 24329 46414 AFLR2 GG : Nodes, Faces = 24383 46522 AFLR2 GG : Nodes, Faces = 24422 46600 AFLR2 GG : Nodes, Faces = 24441 46638 AFLR2 GG : Nodes, Faces = 24449 46654 AFLR2 GG : Nodes, Faces = 24450 46656 AFLR2 : CPU Time = 0.091 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 24450 46656 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 24450 Number of elements = 48900 Number of tris = 46656 Number of quad = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 48 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 10 22 AFLR2 IG : Nodes, Faces = 20 42 AFLR2 IG : Nodes, Faces = 30 62 AFLR2 IG : Nodes, Faces = 38 78 AFLR2 IG : Nodes, Faces = 39 80 AFLR2 IG : Nodes, Faces = 40 82 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 98 AFLR2 IG : Nodes, Faces = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 48 48 AFLR2 GG : Nodes, Faces = 88 128 AFLR2 GG : Nodes, Faces = 106 164 AFLR2 GG : Nodes, Faces = 120 192 AFLR2 GG : Nodes, Faces = 132 216 AFLR2 GG : Nodes, Faces = 143 238 AFLR2 GG : Nodes, Faces = 154 260 AFLR2 GG : Nodes, Faces = 165 282 AFLR2 GG : Nodes, Faces = 174 300 AFLR2 GG : Nodes, Faces = 181 314 AFLR2 GG : Nodes, Faces = 183 318 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 183 318 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 183 Number of elements = 366 Number of tris = 318 Number of quad = 0 ok test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM 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 GG : Nodes, Faces = 344 344 AFLR2 GG : Nodes, Faces = 680 1016 AFLR2 GG : Nodes, Faces = 1009 1674 AFLR2 GG : Nodes, Faces = 1333 2322 AFLR2 GG : Nodes, Faces = 1650 2956 AFLR2 GG : Nodes, Faces = 1957 3570 AFLR2 GG : Nodes, Faces = 2258 4172 AFLR2 GG : Nodes, Faces = 2548 4752 AFLR2 GG : Nodes, Faces = 2831 5318 AFLR2 GG : Nodes, Faces = 3102 5860 AFLR2 GG : Nodes, Faces = 3364 6384 AFLR2 GG : Nodes, Faces = 3614 6884 AFLR2 GG : Nodes, Faces = 3830 7316 AFLR2 GG : Nodes, Faces = 4037 7730 AFLR2 GG : Nodes, Faces = 4229 8114 AFLR2 GG : Nodes, Faces = 4415 8486 AFLR2 GG : Nodes, Faces = 4594 8844 AFLR2 GG : Nodes, Faces = 4763 9182 AFLR2 GG : Nodes, Faces = 4926 9508 AFLR2 GG : Nodes, Faces = 5086 9828 AFLR2 GG : Nodes, Faces = 5239 10134 AFLR2 GG : Nodes, Faces = 5385 10426 AFLR2 GG : Nodes, Faces = 5529 10714 AFLR2 GG : Nodes, Faces = 5669 10994 AFLR2 GG : Nodes, Faces = 5812 11280 AFLR2 GG : Nodes, Faces = 5943 11542 AFLR2 GG : Nodes, Faces = 6070 11796 AFLR2 GG : Nodes, Faces = 6189 12034 AFLR2 GG : Nodes, Faces = 6307 12270 AFLR2 GG : Nodes, Faces = 6415 12486 AFLR2 GG : Nodes, Faces = 6510 12676 AFLR2 GG : Nodes, Faces = 6595 12846 AFLR2 GG : Nodes, Faces = 6665 12986 AFLR2 GG : Nodes, Faces = 6727 13110 AFLR2 GG : Nodes, Faces = 6772 13200 AFLR2 GG : Nodes, Faces = 6806 13268 AFLR2 GG : Nodes, Faces = 6831 13318 AFLR2 GG : Nodes, Faces = 6850 13356 AFLR2 GG : Nodes, Faces = 6864 13384 AFLR2 GG : Nodes, Faces = 6872 13400 AFLR2 GG : Nodes, Faces = 6875 13406 AFLR2 GG : Nodes, Faces = 6876 13408 AFLR2 : CPU Time = 0.016 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6876 13408 AFLR2 : CPU Time = 0.002 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6876 Number of elements = 13752 Number of tris = 13408 Number of quad = 0 Writing TECPLOT file: pyCAPS_aflr2_Tri.dat .... Finished writing TECPLOT file Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 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 = 0.031 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 = 0.010 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 Writing TECPLOT file: pyCAPS_aflr2_Quad.dat .... Finished writing TECPLOT file EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! ok test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM 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 = 0.023 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 = 0.011 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 Writing TECPLOT file: pyCAPS_aflr2_Test.dat .... Finished writing TECPLOT file EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! ok test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.9 AFLR4 : Version Date 08/14/23 @ 12:27AM AFLR4 : Compile OS Darwin 22.5.0 x86_64 AFLR4 : Compile Date 08/14/23 @ 01:13PM 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 = 10456 Number of elements = 58612 Number of triangles = 6352 Number of quadrilatarals = 0 Number of tetrahedrals = 52260 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 = 88489 Number of elements = 497438 Number of triangles = 51750 Number of quadrilatarals = 0 Number of tetrahedrals = 445688 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing AFLR3 file .... Finished writing AFLR3 file ok test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.9 AFLR4 : Version Date 08/14/23 @ 12:27AM AFLR4 : Compile OS Darwin 22.5.0 x86_64 AFLR4 : Compile Date 08/14/23 @ 01:13PM 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 = 17481 Number of elements = 99569 Number of triangles = 8306 Number of quadrilatarals = 0 Number of tetrahedrals = 91263 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2592 Number of elements = 13823 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11065 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5478 Number of elements = 30452 Number of triangles = 3656 Number of quadrilatarals = 0 Number of tetrahedrals = 26796 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 29525 Number of elements = 170763 Number of triangles = 7670 Number of quadrilatarals = 0 Number of tetrahedrals = 163093 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22768 Number of elements = 132033 Number of triangles = 6118 Number of quadrilatarals = 0 Number of tetrahedrals = 125915 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 29525 Number of elements = 170763 Number of triangles = 7670 Number of quadrilatarals = 0 Number of tetrahedrals = 163093 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22768 Number of elements = 132033 Number of triangles = 6118 Number of quadrilatarals = 0 Number of tetrahedrals = 125915 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 29525 Number of elements = 170763 Number of triangles = 7670 Number of quadrilatarals = 0 Number of tetrahedrals = 163093 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22768 Number of elements = 132033 Number of triangles = 6118 Number of quadrilatarals = 0 Number of tetrahedrals = 125915 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file ok test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 29525 Number of elements = 170763 Number of triangles = 7670 Number of quadrilatarals = 0 Number of tetrahedrals = 163093 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22768 Number of elements = 132033 Number of triangles = 6118 Number of quadrilatarals = 0 Number of tetrahedrals = 125915 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file ok test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 39476 Number of elements = 227846 Number of triangles = 12424 Number of quadrilatarals = 0 Number of tetrahedrals = 215422 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 46131 Number of elements = 267176 Number of triangles = 12406 Number of quadrilatarals = 0 Number of tetrahedrals = 254770 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 39476 Number of elements = 227828 Number of triangles = 12406 Number of quadrilatarals = 0 Number of tetrahedrals = 215422 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file ok test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value ok test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - trailingEdge Done getting mesh sizing parameters ok test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value ok test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value ok test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 1 Number of node elements = 1 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 45 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 3 Surface 2: Number of points found for aero-spline = 6 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 8 automatic connections were made for capsConnect Rib_Root (node id 1) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG 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) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG 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 (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Wing1, index = 1 Name = trailingEdge, index = 2 Writing FAST file .... Finished writing FAST file Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value ok test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 10ED54E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 10ED54E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 700008A86000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 700008A86000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value ok test_box (test_egadsTess.TestEGADS.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_egadsTess.TestEGADS.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 700008A86000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 700008A86000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 10ED54E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 10ED54E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) ok test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = nodeBody, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_setInput (test_egadsTess.TestEGADS.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value ok test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of node elements = 0 Number of line elements = 0 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: 0.182395 Creating surface mesh ... Surface mesh seconds: 0.039147 Recovering boundaries... Boundary recovery seconds: 0.126433 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.054614 Recovering Delaunayness... Delaunay recovery seconds: 0.059891 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: 2.33872 Smoothing vertices... Mesh smoothing seconds: 2.24004 Improving mesh... Mesh improvement seconds: 0.041706 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.017902 Total running seconds: 5.10178 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 node elements = 0 Number of line elements = 0 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of node elements = 0 Number of line elements = 0 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: 0.185491 Creating surface mesh ... Surface mesh seconds: 0.042491 Recovering boundaries... Boundary recovery seconds: 0.134751 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.059073 Recovering Delaunayness... Delaunay recovery seconds: 0.062885 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: 2.5252 Smoothing vertices... Mesh smoothing seconds: 2.36482 Improving mesh... Mesh improvement seconds: 0.054212 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.029743 Total running seconds: 5.45957 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_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.9 AFLR4 : Version Date 08/14/23 @ 12:27AM AFLR4 : Compile OS Darwin 22.5.0 x86_64 AFLR4 : Compile Date 08/14/23 @ 01:13PM 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 = 1015 Number of elements = 5450 Number of triangles = 918 Number of quadrilatarals = 0 Number of tetrahedrals = 4532 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 323 Number of elements = 1583 Number of triangles = 496 Number of quadrilatarals = 0 Number of tetrahedrals = 1087 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 975 Number of elements = 5204 Number of triangles = 874 Number of quadrilatarals = 0 Number of tetrahedrals = 4330 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 18938 Number of elements = 109528 Number of triangles = 5240 Number of quadrilatarals = 0 Number of tetrahedrals = 104288 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " ok test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1015 Number of elements = 5450 Number of triangles = 918 Number of quadrilatarals = 0 Number of tetrahedrals = 4532 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_inputs (test_refine.TestREFINE.test_inputs) ... ok test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 398 Number of elements = 1955 Number of triangles = 612 Number of quadrilatarals = 0 Number of tetrahedrals = 1343 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 ok test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 305 Number of elements = 1472 Number of triangles = 468 Number of quadrilatarals = 0 Number of tetrahedrals = 1004 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out ok test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.9 AFLR4 : Version Date 08/14/23 @ 12:27AM AFLR4 : Compile OS Darwin 22.5.0 x86_64 AFLR4 : Compile Date 08/14/23 @ 01:13PM 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 Sense Edges EGADS : 1 Yes 1 1 4 -3 -2 EGADS : 2 Yes 1 3 7 -6 -5 EGADS : 3 Yes 1 6 9 -1 -8 EGADS : 4 Yes 1 -4 -9 -7 EGADS : 5 Yes 1 -10 2 11 -12 EGADS : 6 Yes 1 -11 5 13 -14 EGADS : 7 Yes 1 -13 8 10 -15 EGADS : 8 Yes 1 12 14 15 EGADS : 9 Yes 1 16 19 -18 -17 EGADS : 10 Yes 1 18 22 -21 -20 EGADS : 11 Yes 1 21 24 -16 -23 EGADS : 12 Yes 1 -19 -24 -22 EGADS : 13 Yes 1 -25 17 26 -27 EGADS : 14 Yes 1 -26 20 28 -29 EGADS : 15 Yes 1 -28 23 25 -30 EGADS : 16 Yes 1 27 29 30 EGADS : 17 Yes 1 -31 -32 33 34 EGADS : 18 Yes 1 -35 -34 36 32 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 3 EGADS : 2 0 Yes 1 3 1 1 5 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 4 EGADS : 5 0 Yes 3 5 1 2 6 EGADS : 6 0 Yes 5 6 1 2 3 EGADS : 7 0 Yes 4 6 1 2 4 EGADS : 8 0 Yes 5 1 1 3 7 EGADS : 9 0 Yes 6 2 1 3 4 EGADS : 10 0 Yes 1 7 1 5 7 EGADS : 11 0 Yes 3 8 1 5 6 EGADS : 12 0 Yes 7 8 1 5 8 EGADS : 13 0 Yes 5 9 1 6 7 EGADS : 14 0 Yes 8 9 1 6 8 EGADS : 15 0 Yes 9 7 1 7 8 EGADS : 16 1 Yes 10 11 1 9 11 EGADS : 17 1 Yes 10 12 1 9 13 EGADS : 18 1 Yes 12 13 1 9 10 EGADS : 19 1 Yes 11 13 1 9 12 EGADS : 20 1 Yes 12 14 1 10 14 EGADS : 21 1 Yes 14 15 1 10 11 EGADS : 22 1 Yes 13 15 1 10 12 EGADS : 23 1 Yes 14 10 1 11 15 EGADS : 24 1 Yes 15 11 1 11 12 EGADS : 25 1 Yes 10 16 1 13 15 EGADS : 26 1 Yes 12 17 1 13 14 EGADS : 27 1 Yes 16 17 1 13 16 EGADS : 28 1 Yes 14 18 1 14 15 EGADS : 29 1 Yes 17 18 1 14 16 EGADS : 30 1 Yes 18 16 1 15 16 EGADS : 31 2 DEGEN 19 19 - 17 EGADS : 32 2 Yes 20 19 NA 17 18 EGADS : 33 2 DEGEN 20 20 - 17 EGADS : 34 2 Yes 20 19 NA 17 18 EGADS : 35 2 DEGEN 19 19 - 18 EGADS : 36 2 DEGEN 20 20 - 18 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 3.77246052 0 0.00459131419 EGADS : 2 Yes 5.90487498 7.07106781 0 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 4.0824829 7.07106781 0.123425948 EGADS : 5 Yes 3.77001182 0 0 EGADS : 6 Yes 5.90282524 7.07106781 0 EGADS : 7 Yes 5.90487498 0 0 EGADS : 8 Yes 4.0824829 0 0.123425948 EGADS : 9 Yes 5.90282524 0 0 EGADS : 10 Yes 11.5089842 0 0.00183652568 EGADS : 11 Yes 12.36195 2.82842712 0 EGADS : 12 Yes 10 0 0 EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791 EGADS : 14 Yes 11.5080047 0 0 EGADS : 15 Yes 12.3611301 2.82842712 0 EGADS : 16 Yes 12.36195 0 0 EGADS : 17 Yes 11.6329932 0 0.0493703791 EGADS : 18 Yes 12.3611301 0 0 EGADS : 19 Yes 0 0 80 EGADS : 20 Yes 0 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 160 AFLR4 : Min Bounding Box Length = 160 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 0.890888 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 15.6122 AFLR4 : Abs Min Surf Spacing = 0.00222722 AFLR4 : Min Surf Spacing = 0.00445444 AFLR4 : Max Surf Spacing = 0.0890888 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD AFLR4 : 2 CAD geometry 0 STD AFLR4 : 3 CAD geometry 0 STD AFLR4 : 4 CAD geometry 0 STD AFLR4 : 5 CAD geometry 0 STD AFLR4 : 6 CAD geometry 0 STD AFLR4 : 7 CAD geometry 0 STD AFLR4 : 8 CAD geometry 0 STD AFLR4 : 9 CAD geometry 0 STD AFLR4 : 10 CAD geometry 0 STD AFLR4 : 11 CAD geometry 0 STD AFLR4 : 12 CAD geometry 0 STD AFLR4 : 13 CAD geometry 0 STD AFLR4 : 14 CAD geometry 0 STD AFLR4 : 15 CAD geometry 0 STD AFLR4 : 16 CAD geometry 0 STD AFLR4 : 17 CAD geometry 0 FARFIELD AFLR4 : 18 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 12406 AFLR43 : Nodes = 6209 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.49 AFLR3 : Version Date 07/26/23 @ 12:32AM AFLR3 : Compile OS Darwin 22.5.0 x86_64 AFLR3 : Compile Date 07/26/23 @ 01:42PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 6209 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid UG3 : 7 Solid UG3 : 8 Solid UG3 : 9 Solid UG3 : 10 Solid UG3 : 11 Solid UG3 : 12 Solid UG3 : 13 Solid UG3 : 14 Solid UG3 : 15 Solid UG3 : 16 Solid UG3 : 17 FarField UG3 : 18 FarField AFLR3 : CPU Time = 0.018 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 6209 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1244 7652 AFLR3 IG : Nodes, Elements = 2488 16237 AFLR3 IG : Nodes, Elements = 3732 24911 AFLR3 IG : Nodes, Elements = 4976 33948 AFLR3 IG : Nodes, Elements = 6216 42984 AFLR3 IG : Nodes, Elements = 6216 42930 AFLR3 IG : Nodes, Elements = 6216 42934 AFLR3 IG : Nodes, Elements = 6216 42929 AFLR3 IG : Nodes, Elements = 6216 42934 AFLR3 IG : Nodes, Elements = 6216 42926 AFLR3 IG : Nodes, Elements = 6216 42927 AFLR3 IG : Nodes, Elements = 6209 25549 AFLR3 IG : Nodes, Elements = 6209 25566 AFLR3 IG : Nodes, Elements = 6209 20507 AFLR3 IG : Nodes, Elements = 6209 18413 AFLR3 : CPU Time = 0.212 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 6209 18413 AFLR3 GG : Nodes, Elements = 9086 27269 AFLR3 GG : Nodes, Elements = 9086 38929 AFLR3 GG : Nodes, Elements = 9086 36108 AFLR3 GG : Nodes, Elements = 9086 34647 AFLR3 GG : Nodes, Elements = 11683 42779 AFLR3 GG : Nodes, Elements = 11683 54137 AFLR3 GG : Nodes, Elements = 11683 50954 AFLR3 GG : Nodes, Elements = 11683 50011 AFLR3 GG : Nodes, Elements = 14417 58491 AFLR3 GG : Nodes, Elements = 14417 70525 AFLR3 GG : Nodes, Elements = 14417 67125 AFLR3 GG : Nodes, Elements = 14417 66290 AFLR3 GG : Nodes, Elements = 17349 75293 AFLR3 GG : Nodes, Elements = 17349 88048 AFLR3 GG : Nodes, Elements = 17349 84501 AFLR3 GG : Nodes, Elements = 17349 83647 AFLR3 GG : Nodes, Elements = 20424 93042 AFLR3 GG : Nodes, Elements = 20424 106231 AFLR3 GG : Nodes, Elements = 20424 102647 AFLR3 GG : Nodes, Elements = 20424 101784 AFLR3 GG : Nodes, Elements = 23663 111670 AFLR3 GG : Nodes, Elements = 23663 125600 AFLR3 GG : Nodes, Elements = 23663 121816 AFLR3 GG : Nodes, Elements = 23663 120935 AFLR3 GG : Nodes, Elements = 26946 130934 AFLR3 GG : Nodes, Elements = 26946 145172 AFLR3 GG : Nodes, Elements = 26946 141294 AFLR3 GG : Nodes, Elements = 26946 140472 AFLR3 GG : Nodes, Elements = 30337 150782 AFLR3 GG : Nodes, Elements = 30337 165197 AFLR3 GG : Nodes, Elements = 30337 161283 AFLR3 GG : Nodes, Elements = 30337 160483 AFLR3 GG : Nodes, Elements = 33865 171169 AFLR3 GG : Nodes, Elements = 33865 186241 AFLR3 GG : Nodes, Elements = 33865 182317 AFLR3 GG : Nodes, Elements = 33865 181518 AFLR3 GG : Nodes, Elements = 37465 192392 AFLR3 GG : Nodes, Elements = 37465 207646 AFLR3 GG : Nodes, Elements = 37465 203567 AFLR3 GG : Nodes, Elements = 37465 202753 AFLR3 GG : Nodes, Elements = 40997 213415 AFLR3 GG : Nodes, Elements = 40997 228468 AFLR3 GG : Nodes, Elements = 40997 224524 AFLR3 GG : Nodes, Elements = 40997 223769 AFLR3 GG : Nodes, Elements = 44447 234167 AFLR3 GG : Nodes, Elements = 44447 248845 AFLR3 GG : Nodes, Elements = 44447 244997 AFLR3 GG : Nodes, Elements = 44447 244235 AFLR3 GG : Nodes, Elements = 47895 254613 AFLR3 GG : Nodes, Elements = 47895 269085 AFLR3 GG : Nodes, Elements = 47895 265327 AFLR3 GG : Nodes, Elements = 47895 264716 AFLR3 GG : Nodes, Elements = 51100 274354 AFLR3 GG : Nodes, Elements = 51100 287914 AFLR3 GG : Nodes, Elements = 51100 284442 AFLR3 GG : Nodes, Elements = 51100 283898 AFLR3 GG : Nodes, Elements = 54128 293003 AFLR3 GG : Nodes, Elements = 54128 305860 AFLR3 GG : Nodes, Elements = 54128 302578 AFLR3 GG : Nodes, Elements = 54128 302052 AFLR3 GG : Nodes, Elements = 56983 310628 AFLR3 GG : Nodes, Elements = 56983 322623 AFLR3 GG : Nodes, Elements = 56983 319459 AFLR3 GG : Nodes, Elements = 56983 319004 AFLR3 GG : Nodes, Elements = 59608 326884 AFLR3 GG : Nodes, Elements = 59608 337928 AFLR3 GG : Nodes, Elements = 59608 335180 AFLR3 GG : Nodes, Elements = 59608 334753 AFLR3 GG : Nodes, Elements = 62032 342028 AFLR3 GG : Nodes, Elements = 62032 352195 AFLR3 GG : Nodes, Elements = 62032 349591 AFLR3 GG : Nodes, Elements = 62032 349253 AFLR3 GG : Nodes, Elements = 64192 355736 AFLR3 GG : Nodes, Elements = 64192 364758 AFLR3 GG : Nodes, Elements = 64192 362462 AFLR3 GG : Nodes, Elements = 64192 362170 AFLR3 GG : Nodes, Elements = 65914 367339 AFLR3 GG : Nodes, Elements = 65914 374690 AFLR3 GG : Nodes, Elements = 65914 372769 AFLR3 GG : Nodes, Elements = 65914 372558 AFLR3 GG : Nodes, Elements = 67290 376686 AFLR3 GG : Nodes, Elements = 67290 382441 AFLR3 GG : Nodes, Elements = 67290 380916 AFLR3 GG : Nodes, Elements = 67290 380767 AFLR3 GG : Nodes, Elements = 68317 383850 AFLR3 GG : Nodes, Elements = 68317 388164 AFLR3 GG : Nodes, Elements = 68317 387006 AFLR3 GG : Nodes, Elements = 68317 386911 AFLR3 GG : Nodes, Elements = 69043 389089 AFLR3 GG : Nodes, Elements = 69043 392189 AFLR3 GG : Nodes, Elements = 69043 391323 AFLR3 GG : Nodes, Elements = 69043 391254 AFLR3 GG : Nodes, Elements = 69489 392592 AFLR3 GG : Nodes, Elements = 69489 394593 AFLR3 GG : Nodes, Elements = 69489 393998 AFLR3 GG : Nodes, Elements = 69489 393954 AFLR3 GG : Nodes, Elements = 69728 394671 AFLR3 GG : Nodes, Elements = 69728 395675 AFLR3 GG : Nodes, Elements = 69728 395369 AFLR3 GG : Nodes, Elements = 69728 395351 AFLR3 GG : Nodes, Elements = 69824 395639 AFLR3 GG : Nodes, Elements = 69824 396052 AFLR3 GG : Nodes, Elements = 69824 395920 AFLR3 GG : Nodes, Elements = 69824 395916 AFLR3 GG : Nodes, Elements = 69841 395967 AFLR3 GG : Nodes, Elements = 69841 396045 AFLR3 GG : Nodes, Elements = 69841 396020 AFLR3 GG : Nodes, Elements = 69841 396018 AFLR3 GG : Nodes, Elements = 69847 396036 AFLR3 GG : Nodes, Elements = 69847 396061 AFLR3 GG : Nodes, Elements = 69847 396049 AFLR3 GG : Nodes, Elements = 69847 396051 AFLR3 GG : Nodes, Elements = 69848 396054 AFLR3 GG : Nodes, Elements = 69848 396056 AFLR3 GG : Nodes, Elements = 69878 396146 AFLR3 GG : Nodes, Elements = 69878 396251 AFLR3 GG : Nodes, Elements = 69878 396223 AFLR3 GG : Nodes, Elements = 69878 396216 AFLR3 GG : Nodes, Elements = 69886 396240 AFLR3 GG : Nodes, Elements = 69886 396271 AFLR3 GG : Nodes, Elements = 69886 396260 AFLR3 GG : Nodes, Elements = 69887 396263 AFLR3 GG : Nodes, Elements = 69887 396266 AFLR3 GG : Nodes, Elements = 69887 396265 AFLR3 : CPU Time = 5.070 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 69887 396265 AFLR3 QI : Nodes, Elements = 68520 388548 AFLR3 QI : Nodes, Elements = 68299 387286 AFLR3 QI : Nodes, Elements = 68282 387185 AFLR3 QI : Nodes, Elements = 68279 387169 AFLR3 QI : Nodes, Elements = 68279 391030 AFLR3 QI : Nodes, Elements = 68279 386948 AFLR3 QI : Nodes, Elements = 68279 386549 AFLR3 QI : Nodes, Elements = 68279 389222 AFLR3 QI : Nodes, Elements = 68279 386601 AFLR3 QI : Nodes, Elements = 68279 386517 AFLR3 QI : Nodes, Elements = 68279 387137 AFLR3 QI : Nodes, Elements = 68279 386368 AFLR3 QI : Nodes, Elements = 68279 386212 AFLR3 QI : Nodes, Elements = 68279 386567 AFLR3 QI : Nodes, Elements = 68279 386176 AFLR3 QI : Nodes, Elements = 68279 386086 AFLR3 QI : Nodes, Elements = 68279 386380 AFLR3 QI : Nodes, Elements = 68279 386073 AFLR3 QI : Nodes, Elements = 68279 386010 AFLR3 QI : Nodes, Elements = 68282 386024 AFLR3 QI : Nodes, Elements = 68282 386317 AFLR3 QI : Nodes, Elements = 68282 386046 AFLR3 QI : Nodes, Elements = 68282 386024 AFLR3 QI : Nodes, Elements = 68282 386286 AFLR3 QI : Nodes, Elements = 68282 386025 AFLR3 QI : Nodes, Elements = 68282 385985 AFLR3 : CPU Time = 1.692 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 68282 385985 AFLR3 QRG: Nodes, Elements = 68289 386023 AFLR3 QRG: Nodes, Elements = 68290 386026 AFLR3 QRG: Nodes, Elements = 68296 386059 AFLR3 QRG: Nodes, Elements = 68299 386075 AFLR3 QRG: Nodes, Elements = 68301 386089 AFLR3 QRG: Nodes, Elements = 68311 386144 AFLR3 : CPU Time = 0.044 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 386144 UG3 : Min, Max Ang = 1.234 175.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 55 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.11e+06 UG3 : No. Tet Elems = 386144 UG3 : Min Vol = 6.61e-10 UG3 : Average Vol = 5.46 UG3 : Total-Tet-Vol = 2.11e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 386144 UG3 : Min, Max Q = 0.0571 1 UG3 : Average Q = 0.891 UG3 : No. Q< 0.1 = 19 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 7.327 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 386144 UG3 : Min, Max Ang = 1.234 175.5 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 55 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.11e+06 UG3 : No. Tet Elems = 386144 UG3 : Min Vol = 6.61e-10 UG3 : Average Vol = 5.46 UG3 : Total-Tet-Vol = 2.11e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 386144 UG3 : Min, Max Q = 0.158 1 UG3 : Average Q = 0.853 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 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 = 68311 Number of elements = 398550 Number of triangles = 12406 Number of quadrilatarals = 0 Number of tetrahedrals = 386144 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Cardinal" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Raven" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Falcon" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions Boundary condition name - Wing1 ok test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X ok test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 68311 Number of elements = 398550 Number of triangles = 12406 Number of quadrilatarals = 0 Number of tetrahedrals = 386144 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Running SU2 1 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Running SU2 2 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 68311 Number of elements = 398550 Number of triangles = 12406 Number of quadrilatarals = 0 Number of tetrahedrals = 386144 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " CAPS Info: Hit last success -- going live! Running SU2 1 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " CAPS Info: Hit last success -- going live! Running SU2 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions ok test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 68311 Number of elements = 398550 Number of triangles = 12406 Number of quadrilatarals = 0 Number of tetrahedrals = 386144 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " ok test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " ok test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - 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:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 10ED54E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 10ED54E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 10ED54E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 10ED54E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 294 Number of elements = 584 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 584 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 488 Number of elements = 972 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 972 Number of quadrilateral elements = 0 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 4 (of 7) Number of nodes = 2048 Number of elements = 4096 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 7) Number of nodes = 152 Number of elements = 300 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 300 Number of quadrilateral elements = 0 Body 6 (of 7) Number of nodes = 624 Number of elements = 1248 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1248 Number of quadrilateral elements = 0 Body 7 (of 7) Number of nodes = 488 Number of elements = 972 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- 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 = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.002862 Creating surface mesh ... Surface mesh seconds: 0.000262 Recovering boundaries... Boundary recovery seconds: 0.032686 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000105 Recovering Delaunayness... Delaunay recovery seconds: 0.001201 Refining mesh... Refinement seconds: 0.000611 Smoothing vertices... Mesh smoothing seconds: 0.003343 Improving mesh... Mesh improvement seconds: 0.000157 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 5.5e-05 Total running seconds: 0.041372 Statistics: Input points: 98 Input facets: 192 Input segments: 288 Input holes: 0 Input regions: 0 Mesh points: 100 Mesh tetrahedra: 232 Mesh faces: 560 Mesh faces on exterior boundary: 192 Mesh faces on input facets: 192 Mesh edges on input segments: 288 Steiner points inside domain: 2 Done meshing using TetGen! Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.048911 Creating surface mesh ... Surface mesh seconds: 0.000775 Recovering boundaries... Boundary recovery seconds: 0.002996 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000539 Recovering Delaunayness... Delaunay recovery seconds: 0.004879 Refining mesh... Refinement seconds: 0.077491 Smoothing vertices... Mesh smoothing seconds: 0.026913 Improving mesh... Mesh improvement seconds: 0.000645 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.009581 Total running seconds: 0.172828 Statistics: Input points: 294 Input facets: 584 Input segments: 876 Input holes: 0 Input regions: 0 Mesh points: 342 Mesh tetrahedra: 1038 Mesh faces: 2368 Mesh faces on exterior boundary: 584 Mesh faces on input facets: 584 Mesh edges on input segments: 876 Steiner points inside domain: 48 Done meshing using TetGen! Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.164521 Creating surface mesh ... Surface mesh seconds: 0.001128 Recovering boundaries... Boundary recovery seconds: 0.007302 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001392 Recovering Delaunayness... Delaunay recovery seconds: 0.018316 Refining mesh... 650 insertions, added 167 points, 7377 tetrahedra in queue. 216 insertions, added 8 points, 5933 tetrahedra in queue. 288 insertions, added 11 points, 2914 tetrahedra in queue. 384 insertions, added 11 points, 392 tetrahedra in queue. 512 insertions, added 15 points, 93 tetrahedra in queue. Refinement seconds: 0.191102 Smoothing vertices... Mesh smoothing seconds: 0.076492 Improving mesh... Mesh improvement seconds: 0.001405 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000281 Total running seconds: 0.462065 Statistics: Input points: 488 Input facets: 972 Input segments: 1458 Input holes: 0 Input regions: 0 Mesh points: 706 Mesh tetrahedra: 2870 Mesh faces: 6226 Mesh faces on exterior boundary: 972 Mesh faces on input facets: 972 Mesh edges on input segments: 1458 Steiner points inside domain: 218 Done meshing using TetGen! Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.677675 Creating surface mesh ... Surface mesh seconds: 0.012225 Recovering boundaries... Boundary recovery seconds: 0.016344 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.012382 Recovering Delaunayness... Delaunay recovery seconds: 0.141506 Refining mesh... Refinement seconds: 0.468015 Smoothing vertices... Mesh smoothing seconds: 0.307196 Improving mesh... Mesh improvement seconds: 0.00666 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002205 Total running seconds: 1.64459 Statistics: Input points: 2048 Input facets: 4096 Input segments: 6144 Input holes: 0 Input regions: 0 Mesh points: 2904 Mesh tetrahedra: 11373 Mesh faces: 24794 Mesh faces on exterior boundary: 4096 Mesh faces on input facets: 4096 Mesh edges on input segments: 6144 Steiner points inside domain: 856 Done meshing using TetGen! Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.00056 Creating surface mesh ... Surface mesh seconds: 0.000379 Recovering boundaries... Boundary recovery seconds: 0.000422 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000141 Recovering Delaunayness... Delaunay recovery seconds: 0.000584 Refining mesh... 202 insertions, added 46 points, 0 tetrahedra in queue. Refinement seconds: 0.006879 Smoothing vertices... Mesh smoothing seconds: 0.00471 Improving mesh... Mesh improvement seconds: 0.000418 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000111 Total running seconds: 0.014276 Statistics: Input points: 152 Input facets: 300 Input segments: 450 Input holes: 0 Input regions: 0 Mesh points: 198 Mesh tetrahedra: 672 Mesh faces: 1494 Mesh faces on exterior boundary: 300 Mesh faces on input facets: 300 Mesh edges on input segments: 450 Steiner points inside domain: 46 Done meshing using TetGen! Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.063997 Creating surface mesh ... Surface mesh seconds: 0.001534 Recovering boundaries... Boundary recovery seconds: 0.00976 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001381 Recovering Delaunayness... Delaunay recovery seconds: 0.012917 Refining mesh... 831 insertions, added 215 points, 5504 tetrahedra in queue. Refinement seconds: 0.105485 Smoothing vertices... Mesh smoothing seconds: 0.067815 Improving mesh... Mesh improvement seconds: 0.001691 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000694 Total running seconds: 0.265421 Statistics: Input points: 624 Input facets: 1248 Input segments: 1872 Input holes: 0 Input regions: 0 Mesh points: 846 Mesh tetrahedra: 3169 Mesh faces: 6962 Mesh faces on exterior boundary: 1248 Mesh faces on input facets: 1248 Mesh edges on input segments: 1872 Steiner points inside domain: 222 Done meshing using TetGen! Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.044352 Creating surface mesh ... Surface mesh seconds: 0.001216 Recovering boundaries... Boundary recovery seconds: 0.051684 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000793 Suppressing Steiner points ... Steiner suppression seconds: 5e-06 Recovering Delaunayness... Delaunay recovery seconds: 0.06001 Refining mesh... Refinement seconds: 0.089405 Smoothing vertices... Mesh smoothing seconds: 0.059483 Improving mesh... Mesh improvement seconds: 0.001368 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000298 Total running seconds: 0.309113 Statistics: Input points: 488 Input facets: 972 Input segments: 1458 Input holes: 0 Input regions: 0 Mesh points: 672 Mesh tetrahedra: 2513 Mesh faces: 5512 Mesh faces on exterior boundary: 972 Mesh faces on input facets: 972 Mesh edges on input segments: 1458 Steiner points inside domain: 184 Done meshing using TetGen! Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 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 = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.00314 Creating surface mesh ... Surface mesh seconds: 0.000284 Recovering boundaries... Boundary recovery seconds: 0.001098 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 8e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.001017 Refining mesh... Refinement seconds: 0.000565 Smoothing vertices... Mesh smoothing seconds: 0.003409 Improving mesh... Mesh improvement seconds: 0.000163 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 5.4e-05 Total running seconds: 0.009865 Statistics: Input points: 98 Input facets: 192 Input segments: 288 Input holes: 0 Input regions: 1 Mesh points: 100 Mesh tetrahedra: 232 Mesh faces: 560 Mesh faces on exterior boundary: 192 Mesh faces on input facets: 192 Mesh edges on input segments: 288 Steiner points inside domain: 2 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.016386 Creating surface mesh ... Surface mesh seconds: 0.00076 Recovering boundaries... Boundary recovery seconds: 0.002824 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.000545 Recovering Delaunayness... Delaunay recovery seconds: 0.005053 Refining mesh... Refinement seconds: 0.027894 Smoothing vertices... Mesh smoothing seconds: 0.023977 Improving mesh... Mesh improvement seconds: 0.000566 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000152 Total running seconds: 0.078263 Statistics: Input points: 294 Input facets: 584 Input segments: 876 Input holes: 0 Input regions: 2 Mesh points: 342 Mesh tetrahedra: 1038 Mesh faces: 2368 Mesh faces on exterior boundary: 584 Mesh faces on input facets: 584 Mesh edges on input segments: 876 Steiner points inside domain: 48 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.086185 Creating surface mesh ... Surface mesh seconds: 0.001143 Recovering boundaries... Boundary recovery seconds: 0.012853 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001213 Recovering Delaunayness... Delaunay recovery seconds: 0.026354 Refining mesh... 650 insertions, added 167 points, 7377 tetrahedra in queue. 216 insertions, added 8 points, 5933 tetrahedra in queue. 288 insertions, added 11 points, 2914 tetrahedra in queue. 384 insertions, added 11 points, 392 tetrahedra in queue. 512 insertions, added 15 points, 93 tetrahedra in queue. Refinement seconds: 0.22294 Smoothing vertices... Mesh smoothing seconds: 0.115579 Improving mesh... Mesh improvement seconds: 0.001455 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000337 Total running seconds: 0.468181 Statistics: Input points: 488 Input facets: 972 Input segments: 1458 Input holes: 0 Input regions: 3 Mesh points: 706 Mesh tetrahedra: 2870 Mesh faces: 6226 Mesh faces on exterior boundary: 972 Mesh faces on input facets: 972 Mesh edges on input segments: 1458 Steiner points inside domain: 218 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.583759 Creating surface mesh ... Surface mesh seconds: 0.006415 Recovering boundaries... Boundary recovery seconds: 0.016293 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.006967 Recovering Delaunayness... Delaunay recovery seconds: 0.199191 Refining mesh... Refinement seconds: 0.657358 Smoothing vertices... Mesh smoothing seconds: 0.363172 Improving mesh... Mesh improvement seconds: 0.007033 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001623 Total running seconds: 1.84218 Statistics: Input points: 2048 Input facets: 4096 Input segments: 6144 Input holes: 0 Input regions: 4 Mesh points: 2912 Mesh tetrahedra: 11359 Mesh faces: 24766 Mesh faces on exterior boundary: 4096 Mesh faces on input facets: 4096 Mesh edges on input segments: 6144 Steiner points inside domain: 864 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.000851 Creating surface mesh ... Surface mesh seconds: 0.000412 Recovering boundaries... Boundary recovery seconds: 0.000453 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.000158 Recovering Delaunayness... Delaunay recovery seconds: 0.000594 Refining mesh... 202 insertions, added 46 points, 0 tetrahedra in queue. Refinement seconds: 0.006131 Smoothing vertices... Mesh smoothing seconds: 0.004847 Improving mesh... Mesh improvement seconds: 0.000326 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.0001 Total running seconds: 0.013926 Statistics: Input points: 152 Input facets: 300 Input segments: 450 Input holes: 0 Input regions: 5 Mesh points: 198 Mesh tetrahedra: 672 Mesh faces: 1494 Mesh faces on exterior boundary: 300 Mesh faces on input facets: 300 Mesh edges on input segments: 450 Steiner points inside domain: 46 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.054113 Creating surface mesh ... Surface mesh seconds: 0.001625 Recovering boundaries... Boundary recovery seconds: 0.005678 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Warning: The 5-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001319 Recovering Delaunayness... Delaunay recovery seconds: 0.007633 Refining mesh... 831 insertions, added 215 points, 5504 tetrahedra in queue. Refinement seconds: 0.080002 Smoothing vertices... Mesh smoothing seconds: 0.065902 Improving mesh... Mesh improvement seconds: 0.00182 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000415 Total running seconds: 0.218646 Statistics: Input points: 624 Input facets: 1248 Input segments: 1872 Input holes: 0 Input regions: 6 Mesh points: 846 Mesh tetrahedra: 3169 Mesh faces: 6962 Mesh faces on exterior boundary: 1248 Mesh faces on input facets: 1248 Mesh edges on input segments: 1872 Steiner points inside domain: 222 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.045793 Creating surface mesh ... Surface mesh seconds: 0.001321 Recovering boundaries... Boundary recovery seconds: 0.049825 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Warning: The 5-th region point lies outside the convex hull. Warning: The 6-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001057 Suppressing Steiner points ... Steiner suppression seconds: 3.3e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.05702 Refining mesh... Refinement seconds: 0.063346 Smoothing vertices... Mesh smoothing seconds: 0.043332 Improving mesh... Mesh improvement seconds: 0.001408 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000331 Total running seconds: 0.264092 Statistics: Input points: 488 Input facets: 972 Input segments: 1458 Input holes: 0 Input regions: 7 Mesh points: 673 Mesh tetrahedra: 2528 Mesh faces: 5542 Mesh faces on exterior boundary: 972 Mesh faces on input facets: 972 Mesh edges on input segments: 1458 Steiner points inside domain: 185 Done meshing using TetGen! Writing AFLR3 file .... Finished writing AFLR3 file ok test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 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! Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7173, elements - 14338 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing TECPLOT file: test.dat .... Finished writing TECPLOT file ok test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9601 Number of elements = 19194 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9601 Total number of elements = 19194 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 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 TECPLOT file: test.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 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 TECPLOT file: test.dat .... Finished writing TECPLOT file ok test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok ---------------------------------------------------------------------- Ran 137 tests in 627.371s 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 ================================================= + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'avl_PyTest.py test;' 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 0m2.521s user 0m1.100s sys 0m0.929s + 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 0m8.617s user 0m7.856s sys 0m0.740s + 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 0m6.680s user 0m5.347s sys 0m0.663s + 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 0m2.041s user 0m0.856s sys 0m0.381s + 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 0m1.273s user 0m0.860s sys 0m0.371s + 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 be in the x-y plane... attempting to rotate mesh through node swapping! Swapping z and y coordinates! Writing delaundo control file - delaundo.ctr Writing out *.pts file Reading delaundo mesh file - delaundoMesh.mesh Swapping y and z coordinates! Writing TECPLOT file: delaundoMesh.dat .... Finished writing TECPLOT file real 0m1.969s user 0m1.058s sys 0m0.586s + 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; + tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u egadsTess_PyTest.py -outLevel=0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Name = Wing, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting mesh sizing parameters Mesh sizing name - LeadingEdge Done getting mesh sizing parameters Getting surface mesh for body 1 (of 4) Getting surface mesh for body 2 (of 4) Getting surface mesh for body 3 (of 4) Getting surface mesh for body 4 (of 4) Body 1 (of 4) Number of nodes = 3793 Number of elements = 4001 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 4001 Body 2 (of 4) Number of nodes = 1 Number of elements = 1 Number of node elements = 1 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 3 (of 4) Number of nodes = 76 Number of elements = 55 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 55 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 4 (of 4) Number of nodes = 100 Number of elements = 73 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 73 ---------------------------- Total number of nodes = 3970 Total number of elements = 4130 Writing TECPLOT file: egadsTessMesh_Surf_0.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_1.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_2.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_3.dat .... Finished writing TECPLOT file real 0m19.165s user 0m31.883s sys 0m4.120s + 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 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM 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 = 0.034 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 = 0.011 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 Writing TECPLOT file: pyCAPS_AFLR2_Test.dat .... Finished writing TECPLOT file EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! real 0m1.810s user 0m1.372s sys 0m0.527s + 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 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat .... Finished writing TECPLOT file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.9 AFLR4 : Version Date 08/14/23 @ 12:27AM AFLR4 : Compile OS Darwin 22.5.0 x86_64 AFLR4 : Compile Date 08/14/23 @ 01:13PM 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: pyCAPS_AFLR4_AFLR3_VolMesh.dat .... Finished writing TECPLOT file real 0m20.782s user 0m18.661s sys 0m1.126s + 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 node elements = 0 Number of line elements = 0 Number of triangle elements = 4468 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 636 Number of elements = 1268 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1268 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 267 Number of elements = 530 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 530 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3139 Total number of elements = 6266 Writing TECPLOT file: egadsTessMesh_Surf_0.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_1.dat .... Finished writing TECPLOT file Writing TECPLOT file: egadsTessMesh_Surf_2.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 3139, elements - 6266 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.034576 Creating surface mesh ... Surface mesh seconds: 0.01084 Recovering boundaries... Boundary recovery seconds: 0.104103 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.014165 Suppressing Steiner points ... Steiner suppression seconds: 5.6e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.016196 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: 1.00999 Smoothing vertices... Mesh smoothing seconds: 0.797043 Improving mesh... Mesh improvement seconds: 0.018236 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00512 Total running seconds: 2.01091 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: pyCAPS_Tetgen_Test.dat .... Binary output is not currently supported for Tecplot output ..... switching to ASCII! Finished writing TECPLOT file real 0m9.568s user 0m9.311s sys 0m0.580s + 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 9.14.7 AFLR2 : Version Date 07/16/23 @ 01:42PM AFLR2 : Compile OS Darwin 22.5.0 x86_64 AFLR2 : Compile Date 07/25/23 @ 11:59AM 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 = 0.002 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 = 0.054 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 = 0.020 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 11153 Number of elements = 11885 Number of tris = 917 Number of quad = 10423 Writing TECPLOT file: pyCAPS_su2_aflr2.dat .... Finished writing TECPLOT file EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing SU2 file .... SU2 expects 2D meshes be in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Airfoil Boundary condition name - InFlow Boundary condition name - OutFlow Boundary condition name - TunnelWall Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.4. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_5. Surface(s) plotted in the output file: BC_5, BC_2. Input mesh file name: ../aflr2/aflr2.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat. Surface file name: surface_flow_pyCAPS_su2_aflr2. Volume file name: flow_pyCAPS_su2_aflr2. Restart file name: restart_flow_pyCAPS_su2_aflr2.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 11153 grid points. 11340 volume elements. 4 surface markers. 98 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_4). 399 boundary elements in index 3 (Marker = BC_5). 917 triangles. 10423 quadrilaterals. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 917 TRIANGLE volume elements. There has been a re-orientation of 10423 QUADRILATERAL volume elements. There has been a re-orientation of 73 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.878. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 49.3184| 90| | CV Face Area Aspect Ratio| 1.00035| 33.4982| | CV Sub-Volume Ratio| 1.00001| 7.89914| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11153| 1/1.00| 10| | 1| 2702| 1/4.13| 7.38309| | 2| 549| 1/4.92| 4.99198| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.06265 m. Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m. Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is NOT a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.2670e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.2595e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.2737e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.2730e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.2794e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.2754e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.2777e-01| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.2751e-01| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.2803e-01| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.2629e-01| -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 0m4.876s user 0m3.063s sys 0m1.013s + 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 0m1.134s user 0m0.724s sys 0m0.454s + 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 0m1.750s user 0m1.102s sys 0m0.615s + 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 node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 798 ---------------------------- Total number of nodes = 1159 Total number of elements = 798 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Constraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1159 Number of elements = 798 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 798 Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - Ribs_and_Spars No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Area 3.428666259747 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 0m7.149s user 0m10.510s sys 0m5.109s + 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 0m1.467s user 0m1.086s sys 0m0.242s + 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 0m44.919s user 0m2.522s sys 0m0.566s + 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 Apr 3 12:29 ASTRO.D01 -rw-r--r-- 1 jenkins staff 277K Apr 3 12:29 ASTRO.IDX -rwxr-xr-x 1 jenkins staff 131K Apr 3 12:29 ESPxddm -rwxr-xr-x 1 jenkins staff 229K Apr 3 12:29 Slugs -rwxr-xr-x 1 jenkins staff 102K Apr 3 12:29 TestFit -rwxr-xr-x 1 jenkins staff 1.8M Apr 3 12:29 avl -rwxr-xr-x 1 jenkins staff 50K Apr 3 12:29 cart3dTest -rwxr-xr-x 1 jenkins staff 50K Apr 3 12:28 egads2cart -rwxr-xr-x 1 jenkins staff 86K Apr 3 12:29 egads2cgt -rwxr-xr-x 1 jenkins staff 383K Apr 3 12:29 friction -rwxr-xr-x 1 jenkins staff 8.9M Apr 3 12:29 mastros.exe -rwxr-xr-x 1 jenkins staff 2.2M Apr 3 12:29 mses -rwxr-xr-x 1 jenkins staff 2.5M Apr 3 12:29 mset -rwxr-xr-x 1 jenkins staff 51K Apr 3 12:29 phaseUtil -rw-r--r-- 1 jenkins staff 1.6K Apr 3 12:31 pod.egads -rw-r--r-- 1 jenkins staff 0B Apr 3 12:31 port7681.jrnl -rwxr-xr-x 1 jenkins staff 1.2M Apr 3 12:29 pplot -rwxr-xr-x 1 jenkins staff 1.2M Apr 3 12:29 pxplot -rwxr-xr-x 1 jenkins staff 84K Apr 3 12:28 sensCSM -rwxr-xr-x 1 jenkins staff 224K Apr 3 12:28 serveCSM -rwxr-xr-x 1 jenkins staff 191K Apr 3 12:28 serveESP -rwxr-xr-x 1 jenkins staff 68K Apr 3 12:28 vCurvature -rwxr-xr-x 1 jenkins staff 51K Apr 3 12:28 vGeom -rwxr-xr-x 1 jenkins staff 52K Apr 3 12:28 vTess -rwxr-xr-x 1 jenkins staff 2.3M Apr 3 12:28 vTesstatic -rw-r--r-- 1 jenkins staff 195K Apr 3 12:31 wingMultiModel.bdf -rwxr-xr-x 1 jenkins staff 1.8M Apr 3 12:29 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 0m47.281s user 0m8.602s sys 0m0.653s ++ 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 0m8.725s user 0m10.301s sys 0m0.100s ++ 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 0m26.504s user 0m39.783s sys 0m0.293s ++ 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 0m28.407s user 0m42.223s sys 0m0.337s ++ 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 #702'. [Checks API] No suitable checks publisher found. [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] done Finished: SUCCESS