![[Jenkins]](/csi/static/a404d988/images/svgs/logo.svg){kind=logo}
Started by upstream project "ESP_Beta" build number 713 originally caused by: Started by remote host 18.18.33.14 Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on macys_VM in workspace /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64 Cleaning local Directory . Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-02T23:57:55.551 -0400' --quiet Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 2483 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP doesn't exist Cleaning local Directory JenkinsESP Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-02T23:57:55.551 -0400' --quiet Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 860 No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [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/jenkins10480681573753243813.sh + bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/ESP_Beta.sh + source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/ESP_Env.sh ++ export OCCTREF=7.8 ++ OCCTREF=7.8 ++ AFLR_VERSION=11.5.14 ++ SU2_VERSION=8.0.0 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.38.0 ++ export PYTHON_VERSION=3.11.9 ++ PYTHON_VERSION=3.11.9 ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ [[ macys_VM == \r\e\y\n\o\l\d\s ]] ++ [[ DARWIN64 == *\.\i\f\o\r\t ]] ++ '[' -f /opt/intel/oneapi/setvars.sh ']' ++ source /opt/intel/oneapi/setvars.sh ++ '[' -f /Users/jenkins/.bashrc ']' ++ export CAPS_OUTLEVEL=0 ++ CAPS_OUTLEVEL=0 ++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.8 != '' ]] ++ [[ '' != '' ]] ++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]] ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile +++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]] +++ . /usr/local/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/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/7.8/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14 ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-x86-64 ++ AFLR_ARCH=MacOSX-x86-64 ++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ export CART3D_ARCH=OSX64_ICC ++ CART3D_ARCH=OSX64_ICC ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/ESP/DARWIN64/bin ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/ESP/DARWIN64/bin/python ++ ln -s /usr/local/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python-config ++ ln -s /usr/local/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/DARWIN64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/data + virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv created virtual environment CPython3.11.5.final.0-64 in 4635ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.8/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==69.2.0, wheel==0.43.0 activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator + . /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/activate ++ '[' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/ESP_venv ++ '[' darwin20 = cygwin ']' ++ '[' darwin20 = msys ']' ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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-3.3-py3-none-any.whl.metadata (5.1 kB) Requirement already satisfied: numpy in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4) Collecting scipy (from openmdao) Using cached scipy-1.13.0-cp311-cp311-macosx_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-3.7-py3-none-any.whl.metadata (9.9 kB) Collecting urllib3<3,>=1.21.1 (from requests->openmdao) Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB) Collecting certifi>=2017.4.17 (from requests->openmdao) Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB) Using cached networkx-3.3-py3-none-any.whl (1.7 MB) Using cached packaging-24.0-py3-none-any.whl (53 kB) Using cached requests-2.31.0-py3-none-any.whl (62 kB) Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl (39.3 MB) Using cached certifi-2024.2.2-py3-none-any.whl (163 kB) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl (121 kB) Using cached idna-3.7-py3-none-any.whl (66 kB) Using cached urllib3-2.2.1-py3-none-any.whl (121 kB) Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.31.1 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/7.8/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/7.8/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/7.8/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/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.8.4-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-4.51.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl.metadata (6.4 kB) Requirement already satisfied: numpy>=1.21 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-3.8.4-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-4.51.0-cp311-cp311-macosx_10_9_x86_64.whl (2.3 MB) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl (68 kB) Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl (3.5 MB) Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB) Using cached six-1.16.0-py2.py3-none-any.whl (11 kB) Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.8.4 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0 + pip_install scipy + /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.0) Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4) + unset PYTHONINC + unset PYTHONLIB + unset UDUNITS2_XML_PATH + unset ESP_BLOC + unset ESP_ROOT + unset ESP_ARCH + unset AWAVE + unset AFLR + unset AFLR_ARCH + wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz --2024-05-03 00:35:03-- https://acdl.mit.edu/ESP/archive/ESPbeta.tgz Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14 Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected. HTTP request sent, awaiting response... 200 OK Length: 268501958 (256M) [application/x-gzip] Saving to: ‘ESPbeta.tgz’ 0K .......... .......... .......... .......... .......... 0% 7.06M 36s 50K .......... .......... .......... .......... .......... 0% 16.3M 26s 100K .......... .......... .......... .......... .......... 0% 94.6M 18s 150K .......... .......... .......... .......... .......... 0% 92.3M 14s 200K .......... .......... .......... .......... .......... 0% 21.7M 14s 250K .......... .......... .......... .......... .......... 0% 14.9M 14s 300K .......... .......... .......... .......... .......... 0% 148M 13s 350K .......... .......... .......... .......... .......... 0% 79.9M 11s 400K .......... .......... .......... .......... .......... 0% 80.7M 10s 450K .......... .......... .......... .......... .......... 0% 10.5M 12s 500K .......... .......... .......... .......... .......... 0% 103M 11s 550K .......... .......... .......... .......... .......... 0% 201M 10s 600K .......... .......... .......... .......... .......... 0% 177M 10s 650K .......... .......... .......... .......... .......... 0% 190M 9s 700K .......... .......... .......... .......... .......... 0% 6.47M 11s 750K .......... .......... .......... .......... .......... 0% 111M 10s 800K .......... .......... .......... .......... .......... 0% 157M 10s 850K .......... .......... .......... .......... .......... 0% 139M 9s 900K .......... .......... .......... .......... .......... 0% 121M 9s 950K .......... .......... .......... .......... .......... 0% 158M 9s 1000K .......... .......... .......... .......... .......... 0% 135M 8s 1050K .......... .......... .......... .......... .......... 0% 124M 8s 1100K .......... .......... .......... .......... .......... 0% 161M 8s 1150K .......... .......... .......... .......... .......... 0% 138M 8s 1200K .......... .......... .......... .......... .......... 0% 3.08M 11s 1250K .......... .......... .......... .......... .......... 0% 124M 10s 1300K .......... .......... .......... .......... .......... 0% 168M 10s 1350K .......... .......... .......... .......... .......... 0% 137M 10s 1400K .......... .......... .......... .......... .......... 0% 223M 9s 1450K .......... .......... .......... .......... .......... 0% 173M 9s 1500K .......... .......... .......... .......... .......... 0% 173M 9s 1550K .......... .......... .......... .......... .......... 0% 162M 9s 1600K .......... .......... .......... .......... .......... 0% 91.6M 8s 1650K .......... .......... .......... .......... .......... 0% 69.1M 8s 1700K .......... .......... .......... .......... .......... 0% 85.2M 8s 1750K .......... .......... .......... .......... .......... 0% 1.11M 14s 1800K .......... .......... .......... .......... .......... 0% 111M 14s 1850K .......... .......... .......... .......... .......... 0% 129M 14s 1900K .......... .......... .......... .......... .......... 0% 146M 13s 1950K .......... .......... .......... .......... .......... 0% 68.6M 13s 2000K .......... .......... .......... .......... .......... 0% 95.7M 13s 2050K .......... .......... .......... .......... .......... 0% 107M 13s 2100K .......... .......... .......... .......... .......... 0% 170M 12s 2150K .......... .......... .......... .......... .......... 0% 186M 12s 2200K .......... .......... .......... .......... .......... 0% 157M 12s 2250K .......... .......... .......... .......... .......... 0% 183M 12s 2300K .......... .......... .......... .......... .......... 0% 94.3M 11s 2350K .......... .......... .......... .......... .......... 0% 94.3M 11s 2400K .......... .......... .......... .......... .......... 0% 142M 11s 2450K .......... .......... .......... .......... .......... 0% 126M 11s 2500K .......... .......... .......... .......... .......... 0% 145M 11s 2550K .......... .......... .......... .......... .......... 0% 120M 10s 2600K .......... .......... .......... .......... .......... 1% 149M 10s 2650K .......... .......... .......... .......... .......... 1% 167M 10s 2700K .......... .......... .......... .......... .......... 1% 161M 10s 2750K .......... .......... .......... .......... .......... 1% 202M 10s 2800K .......... .......... .......... .......... .......... 1% 209M 10s 2850K .......... .......... .......... .......... .......... 1% 148M 10s 2900K .......... .......... .......... .......... .......... 1% 186M 9s 2950K .......... .......... .......... .......... .......... 1% 160M 9s 3000K .......... .......... .......... .......... .......... 1% 184M 9s 3050K .......... .......... .......... .......... .......... 1% 200M 9s 3100K .......... .......... .......... .......... .......... 1% 178M 9s 3150K .......... .......... .......... .......... .......... 1% 187M 9s 3200K .......... .......... .......... .......... .......... 1% 158M 9s 3250K .......... .......... .......... .......... .......... 1% 167M 9s 3300K .......... .......... .......... .......... .......... 1% 208M 8s 3350K .......... .......... .......... .......... .......... 1% 175M 8s 3400K .......... .......... .......... .......... .......... 1% 203M 8s 3450K .......... .......... .......... .......... .......... 1% 162M 8s 3500K .......... .......... .......... .......... .......... 1% 173M 8s 3550K .......... .......... .......... .......... .......... 1% 1.45M 10s 3600K .......... .......... .......... .......... .......... 1% 79.8M 10s 3650K .......... .......... .......... .......... .......... 1% 88.5M 10s 3700K .......... .......... .......... .......... .......... 1% 120M 10s 3750K .......... .......... .......... .......... .......... 1% 117M 10s 3800K .......... .......... .......... .......... .......... 1% 135M 10s 3850K .......... .......... .......... .......... .......... 1% 73.6M 10s 3900K .......... .......... .......... .......... .......... 1% 87.0M 10s 3950K .......... .......... .......... .......... .......... 1% 108M 10s 4000K .......... .......... .......... .......... .......... 1% 168M 9s 4050K .......... .......... .......... .......... .......... 1% 133M 9s 4100K .......... .......... .......... .......... .......... 1% 1.05M 12s 4150K .......... .......... .......... .......... .......... 1% 1001K 15s 4200K .......... .......... .......... .......... .......... 1% 82.3M 15s 4250K .......... .......... .......... .......... .......... 1% 119M 15s 4300K .......... .......... .......... .......... .......... 1% 200M 15s 4350K .......... .......... .......... .......... .......... 1% 140M 14s 4400K .......... .......... .......... .......... .......... 1% 194M 14s 4450K .......... .......... .......... .......... .......... 1% 141M 14s 4500K .......... .......... .......... .......... .......... 1% 220M 14s 4550K .......... .......... .......... .......... .......... 1% 224M 14s 4600K .......... .......... .......... .......... .......... 1% 190M 14s 4650K .......... .......... .......... .......... .......... 1% 233M 14s 4700K .......... .......... .......... .......... .......... 1% 196M 13s 4750K .......... .......... .......... .......... .......... 1% 227M 13s 4800K .......... .......... .......... .......... .......... 1% 234M 13s 4850K .......... .......... .......... .......... .......... 1% 191M 13s 4900K .......... .......... .......... .......... .......... 1% 228M 13s 4950K .......... .......... .......... .......... .......... 1% 193M 13s 5000K .......... .......... .......... .......... .......... 1% 205M 13s 5050K .......... .......... .......... .......... .......... 1% 117M 13s 5100K .......... .......... .......... .......... .......... 1% 56.6M 13s 5150K .......... .......... .......... .......... .......... 1% 73.8M 12s 5200K .......... .......... .......... .......... .......... 2% 130M 12s 5250K .......... .......... .......... .......... .......... 2% 203M 12s 5300K .......... .......... .......... .......... .......... 2% 172M 12s 5350K .......... .......... .......... .......... .......... 2% 126M 12s 5400K .......... .......... .......... .......... .......... 2% 111M 12s 5450K .......... .......... .......... .......... .......... 2% 131M 12s 5500K .......... .......... .......... .......... .......... 2% 210M 12s 5550K .......... .......... .......... .......... .......... 2% 168M 12s 5600K .......... .......... .......... .......... .......... 2% 187M 12s 5650K .......... .......... .......... .......... .......... 2% 146M 11s 5700K .......... .......... .......... .......... .......... 2% 66.8M 11s 5750K .......... .......... .......... .......... .......... 2% 139M 11s 5800K .......... .......... .......... .......... .......... 2% 105M 11s 5850K .......... .......... .......... .......... .......... 2% 81.7M 11s 5900K .......... .......... .......... .......... .......... 2% 5.62M 11s 5950K .......... .......... .......... .......... .......... 2% 185M 11s 6000K .......... .......... .......... .......... .......... 2% 220M 11s 6050K .......... .......... .......... .......... .......... 2% 223M 11s 6100K .......... .......... .......... .......... .......... 2% 135M 11s 6150K .......... .......... .......... .......... .......... 2% 181M 11s 6200K .......... .......... .......... .......... .......... 2% 198M 11s 6250K .......... .......... .......... .......... .......... 2% 201M 11s 6300K .......... .......... .......... .......... .......... 2% 235M 11s 6350K .......... .......... .......... .......... .......... 2% 198M 11s 6400K .......... .......... .......... .......... .......... 2% 227M 11s 6450K .......... .......... .......... .......... .......... 2% 203M 11s 6500K .......... .......... .......... .......... .......... 2% 189M 10s 6550K .......... .......... .......... .......... .......... 2% 225M 10s 6600K .......... .......... .......... .......... .......... 2% 194M 10s 6650K .......... .......... .......... .......... .......... 2% 198M 10s 6700K .......... .......... .......... .......... .......... 2% 197M 10s 6750K .......... .......... .......... .......... .......... 2% 230M 10s 6800K .......... .......... .......... .......... .......... 2% 238M 10s 6850K .......... .......... .......... .......... .......... 2% 184M 10s 6900K .......... .......... .......... .......... .......... 2% 225M 10s 6950K .......... .......... .......... .......... .......... 2% 174M 10s 7000K .......... .......... .......... .......... .......... 2% 217M 10s 7050K .......... .......... .......... .......... .......... 2% 157M 10s 7100K .......... .......... .......... .......... .......... 2% 151M 10s 7150K .......... .......... .......... .......... .......... 2% 217M 10s 7200K .......... .......... .......... .......... .......... 2% 168M 10s 7250K .......... .......... .......... .......... .......... 2% 216M 10s 7300K .......... .......... .......... .......... .......... 2% 168M 9s 7350K .......... .......... .......... .......... .......... 2% 143M 9s 7400K .......... .......... .......... .......... .......... 2% 213M 9s 7450K .......... .......... .......... .......... .......... 2% 198M 9s 7500K .......... .......... .......... .......... .......... 2% 227M 9s 7550K .......... .......... .......... .......... .......... 2% 226M 9s 7600K .......... .......... .......... .......... .......... 2% 195M 9s 7650K .......... .......... .......... .......... .......... 2% 231M 9s 7700K .......... .......... .......... .......... .......... 2% 194M 9s 7750K .......... .......... .......... .......... .......... 2% 226M 9s 7800K .......... .......... .......... .......... .......... 2% 233M 9s 7850K .......... .......... .......... .......... .......... 3% 195M 9s 7900K .......... .......... .......... .......... .......... 3% 225M 9s 7950K .......... .......... .......... .......... .......... 3% 198M 9s 8000K .......... .......... .......... .......... .......... 3% 227M 9s 8050K .......... .......... .......... .......... .......... 3% 224M 9s 8100K .......... .......... .......... .......... .......... 3% 189M 9s 8150K .......... .......... .......... .......... .......... 3% 295K 14s 8200K .......... .......... .......... .......... .......... 3% 148M 14s 8250K .......... .......... .......... .......... .......... 3% 190M 14s 8300K .......... .......... .......... .......... .......... 3% 144M 14s 8350K .......... .......... .......... .......... .......... 3% 95.6M 14s 8400K .......... .......... .......... .......... .......... 3% 43.4M 13s 8450K .......... .......... .......... .......... .......... 3% 133M 13s 8500K .......... .......... .......... .......... .......... 3% 73.2M 13s 8550K .......... .......... .......... .......... .......... 3% 211M 13s 8600K .......... .......... .......... .......... .......... 3% 65.8M 13s 8650K .......... .......... .......... .......... .......... 3% 127M 13s 8700K .......... .......... .......... .......... .......... 3% 69.6M 13s 8750K .......... .......... .......... .......... .......... 3% 71.2M 13s 8800K .......... .......... .......... .......... .......... 3% 103M 13s 8850K .......... .......... .......... .......... .......... 3% 105M 13s 8900K .......... .......... .......... .......... .......... 3% 100M 13s 8950K .......... .......... .......... .......... .......... 3% 85.5M 13s 9000K .......... .......... .......... .......... .......... 3% 49.0M 13s 9050K .......... .......... .......... .......... .......... 3% 102M 13s 9100K .......... .......... .......... .......... .......... 3% 101M 13s 9150K .......... .......... .......... .......... .......... 3% 77.5M 13s 9200K .......... .......... .......... .......... .......... 3% 97.1M 13s 9250K .......... .......... .......... .......... .......... 3% 109M 12s 9300K .......... .......... .......... .......... .......... 3% 64.2M 12s 9350K .......... .......... .......... .......... .......... 3% 70.1M 12s 9400K .......... .......... .......... .......... .......... 3% 105M 12s 9450K .......... .......... .......... .......... .......... 3% 124M 12s 9500K .......... .......... .......... .......... .......... 3% 114M 12s 9550K .......... .......... .......... .......... .......... 3% 93.5M 12s 9600K .......... .......... .......... .......... .......... 3% 40.7M 12s 9650K .......... .......... .......... .......... .......... 3% 58.8M 12s 9700K .......... .......... .......... .......... .......... 3% 81.4M 12s 9750K .......... .......... .......... .......... .......... 3% 88.5M 12s 9800K .......... .......... .......... .......... .......... 3% 124M 12s 9850K .......... .......... .......... .......... .......... 3% 90.1M 12s 9900K .......... .......... .......... .......... .......... 3% 134M 12s 9950K .......... .......... .......... .......... .......... 3% 183M 12s 10000K .......... .......... .......... .......... .......... 3% 144M 12s 10050K .......... .......... .......... .......... .......... 3% 155M 12s 10100K .......... .......... .......... .......... .......... 3% 162M 12s 10150K .......... .......... .......... .......... .......... 3% 214M 12s 10200K .......... .......... .......... .......... .......... 3% 148K 20s 10250K .......... .......... .......... .......... .......... 3% 115M 20s 10300K .......... .......... .......... .......... .......... 3% 87.3M 20s 10350K .......... .......... .......... .......... .......... 3% 30.7M 20s 10400K .......... .......... .......... .......... .......... 3% 75.7M 19s 10450K .......... .......... .......... .......... .......... 4% 117M 19s 10500K .......... .......... .......... .......... .......... 4% 54.0M 19s 10550K .......... .......... .......... .......... .......... 4% 113M 19s 10600K .......... .......... .......... .......... .......... 4% 89.8M 19s 10650K .......... .......... .......... .......... .......... 4% 96.5M 19s 10700K .......... .......... .......... .......... .......... 4% 90.9M 19s 10750K .......... .......... .......... .......... .......... 4% 108M 19s 10800K .......... .......... .......... .......... .......... 4% 97.9M 19s 10850K .......... .......... .......... .......... .......... 4% 124M 19s 10900K .......... .......... .......... .......... .......... 4% 86.1M 19s 10950K .......... .......... .......... .......... .......... 4% 146M 19s 11000K .......... .......... .......... .......... .......... 4% 195M 19s 11050K .......... .......... .......... .......... .......... 4% 165M 18s 11100K .......... .......... .......... .......... .......... 4% 92.1M 18s 11150K .......... .......... .......... .......... .......... 4% 113M 18s 11200K .......... .......... .......... .......... .......... 4% 85.7M 18s 11250K .......... .......... .......... .......... .......... 4% 75.7M 18s 11300K .......... .......... .......... .......... .......... 4% 89.3M 18s 11350K .......... .......... .......... .......... .......... 4% 55.2M 18s 11400K .......... .......... .......... .......... .......... 4% 65.0M 18s 11450K .......... .......... .......... .......... .......... 4% 95.2M 18s 11500K .......... .......... .......... .......... .......... 4% 61.1M 18s 11550K .......... .......... .......... .......... .......... 4% 87.3M 18s 11600K .......... .......... .......... .......... .......... 4% 110M 18s 11650K .......... .......... .......... .......... .......... 4% 122M 18s 11700K .......... .......... .......... .......... .......... 4% 126M 18s 11750K .......... .......... .......... .......... .......... 4% 958K 19s 11800K .......... .......... .......... .......... .......... 4% 75.0M 18s 11850K .......... .......... .......... .......... .......... 4% 53.5M 18s 11900K .......... .......... .......... .......... .......... 4% 198M 18s 11950K .......... .......... .......... .......... .......... 4% 173M 18s 12000K .......... .......... .......... .......... .......... 4% 119M 18s 12050K .......... .......... .......... .......... .......... 4% 214M 18s 12100K .......... .......... .......... .......... .......... 4% 104M 18s 12150K .......... .......... .......... .......... .......... 4% 171M 18s 12200K .......... .......... .......... .......... .......... 4% 187M 18s 12250K .......... .......... .......... .......... .......... 4% 162K 24s 12300K .......... .......... .......... .......... .......... 4% 89.1M 24s 12350K .......... .......... .......... .......... .......... 4% 186M 24s 12400K .......... .......... .......... .......... .......... 4% 217M 24s 12450K .......... .......... .......... .......... .......... 4% 191M 24s 12500K .......... .......... .......... .......... .......... 4% 80.4M 24s 12550K .......... .......... .......... .......... .......... 4% 287M 24s 12600K .......... .......... .......... .......... .......... 4% 241M 23s 12650K .......... .......... .......... .......... .......... 4% 286M 23s 12700K .......... .......... .......... .......... .......... 4% 239M 23s 12750K .......... .......... .......... .......... .......... 4% 164M 23s 12800K .......... .......... .......... .......... .......... 4% 88.6M 23s 12850K .......... .......... .......... .......... .......... 4% 65.7M 23s 12900K .......... .......... .......... .......... .......... 4% 151M 23s 12950K .......... .......... .......... .......... .......... 4% 175M 23s 13000K .......... .......... .......... .......... .......... 4% 145M 23s 13050K .......... .......... .......... .......... .......... 4% 198M 23s 13100K .......... .......... .......... .......... .......... 5% 189M 23s 13150K .......... .......... .......... .......... .......... 5% 140M 23s 13200K .......... .......... .......... .......... .......... 5% 118M 22s 13250K .......... .......... .......... .......... .......... 5% 305M 22s 13300K .......... .......... .......... .......... .......... 5% 160M 22s 13350K .......... .......... .......... .......... .......... 5% 277M 22s 13400K .......... .......... .......... .......... .......... 5% 273M 22s 13450K .......... .......... .......... .......... .......... 5% 273M 22s 13500K .......... .......... .......... .......... .......... 5% 206M 22s 13550K .......... .......... .......... .......... .......... 5% 182M 22s 13600K .......... .......... .......... .......... .......... 5% 198M 22s 13650K .......... .......... .......... .......... .......... 5% 277M 22s 13700K .......... .......... .......... .......... .......... 5% 198M 22s 13750K .......... .......... .......... .......... .......... 5% 218M 22s 13800K .......... .......... .......... .......... .......... 5% 224M 21s 13850K .......... .......... .......... .......... .......... 5% 11.3M 21s 13900K .......... .......... .......... .......... .......... 5% 120M 21s 13950K .......... .......... .......... .......... .......... 5% 167M 21s 14000K .......... .......... .......... .......... .......... 5% 143M 21s 14050K .......... .......... .......... .......... .......... 5% 158M 21s 14100K .......... .......... .......... .......... .......... 5% 210M 21s 14150K .......... .......... .......... .......... .......... 5% 228M 21s 14200K .......... .......... .......... .......... .......... 5% 230M 21s 14250K .......... .......... .......... .......... .......... 5% 235M 21s 14300K .......... .......... .......... .......... .......... 5% 161M 21s 14350K .......... .......... .......... .......... .......... 5% 166M 21s 14400K .......... .......... .......... .......... .......... 5% 93.5M 21s 14450K .......... .......... .......... .......... .......... 5% 131M 21s 14500K .......... .......... .......... .......... .......... 5% 143M 21s 14550K .......... .......... .......... .......... .......... 5% 166M 20s 14600K .......... .......... .......... .......... .......... 5% 182M 20s 14650K .......... .......... .......... .......... .......... 5% 123M 20s 14700K .......... .......... .......... .......... .......... 5% 179M 20s 14750K .......... .......... .......... .......... .......... 5% 198M 20s 14800K .......... .......... .......... .......... .......... 5% 328M 20s 14850K .......... .......... .......... .......... .......... 5% 155M 20s 14900K .......... .......... .......... .......... .......... 5% 257M 20s 14950K .......... .......... .......... .......... .......... 5% 270M 20s 15000K .......... .......... .......... .......... .......... 5% 204M 20s 15050K .......... .......... .......... .......... .......... 5% 215M 20s 15100K .......... .......... .......... .......... .......... 5% 195M 20s 15150K .......... .......... .......... .......... .......... 5% 198M 20s 15200K .......... .......... .......... .......... .......... 5% 184M 20s 15250K .......... .......... .......... .......... .......... 5% 130M 20s 15300K .......... .......... .......... .......... .......... 5% 216M 19s 15350K .......... .......... .......... .......... .......... 5% 580K 21s 15400K .......... .......... .......... .......... .......... 5% 261M 21s 15450K .......... .......... .......... .......... .......... 5% 44.8M 21s 15500K .......... .......... .......... .......... .......... 5% 209M 21s 15550K .......... .......... .......... .......... .......... 5% 207M 20s 15600K .......... .......... .......... .......... .......... 5% 144M 20s 15650K .......... .......... .......... .......... .......... 5% 305M 20s 15700K .......... .......... .......... .......... .......... 6% 261M 20s 15750K .......... .......... .......... .......... .......... 6% 271M 20s 15800K .......... .......... .......... .......... .......... 6% 205M 20s 15850K .......... .......... .......... .......... .......... 6% 160M 20s 15900K .......... .......... .......... .......... .......... 6% 56.8M 20s 15950K .......... .......... .......... .......... .......... 6% 273M 20s 16000K .......... .......... .......... .......... .......... 6% 326M 20s 16050K .......... .......... .......... .......... .......... 6% 61.4M 20s 16100K .......... .......... .......... .......... .......... 6% 143M 20s 16150K .......... .......... .......... .......... .......... 6% 121M 20s 16200K .......... .......... .......... .......... .......... 6% 58.8M 20s 16250K .......... .......... .......... .......... .......... 6% 260M 20s 16300K .......... .......... .......... .......... .......... 6% 124M 20s 16350K .......... .......... .......... .......... .......... 6% 103M 20s 16400K .......... .......... .......... .......... .......... 6% 223M 19s 16450K .......... .......... .......... .......... .......... 6% 125M 19s 16500K .......... .......... .......... .......... .......... 6% 174M 19s 16550K .......... .......... .......... .......... .......... 6% 140M 19s 16600K .......... .......... .......... .......... .......... 6% 66.1M 19s 16650K .......... .......... .......... .......... .......... 6% 243M 19s 16700K .......... .......... .......... .......... .......... 6% 168M 19s 16750K .......... .......... .......... .......... .......... 6% 85.2M 19s 16800K .......... .......... .......... .......... .......... 6% 123M 19s 16850K .......... .......... .......... .......... .......... 6% 87.3M 19s 16900K .......... .......... .......... .......... .......... 6% 74.5M 19s 16950K .......... .......... .......... .......... .......... 6% 186M 19s 17000K .......... .......... .......... .......... .......... 6% 139M 19s 17050K .......... .......... .......... .......... .......... 6% 62.3M 19s 17100K .......... .......... .......... .......... .......... 6% 233M 19s 17150K .......... .......... .......... .......... .......... 6% 254M 19s 17200K .......... .......... .......... .......... .......... 6% 173M 19s 17250K .......... .......... .......... .......... .......... 6% 204M 19s 17300K .......... .......... .......... .......... .......... 6% 291M 18s 17350K .......... .......... .......... .......... .......... 6% 144M 18s 17400K .......... .......... .......... .......... .......... 6% 1.74M 19s 17450K .......... .......... .......... .......... .......... 6% 1.77M 19s 17500K .......... .......... .......... .......... .......... 6% 294M 19s 17550K .......... .......... .......... .......... .......... 6% 59.0M 19s 17600K .......... .......... .......... .......... .......... 6% 120M 19s 17650K .......... .......... .......... .......... .......... 6% 167M 19s 17700K .......... .......... .......... .......... .......... 6% 164M 19s 17750K .......... .......... .......... .......... .......... 6% 180M 19s 17800K .......... .......... .......... .......... .......... 6% 215M 19s 17850K .......... .......... .......... .......... .......... 6% 183M 19s 17900K .......... .......... .......... .......... .......... 6% 204M 19s 17950K .......... .......... .......... .......... .......... 6% 167M 19s 18000K .......... .......... .......... .......... .......... 6% 90.1M 19s 18050K .......... .......... .......... .......... .......... 6% 196M 18s 18100K .......... .......... .......... .......... .......... 6% 131M 18s 18150K .......... .......... .......... .......... .......... 6% 178M 18s 18200K .......... .......... .......... .......... .......... 6% 89.4M 18s 18250K .......... .......... .......... .......... .......... 6% 158M 18s 18300K .......... .......... .......... .......... .......... 6% 131M 18s 18350K .......... .......... .......... .......... .......... 7% 92.0M 18s 18400K .......... .......... .......... .......... .......... 7% 2.63M 18s 18450K .......... .......... .......... .......... .......... 7% 13.9M 18s 18500K .......... .......... .......... .......... .......... 7% 32.7M 18s 18550K .......... .......... .......... .......... .......... 7% 24.8M 18s 18600K .......... .......... .......... .......... .......... 7% 14.0M 18s 18650K .......... .......... .......... .......... .......... 7% 9.86M 18s 18700K .......... .......... .......... .......... .......... 7% 20.6M 18s 18750K .......... .......... .......... .......... .......... 7% 13.6M 18s 18800K .......... .......... .......... .......... .......... 7% 140M 18s 18850K .......... .......... .......... .......... .......... 7% 96.1M 18s 18900K .......... .......... .......... .......... .......... 7% 128M 18s 18950K .......... .......... .......... .......... .......... 7% 11.6M 18s 19000K .......... .......... .......... .......... .......... 7% 80.2M 18s 19050K .......... .......... .......... .......... .......... 7% 9.38M 18s 19100K .......... .......... .......... .......... .......... 7% 25.8M 18s 19150K .......... .......... .......... .......... .......... 7% 9.07M 18s 19200K .......... .......... .......... .......... .......... 7% 11.8M 18s 19250K .......... .......... .......... .......... .......... 7% 48.0M 18s 19300K .......... .......... .......... .......... .......... 7% 72.4M 18s 19350K .......... .......... .......... .......... .......... 7% 48.0M 18s 19400K .......... .......... .......... .......... .......... 7% 47.3M 18s 19450K .......... .......... .......... .......... .......... 7% 39.3M 18s 19500K .......... .......... .......... .......... .......... 7% 3.58M 18s 19550K .......... .......... .......... .......... .......... 7% 315M 18s 19600K .......... .......... .......... .......... .......... 7% 292M 18s 19650K .......... .......... .......... .......... .......... 7% 48.6M 18s 19700K .......... .......... .......... .......... .......... 7% 43.4M 18s 19750K .......... .......... .......... .......... .......... 7% 48.2M 18s 19800K .......... .......... .......... .......... .......... 7% 72.8M 18s 19850K .......... .......... .......... .......... .......... 7% 70.3M 18s 19900K .......... .......... .......... .......... .......... 7% 103M 18s 19950K .......... .......... .......... .......... .......... 7% 78.0M 18s 20000K .......... .......... .......... .......... .......... 7% 76.3M 18s 20050K .......... .......... .......... .......... .......... 7% 118M 18s 20100K .......... .......... .......... .......... .......... 7% 159M 18s 20150K .......... .......... .......... .......... .......... 7% 49.3M 18s 20200K .......... .......... .......... .......... .......... 7% 2.86M 18s 20250K .......... .......... .......... .......... .......... 7% 46.6M 18s 20300K .......... .......... .......... .......... .......... 7% 15.8M 18s 20350K .......... .......... .......... .......... .......... 7% 42.3M 18s 20400K .......... .......... .......... .......... .......... 7% 109M 18s 20450K .......... .......... .......... .......... .......... 7% 194K 21s 20500K .......... .......... .......... .......... .......... 7% 77.3M 20s 20550K .......... .......... .......... .......... .......... 7% 105M 20s 20600K .......... .......... .......... .......... .......... 7% 43.9M 20s 20650K .......... .......... .......... .......... .......... 7% 62.1M 20s 20700K .......... .......... .......... .......... .......... 7% 169M 20s 20750K .......... .......... .......... .......... .......... 7% 201M 20s 20800K .......... .......... .......... .......... .......... 7% 74.1M 20s 20850K .......... .......... .......... .......... .......... 7% 97.7M 20s 20900K .......... .......... .......... .......... .......... 7% 50.1M 20s 20950K .......... .......... .......... .......... .......... 8% 86.9M 20s 21000K .......... .......... .......... .......... .......... 8% 245M 20s 21050K .......... .......... .......... .......... .......... 8% 105M 20s 21100K .......... .......... .......... .......... .......... 8% 216M 20s 21150K .......... .......... .......... .......... .......... 8% 330M 20s 21200K .......... .......... .......... .......... .......... 8% 289M 20s 21250K .......... .......... .......... .......... .......... 8% 326M 20s 21300K .......... .......... .......... .......... .......... 8% 330M 20s 21350K .......... .......... .......... .......... .......... 8% 277M 20s 21400K .......... .......... .......... .......... .......... 8% 332M 20s 21450K .......... .......... .......... .......... .......... 8% 112M 20s 21500K .......... .......... .......... .......... .......... 8% 12.1M 20s 21550K .......... .......... .......... .......... .......... 8% 170M 20s 21600K .......... .......... .......... .......... .......... 8% 97.5M 20s 21650K .......... .......... .......... .......... .......... 8% 191M 19s 21700K .......... .......... .......... .......... .......... 8% 198M 19s 21750K .......... .......... .......... .......... .......... 8% 220M 19s 21800K .......... .......... .......... .......... .......... 8% 184M 19s 21850K .......... .......... .......... .......... .......... 8% 67.7M 19s 21900K .......... .......... .......... .......... .......... 8% 210M 19s 21950K .......... .......... .......... .......... .......... 8% 83.9M 19s 22000K .......... .......... .......... .......... .......... 8% 176M 19s 22050K .......... .......... .......... .......... .......... 8% 120M 19s 22100K .......... .......... .......... .......... .......... 8% 94.4M 19s 22150K .......... .......... .......... .......... .......... 8% 117M 19s 22200K .......... .......... .......... .......... .......... 8% 144M 19s 22250K .......... .......... .......... .......... .......... 8% 194M 19s 22300K .......... .......... .......... .......... .......... 8% 239M 19s 22350K .......... .......... .......... .......... .......... 8% 186M 19s 22400K .......... .......... .......... .......... .......... 8% 239M 19s 22450K .......... .......... .......... .......... .......... 8% 109M 19s 22500K .......... .......... .......... .......... .......... 8% 3.59M 19s 22550K .......... .......... .......... .......... .......... 8% 6.14M 19s 22600K .......... .......... .......... .......... .......... 8% 4.18M 19s 22650K .......... .......... .......... .......... .......... 8% 313M 19s 22700K .......... .......... .......... .......... .......... 8% 284M 19s 22750K .......... .......... .......... .......... .......... 8% 341M 19s 22800K .......... .......... .......... .......... .......... 8% 337M 19s 22850K .......... .......... .......... .......... .......... 8% 298M 19s 22900K .......... .......... .......... .......... .......... 8% 341M 19s 22950K .......... .......... .......... .......... .......... 8% 291M 19s 23000K .......... .......... .......... .......... .......... 8% 341M 19s 23050K .......... .......... .......... .......... .......... 8% 346M 19s 23100K .......... .......... .......... .......... .......... 8% 294M 19s 23150K .......... .......... .......... .......... .......... 8% 341M 19s 23200K .......... .......... .......... .......... .......... 8% 289M 18s 23250K .......... .......... .......... .......... .......... 8% 341M 18s 23300K .......... .......... .......... .......... .......... 8% 339M 18s 23350K .......... .......... .......... .......... .......... 8% 298M 18s 23400K .......... .......... .......... .......... .......... 8% 321M 18s 23450K .......... .......... .......... .......... .......... 8% 292M 18s 23500K .......... .......... .......... .......... .......... 8% 337M 18s 23550K .......... .......... .......... .......... .......... 9% 8.41M 18s 23600K .......... .......... .......... .......... .......... 9% 149M 18s 23650K .......... .......... .......... .......... .......... 9% 95.9M 18s 23700K .......... .......... .......... .......... .......... 9% 151M 18s 23750K .......... .......... .......... .......... .......... 9% 301M 18s 23800K .......... .......... .......... .......... .......... 9% 311M 18s 23850K .......... .......... .......... .......... .......... 9% 218M 18s 23900K .......... .......... .......... .......... .......... 9% 187M 18s 23950K .......... .......... .......... .......... .......... 9% 260M 18s 24000K .......... .......... .......... .......... .......... 9% 309M 18s 24050K .......... .......... .......... .......... .......... 9% 104M 18s 24100K .......... .......... .......... .......... .......... 9% 180M 18s 24150K .......... .......... .......... .......... .......... 9% 157M 18s 24200K .......... .......... .......... .......... .......... 9% 154M 18s 24250K .......... .......... .......... .......... .......... 9% 197M 18s 24300K .......... .......... .......... .......... .......... 9% 213M 18s 24350K .......... .......... .......... .......... .......... 9% 149M 18s 24400K .......... .......... .......... .......... .......... 9% 223M 18s 24450K .......... .......... .......... .......... .......... 9% 253M 18s 24500K .......... .......... .......... .......... .......... 9% 252M 18s 24550K .......... .......... .......... .......... .......... 9% 2.46M 18s 24600K .......... .......... .......... .......... .......... 9% 39.6M 18s 24650K .......... .......... .......... .......... .......... 9% 192M 18s 24700K .......... .......... .......... .......... .......... 9% 94.8M 18s 24750K .......... .......... .......... .......... .......... 9% 3.46M 18s 24800K .......... .......... .......... .......... .......... 9% 315M 18s 24850K .......... .......... .......... .......... .......... 9% 286M 18s 24900K .......... .......... .......... .......... .......... 9% 330M 18s 24950K .......... .......... .......... .......... .......... 9% 286M 18s 25000K .......... .......... .......... .......... .......... 9% 332M 17s 25050K .......... .......... .......... .......... .......... 9% 339M 17s 25100K .......... .......... .......... .......... .......... 9% 296M 17s 25150K .......... .......... .......... .......... .......... 9% 337M 17s 25200K .......... .......... .......... .......... .......... 9% 296M 17s 25250K .......... .......... .......... .......... .......... 9% 337M 17s 25300K .......... .......... .......... .......... .......... 9% 334M 17s 25350K .......... .......... .......... .......... .......... 9% 249M 17s 25400K .......... .......... .......... .......... .......... 9% 53.8M 17s 25450K .......... .......... .......... .......... .......... 9% 170M 17s 25500K .......... .......... .......... .......... .......... 9% 307M 17s 25550K .......... .......... .......... .......... .......... 9% 326M 17s 25600K .......... .......... .......... .......... .......... 9% 168K 20s 25650K .......... .......... .......... .......... .......... 9% 180M 20s 25700K .......... .......... .......... .......... .......... 9% 148M 20s 25750K .......... .......... .......... .......... .......... 9% 130M 20s 25800K .......... .......... .......... .......... .......... 9% 54.4M 20s 25850K .......... .......... .......... .......... .......... 9% 77.6M 20s 25900K .......... .......... .......... .......... .......... 9% 190M 20s 25950K .......... .......... .......... .......... .......... 9% 135M 20s 26000K .......... .......... .......... .......... .......... 9% 296M 19s 26050K .......... .......... .......... .......... .......... 9% 276M 19s 26100K .......... .......... .......... .......... .......... 9% 263M 19s 26150K .......... .......... .......... .......... .......... 9% 230M 19s 26200K .......... .......... .......... .......... .......... 10% 268M 19s 26250K .......... .......... .......... .......... .......... 10% 256M 19s 26300K .......... .......... .......... .......... .......... 10% 273M 19s 26350K .......... .......... .......... .......... .......... 10% 268M 19s 26400K .......... .......... .......... .......... .......... 10% 256M 19s 26450K .......... .......... .......... .......... .......... 10% 182M 19s 26500K .......... .......... .......... .......... .......... 10% 270M 19s 26550K .......... .......... .......... .......... .......... 10% 267M 19s 26600K .......... .......... .......... .......... .......... 10% 110M 19s 26650K .......... .......... .......... .......... .......... 10% 301M 19s 26700K .......... .......... .......... .......... .......... 10% 91.4M 19s 26750K .......... .......... .......... .......... .......... 10% 178M 19s 26800K .......... .......... .......... .......... .......... 10% 176M 19s 26850K .......... .......... .......... .......... .......... 10% 228M 19s 26900K .......... .......... .......... .......... .......... 10% 226M 19s 26950K .......... .......... .......... .......... .......... 10% 203M 19s 27000K .......... .......... .......... .......... .......... 10% 276M 19s 27050K .......... .......... .......... .......... .......... 10% 273M 19s 27100K .......... .......... .......... .......... .......... 10% 140M 19s 27150K .......... .......... .......... .......... .......... 10% 233M 19s 27200K .......... .......... .......... .......... .......... 10% 227M 19s 27250K .......... .......... .......... .......... .......... 10% 189M 19s 27300K .......... .......... .......... .......... .......... 10% 88.1M 19s 27350K .......... .......... .......... .......... .......... 10% 239M 18s 27400K .......... .......... .......... .......... .......... 10% 167M 18s 27450K .......... .......... .......... .......... .......... 10% 241M 18s 27500K .......... .......... .......... .......... .......... 10% 339M 18s 27550K .......... .......... .......... .......... .......... 10% 183M 18s 27600K .......... .......... .......... .......... .......... 10% 55.4M 18s 27650K .......... .......... .......... .......... .......... 10% 69.8M 18s 27700K .......... .......... .......... .......... .......... 10% 211M 18s 27750K .......... .......... .......... .......... .......... 10% 258M 18s 27800K .......... .......... .......... .......... .......... 10% 74.4M 18s 27850K .......... .......... .......... .......... .......... 10% 122M 18s 27900K .......... .......... .......... .......... .......... 10% 91.3M 18s 27950K .......... .......... .......... .......... .......... 10% 223M 18s 28000K .......... .......... .......... .......... .......... 10% 192M 18s 28050K .......... .......... .......... .......... .......... 10% 103M 18s 28100K .......... .......... .......... .......... .......... 10% 213M 18s 28150K .......... .......... .......... .......... .......... 10% 253M 18s 28200K .......... .......... .......... .......... .......... 10% 221M 18s 28250K .......... .......... .......... .......... .......... 10% 260M 18s 28300K .......... .......... .......... .......... .......... 10% 247M 18s 28350K .......... .......... .......... .......... .......... 10% 222M 18s 28400K .......... .......... .......... .......... .......... 10% 254M 18s 28450K .......... .......... .......... .......... .......... 10% 220M 18s 28500K .......... .......... .......... .......... .......... 10% 261M 18s 28550K .......... .......... .......... .......... .......... 10% 250M 18s 28600K .......... .......... .......... .......... .......... 10% 216M 18s 28650K .......... .......... .......... .......... .......... 10% 3.25M 18s 28700K .......... .......... .......... .......... .......... 10% 6.89M 18s 28750K .......... .......... .......... .......... .......... 10% 165M 18s 28800K .......... .......... .......... .......... .......... 11% 132M 18s 28850K .......... .......... .......... .......... .......... 11% 138M 18s 28900K .......... .......... .......... .......... .......... 11% 105M 18s 28950K .......... .......... .......... .......... .......... 11% 194M 18s 29000K .......... .......... .......... .......... .......... 11% 276M 18s 29050K .......... .......... .......... .......... .......... 11% 164M 18s 29100K .......... .......... .......... .......... .......... 11% 171M 17s 29150K .......... .......... .......... .......... .......... 11% 142M 17s 29200K .......... .......... .......... .......... .......... 11% 133M 17s 29250K .......... .......... .......... .......... .......... 11% 203M 17s 29300K .......... .......... .......... .......... .......... 11% 154M 17s 29350K .......... .......... .......... .......... .......... 11% 143M 17s 29400K .......... .......... .......... .......... .......... 11% 177M 17s 29450K .......... .......... .......... .......... .......... 11% 268M 17s 29500K .......... .......... .......... .......... .......... 11% 274M 17s 29550K .......... .......... .......... .......... .......... 11% 164M 17s 29600K .......... .......... .......... .......... .......... 11% 234M 17s 29650K .......... .......... .......... .......... .......... 11% 317M 17s 29700K .......... .......... .......... .......... .......... 11% 83.2M 17s 29750K .......... .......... .......... .......... .......... 11% 144M 17s 29800K .......... .......... .......... .......... .......... 11% 113M 17s 29850K .......... .......... .......... .......... .......... 11% 140M 17s 29900K .......... .......... .......... .......... .......... 11% 296M 17s 29950K .......... .......... .......... .......... .......... 11% 150M 17s 30000K .......... .......... .......... .......... .......... 11% 326M 17s 30050K .......... .......... .......... .......... .......... 11% 311M 17s 30100K .......... .......... .......... .......... .......... 11% 271M 17s 30150K .......... .......... .......... .......... .......... 11% 341M 17s 30200K .......... .......... .......... .......... .......... 11% 223M 17s 30250K .......... .......... .......... .......... .......... 11% 317M 17s 30300K .......... .......... .......... .......... .......... 11% 332M 17s 30350K .......... .......... .......... .......... .......... 11% 271M 17s 30400K .......... .......... .......... .......... .......... 11% 332M 17s 30450K .......... .......... .......... .......... .......... 11% 273M 17s 30500K .......... .......... .......... .......... .......... 11% 337M 17s 30550K .......... .......... .......... .......... .......... 11% 339M 17s 30600K .......... .......... .......... .......... .......... 11% 292M 17s 30650K .......... .......... .......... .......... .......... 11% 311M 17s 30700K .......... .......... .......... .......... .......... 11% 2.63M 17s 30750K .......... .......... .......... .......... .......... 11% 190M 17s 30800K .......... .......... .......... .......... .......... 11% 25.6M 17s 30850K .......... .......... .......... .......... .......... 11% 106M 17s 30900K .......... .......... .......... .......... .......... 11% 103M 17s 30950K .......... .......... .......... .......... .......... 11% 105M 17s 31000K .......... .......... .......... .......... .......... 11% 106M 17s 31050K .......... .......... .......... .......... .......... 11% 260M 16s 31100K .......... .......... .......... .......... .......... 11% 120M 16s 31150K .......... .......... .......... .......... .......... 11% 213M 16s 31200K .......... .......... .......... .......... .......... 11% 200M 16s 31250K .......... .......... .......... .......... .......... 11% 102M 16s 31300K .......... .......... .......... .......... .......... 11% 248M 16s 31350K .......... .......... .......... .......... .......... 11% 189M 16s 31400K .......... .......... .......... .......... .......... 11% 250M 16s 31450K .......... .......... .......... .......... .......... 12% 210M 16s 31500K .......... .......... .......... .......... .......... 12% 254M 16s 31550K .......... .......... .......... .......... .......... 12% 254M 16s 31600K .......... .......... .......... .......... .......... 12% 228M 16s 31650K .......... .......... .......... .......... .......... 12% 121M 16s 31700K .......... .......... .......... .......... .......... 12% 1.67M 16s 31750K .......... .......... .......... .......... .......... 12% 277M 16s 31800K .......... .......... .......... .......... .......... 12% 225M 16s 31850K .......... .......... .......... .......... .......... 12% 53.7M 16s 31900K .......... .......... .......... .......... .......... 12% 159M 16s 31950K .......... .......... .......... .......... .......... 12% 136M 16s 32000K .......... .......... .......... .......... .......... 12% 107M 16s 32050K .......... .......... .......... .......... .......... 12% 263M 16s 32100K .......... .......... .......... .......... .......... 12% 210M 16s 32150K .......... .......... .......... .......... .......... 12% 213M 16s 32200K .......... .......... .......... .......... .......... 12% 270M 16s 32250K .......... .......... .......... .......... .......... 12% 206M 16s 32300K .......... .......... .......... .......... .......... 12% 164M 16s 32350K .......... .......... .......... .......... .......... 12% 203M 16s 32400K .......... .......... .......... .......... .......... 12% 301M 16s 32450K .......... .......... .......... .......... .......... 12% 194M 16s 32500K .......... .......... .......... .......... .......... 12% 238M 16s 32550K .......... .......... .......... .......... .......... 12% 286M 16s 32600K .......... .......... .......... .......... .......... 12% 212M 16s 32650K .......... .......... .......... .......... .......... 12% 321M 16s 32700K .......... .......... .......... .......... .......... 12% 281M 16s 32750K .......... .......... .......... .......... .......... 12% 168M 16s 32800K .......... .......... .......... .......... .......... 12% 287M 16s 32850K .......... .......... .......... .......... .......... 12% 21.4M 16s 32900K .......... .......... .......... .......... .......... 12% 219M 16s 32950K .......... .......... .......... .......... .......... 12% 245M 16s 33000K .......... .......... .......... .......... .......... 12% 204M 16s 33050K .......... .......... .......... .......... .......... 12% 234M 16s 33100K .......... .......... .......... .......... .......... 12% 186M 16s 33150K .......... .......... .......... .......... .......... 12% 133M 16s 33200K .......... .......... .......... .......... .......... 12% 142M 16s 33250K .......... .......... .......... .......... .......... 12% 252M 16s 33300K .......... .......... .......... .......... .......... 12% 143M 16s 33350K .......... .......... .......... .......... .......... 12% 171M 15s 33400K .......... .......... .......... .......... .......... 12% 313M 15s 33450K .......... .......... .......... .......... .......... 12% 231M 15s 33500K .......... .......... .......... .......... .......... 12% 267M 15s 33550K .......... .......... .......... .......... .......... 12% 224M 15s 33600K .......... .......... .......... .......... .......... 12% 287M 15s 33650K .......... .......... .......... .......... .......... 12% 263M 15s 33700K .......... .......... .......... .......... .......... 12% 215M 15s 33750K .......... .......... .......... .......... .......... 12% 2.46M 15s 33800K .......... .......... .......... .......... .......... 12% 212M 15s 33850K .......... .......... .......... .......... .......... 12% 13.7M 15s 33900K .......... .......... .......... .......... .......... 12% 195M 15s 33950K .......... .......... .......... .......... .......... 12% 119M 15s 34000K .......... .......... .......... .......... .......... 12% 294M 15s 34050K .......... .......... .......... .......... .......... 13% 309M 15s 34100K .......... .......... .......... .......... .......... 13% 3.60M 15s 34150K .......... .......... .......... .......... .......... 13% 157M 15s 34200K .......... .......... .......... .......... .......... 13% 73.1M 15s 34250K .......... .......... .......... .......... .......... 13% 298M 15s 34300K .......... .......... .......... .......... .......... 13% 158M 15s 34350K .......... .......... .......... .......... .......... 13% 242M 15s 34400K .......... .......... .......... .......... .......... 13% 281M 15s 34450K .......... .......... .......... .......... .......... 13% 284M 15s 34500K .......... .......... .......... .......... .......... 13% 300M 15s 34550K .......... .......... .......... .......... .......... 13% 296M 15s 34600K .......... .......... .......... .......... .......... 13% 271M 15s 34650K .......... .......... .......... .......... .......... 13% 339M 15s 34700K .......... .......... .......... .......... .......... 13% 271M 15s 34750K .......... .......... .......... .......... .......... 13% 328M 15s 34800K .......... .......... .......... .......... .......... 13% 233M 15s 34850K .......... .......... .......... .......... .......... 13% 281M 15s 34900K .......... .......... .......... .......... .......... 13% 326M 15s 34950K .......... .......... .......... .......... .......... 13% 277M 15s 35000K .......... .......... .......... .......... .......... 13% 326M 15s 35050K .......... .......... .......... .......... .......... 13% 330M 15s 35100K .......... .......... .......... .......... .......... 13% 284M 15s 35150K .......... .......... .......... .......... .......... 13% 344M 15s 35200K .......... .......... .......... .......... .......... 13% 267M 15s 35250K .......... .......... .......... .......... .......... 13% 319M 15s 35300K .......... .......... .......... .......... .......... 13% 332M 15s 35350K .......... .......... .......... .......... .......... 13% 289M 15s 35400K .......... .......... .......... .......... .......... 13% 332M 15s 35450K .......... .......... .......... .......... .......... 13% 291M 15s 35500K .......... .......... .......... .......... .......... 13% 337M 15s 35550K .......... .......... .......... .......... .......... 13% 344M 15s 35600K .......... .......... .......... .......... .......... 13% 279M 15s 35650K .......... .......... .......... .......... .......... 13% 326M 15s 35700K .......... .......... .......... .......... .......... 13% 287M 15s 35750K .......... .......... .......... .......... .......... 13% 326M 15s 35800K .......... .......... .......... .......... .......... 13% 205K 16s 35850K .......... .......... .......... .......... .......... 13% 92.1M 16s 35900K .......... .......... .......... .......... .......... 13% 105M 16s 35950K .......... .......... .......... .......... .......... 13% 157M 16s 36000K .......... .......... .......... .......... .......... 13% 67.4M 16s 36050K .......... .......... .......... .......... .......... 13% 138M 16s 36100K .......... .......... .......... .......... .......... 13% 81.7M 16s 36150K .......... .......... .......... .......... .......... 13% 83.3M 16s 36200K .......... .......... .......... .......... .......... 13% 59.0M 16s 36250K .......... .......... .......... .......... .......... 13% 139M 16s 36300K .......... .......... .......... .......... .......... 13% 140M 16s 36350K .......... .......... .......... .......... .......... 13% 104M 16s 36400K .......... .......... .......... .......... .......... 13% 50.3M 16s 36450K .......... .......... .......... .......... .......... 13% 160M 16s 36500K .......... .......... .......... .......... .......... 13% 205M 16s 36550K .......... .......... .......... .......... .......... 13% 90.8M 16s 36600K .......... .......... .......... .......... .......... 13% 114M 16s 36650K .......... .......... .......... .......... .......... 13% 138M 16s 36700K .......... .......... .......... .......... .......... 14% 111M 16s 36750K .......... .......... .......... .......... .......... 14% 202M 16s 36800K .......... .......... .......... .......... .......... 14% 123M 16s 36850K .......... .......... .......... .......... .......... 14% 42.0M 16s 36900K .......... .......... .......... .......... .......... 14% 138M 16s 36950K .......... .......... .......... .......... .......... 14% 101M 16s 37000K .......... .......... .......... .......... .......... 14% 182M 16s 37050K .......... .......... .......... .......... .......... 14% 191M 16s 37100K .......... .......... .......... .......... .......... 14% 91.1M 16s 37150K .......... .......... .......... .......... .......... 14% 102M 16s 37200K .......... .......... .......... .......... .......... 14% 108M 15s 37250K .......... .......... .......... .......... .......... 14% 131M 15s 37300K .......... .......... .......... .......... .......... 14% 178M 15s 37350K .......... .......... .......... .......... .......... 14% 156M 15s 37400K .......... .......... .......... .......... .......... 14% 165M 15s 37450K .......... .......... .......... .......... .......... 14% 170M 15s 37500K .......... .......... .......... .......... .......... 14% 188M 15s 37550K .......... .......... .......... .......... .......... 14% 291M 15s 37600K .......... .......... .......... .......... .......... 14% 168M 15s 37650K .......... .......... .......... .......... .......... 14% 82.2M 15s 37700K .......... .......... .......... .......... .......... 14% 117M 15s 37750K .......... .......... .......... .......... .......... 14% 120M 15s 37800K .......... .......... .......... .......... .......... 14% 84.9M 15s 37850K .......... .......... .......... .......... .......... 14% 1.86M 15s 37900K .......... .......... .......... .......... .......... 14% 183M 15s 37950K .......... .......... .......... .......... .......... 14% 279M 15s 38000K .......... .......... .......... .......... .......... 14% 152M 15s 38050K .......... .......... .......... .......... .......... 14% 252M 15s 38100K .......... .......... .......... .......... .......... 14% 236M 15s 38150K .......... .......... .......... .......... .......... 14% 279M 15s 38200K .......... .......... .......... .......... .......... 14% 115M 15s 38250K .......... .......... .......... .......... .......... 14% 116M 15s 38300K .......... .......... .......... .......... .......... 14% 143M 15s 38350K .......... .......... .......... .......... .......... 14% 125M 15s 38400K .......... .......... .......... .......... .......... 14% 149M 15s 38450K .......... .......... .......... .......... .......... 14% 125M 15s 38500K .......... .......... .......... .......... .......... 14% 230M 15s 38550K .......... .......... .......... .......... .......... 14% 332M 15s 38600K .......... .......... .......... .......... .......... 14% 286M 15s 38650K .......... .......... .......... .......... .......... 14% 334M 15s 38700K .......... .......... .......... .......... .......... 14% 261M 15s 38750K .......... .......... .......... .......... .......... 14% 313M 15s 38800K .......... .......... .......... .......... .......... 14% 334M 15s 38850K .......... .......... .......... .......... .......... 14% 291M 15s 38900K .......... .......... .......... .......... .......... 14% 4.15M 15s 38950K .......... .......... .......... .......... .......... 14% 60.0M 15s 39000K .......... .......... .......... .......... .......... 14% 298M 15s 39050K .......... .......... .......... .......... .......... 14% 118M 15s 39100K .......... .......... .......... .......... .......... 14% 248M 15s 39150K .......... .......... .......... .......... .......... 14% 155M 15s 39200K .......... .......... .......... .......... .......... 14% 230M 15s 39250K .......... .......... .......... .......... .......... 14% 223M 15s 39300K .......... .......... .......... .......... .......... 15% 326M 15s 39350K .......... .......... .......... .......... .......... 15% 281M 15s 39400K .......... .......... .......... .......... .......... 15% 332M 15s 39450K .......... .......... .......... .......... .......... 15% 281M 15s 39500K .......... .......... .......... .......... .......... 15% 319M 15s 39550K .......... .......... .......... .......... .......... 15% 315M 15s 39600K .......... .......... .......... .......... .......... 15% 289M 15s 39650K .......... .......... .......... .......... .......... 15% 237M 15s 39700K .......... .......... .......... .......... .......... 15% 282M 15s 39750K .......... .......... .......... .......... .......... 15% 332M 15s 39800K .......... .......... .......... .......... .......... 15% 309M 15s 39850K .......... .......... .......... .......... .......... 15% 261M 15s 39900K .......... .......... .......... .......... .......... 15% 234M 15s 39950K .......... .......... .......... .......... .......... 15% 267M 15s 40000K .......... .......... .......... .......... .......... 15% 238M 15s 40050K .......... .......... .......... .......... .......... 15% 326M 14s 40100K .......... .......... .......... .......... .......... 15% 264M 14s 40150K .......... .......... .......... .......... .......... 15% 313M 14s 40200K .......... .......... .......... .......... .......... 15% 281M 14s 40250K .......... .......... .......... .......... .......... 15% 334M 14s 40300K .......... .......... .......... .......... .......... 15% 328M 14s 40350K .......... .......... .......... .......... .......... 15% 279M 14s 40400K .......... .......... .......... .......... .......... 15% 315M 14s 40450K .......... .......... .......... .......... .......... 15% 212M 14s 40500K .......... .......... .......... .......... .......... 15% 319M 14s 40550K .......... .......... .......... .......... .......... 15% 303M 14s 40600K .......... .......... .......... .......... .......... 15% 170M 14s 40650K .......... .......... .......... .......... .......... 15% 289M 14s 40700K .......... .......... .......... .......... .......... 15% 131M 14s 40750K .......... .......... .......... .......... .......... 15% 238M 14s 40800K .......... .......... .......... .......... .......... 15% 217M 14s 40850K .......... .......... .......... .......... .......... 15% 159M 14s 40900K .......... .......... .......... .......... .......... 15% 171M 14s 40950K .......... .......... .......... .......... .......... 15% 260K 15s 41000K .......... .......... .......... .......... .......... 15% 163M 15s 41050K .......... .......... .......... .......... .......... 15% 65.1M 15s 41100K .......... .......... .......... .......... .......... 15% 99.4M 15s 41150K .......... .......... .......... .......... .......... 15% 130M 15s 41200K .......... .......... .......... .......... .......... 15% 101M 15s 41250K .......... .......... .......... .......... .......... 15% 148M 15s 41300K .......... .......... .......... .......... .......... 15% 164M 15s 41350K .......... .......... .......... .......... .......... 15% 46.5M 15s 41400K .......... .......... .......... .......... .......... 15% 188M 15s 41450K .......... .......... .......... .......... .......... 15% 117M 15s 41500K .......... .......... .......... .......... .......... 15% 127M 15s 41550K .......... .......... .......... .......... .......... 15% 221M 15s 41600K .......... .......... .......... .......... .......... 15% 284M 15s 41650K .......... .......... .......... .......... .......... 15% 93.0M 15s 41700K .......... .......... .......... .......... .......... 15% 127M 15s 41750K .......... .......... .......... .......... .......... 15% 317M 15s 41800K .......... .......... .......... .......... .......... 15% 202M 15s 41850K .......... .......... .......... .......... .......... 15% 114M 15s 41900K .......... .......... .......... .......... .......... 15% 87.7M 15s 41950K .......... .......... .......... .......... .......... 16% 45.7M 15s 42000K .......... .......... .......... .......... .......... 16% 202M 15s 42050K .......... .......... .......... .......... .......... 16% 211M 15s 42100K .......... .......... .......... .......... .......... 16% 186M 15s 42150K .......... .......... .......... .......... .......... 16% 1.35M 15s 42200K .......... .......... .......... .......... .......... 16% 189M 15s 42250K .......... .......... .......... .......... .......... 16% 228M 15s 42300K .......... .......... .......... .......... .......... 16% 76.1M 15s 42350K .......... .......... .......... .......... .......... 16% 155M 15s 42400K .......... .......... .......... .......... .......... 16% 136M 15s 42450K .......... .......... .......... .......... .......... 16% 117M 15s 42500K .......... .......... .......... .......... .......... 16% 153M 15s 42550K .......... .......... .......... .......... .......... 16% 157M 15s 42600K .......... .......... .......... .......... .......... 16% 189M 15s 42650K .......... .......... .......... .......... .......... 16% 174M 15s 42700K .......... .......... .......... .......... .......... 16% 135M 15s 42750K .......... .......... .......... .......... .......... 16% 85.4M 15s 42800K .......... .......... .......... .......... .......... 16% 148M 15s 42850K .......... .......... .......... .......... .......... 16% 125M 15s 42900K .......... .......... .......... .......... .......... 16% 146M 15s 42950K .......... .......... .......... .......... .......... 16% 95.4M 15s 43000K .......... .......... .......... .......... .......... 16% 897K 15s 43050K .......... .......... .......... .......... .......... 16% 86.4M 15s 43100K .......... .......... .......... .......... .......... 16% 108M 15s 43150K .......... .......... .......... .......... .......... 16% 205M 15s 43200K .......... .......... .......... .......... .......... 16% 120M 15s 43250K .......... .......... .......... .......... .......... 16% 187M 15s 43300K .......... .......... .......... .......... .......... 16% 89.4M 15s 43350K .......... .......... .......... .......... .......... 16% 184M 15s 43400K .......... .......... .......... .......... .......... 16% 191M 15s 43450K .......... .......... .......... .......... .......... 16% 130M 15s 43500K .......... .......... .......... .......... .......... 16% 161M 15s 43550K .......... .......... .......... .......... .......... 16% 317M 15s 43600K .......... .......... .......... .......... .......... 16% 217M 15s 43650K .......... .......... .......... .......... .......... 16% 159M 15s 43700K .......... .......... .......... .......... .......... 16% 170M 15s 43750K .......... .......... .......... .......... .......... 16% 98.4M 15s 43800K .......... .......... .......... .......... .......... 16% 284M 15s 43850K .......... .......... .......... .......... .......... 16% 215M 15s 43900K .......... .......... .......... .......... .......... 16% 279M 15s 43950K .......... .......... .......... .......... .......... 16% 223M 15s 44000K .......... .......... .......... .......... .......... 16% 46.6M 14s 44050K .......... .......... .......... .......... .......... 16% 98.6M 14s 44100K .......... .......... .......... .......... .......... 16% 51.9M 14s 44150K .......... .......... .......... .......... .......... 16% 114M 14s 44200K .......... .......... .......... .......... .......... 16% 1.98M 15s 44250K .......... .......... .......... .......... .......... 16% 287M 15s 44300K .......... .......... .......... .......... .......... 16% 303M 15s 44350K .......... .......... .......... .......... .......... 16% 71.1M 14s 44400K .......... .......... .......... .......... .......... 16% 212M 14s 44450K .......... .......... .......... .......... .......... 16% 98.8M 14s 44500K .......... .......... .......... .......... .......... 16% 128M 14s 44550K .......... .......... .......... .......... .......... 17% 219M 14s 44600K .......... .......... .......... .......... .......... 17% 115M 14s 44650K .......... .......... .......... .......... .......... 17% 208M 14s 44700K .......... .......... .......... .......... .......... 17% 168M 14s 44750K .......... .......... .......... .......... .......... 17% 205M 14s 44800K .......... .......... .......... .......... .......... 17% 119M 14s 44850K .......... .......... .......... .......... .......... 17% 117M 14s 44900K .......... .......... .......... .......... .......... 17% 165M 14s 44950K .......... .......... .......... .......... .......... 17% 208M 14s 45000K .......... .......... .......... .......... .......... 17% 156M 14s 45050K .......... .......... .......... .......... .......... 17% 5.14M 14s 45100K .......... .......... .......... .......... .......... 17% 74.8M 14s 45150K .......... .......... .......... .......... .......... 17% 199M 14s 45200K .......... .......... .......... .......... .......... 17% 158M 14s 45250K .......... .......... .......... .......... .......... 17% 123M 14s 45300K .......... .......... .......... .......... .......... 17% 311M 14s 45350K .......... .......... .......... .......... .......... 17% 192M 14s 45400K .......... .......... .......... .......... .......... 17% 260M 14s 45450K .......... .......... .......... .......... .......... 17% 86.7M 14s 45500K .......... .......... .......... .......... .......... 17% 117M 14s 45550K .......... .......... .......... .......... .......... 17% 212M 14s 45600K .......... .......... .......... .......... .......... 17% 182M 14s 45650K .......... .......... .......... .......... .......... 17% 132M 14s 45700K .......... .......... .......... .......... .......... 17% 151M 14s 45750K .......... .......... .......... .......... .......... 17% 258M 14s 45800K .......... .......... .......... .......... .......... 17% 130M 14s 45850K .......... .......... .......... .......... .......... 17% 118M 14s 45900K .......... .......... .......... .......... .......... 17% 111M 14s 45950K .......... .......... .......... .......... .......... 17% 183M 14s 46000K .......... .......... .......... .......... .......... 17% 279M 14s 46050K .......... .......... .......... .......... .......... 17% 342K 15s 46100K .......... .......... .......... .......... .......... 17% 135M 15s 46150K .......... .......... .......... .......... .......... 17% 113M 15s 46200K .......... .......... .......... .......... .......... 17% 74.0M 15s 46250K .......... .......... .......... .......... .......... 17% 50.3M 15s 46300K .......... .......... .......... .......... .......... 17% 87.8M 15s 46350K .......... .......... .......... .......... .......... 17% 104M 15s 46400K .......... .......... .......... .......... .......... 17% 75.9M 15s 46450K .......... .......... .......... .......... .......... 17% 148M 14s 46500K .......... .......... .......... .......... .......... 17% 144M 14s 46550K .......... .......... .......... .......... .......... 17% 139M 14s 46600K .......... .......... .......... .......... .......... 17% 79.7M 14s 46650K .......... .......... .......... .......... .......... 17% 157M 14s 46700K .......... .......... .......... .......... .......... 17% 94.8M 14s 46750K .......... .......... .......... .......... .......... 17% 69.2M 14s 46800K .......... .......... .......... .......... .......... 17% 78.9M 14s 46850K .......... .......... .......... .......... .......... 17% 85.5M 14s 46900K .......... .......... .......... .......... .......... 17% 124M 14s 46950K .......... .......... .......... .......... .......... 17% 164M 14s 47000K .......... .......... .......... .......... .......... 17% 176M 14s 47050K .......... .......... .......... .......... .......... 17% 209M 14s 47100K .......... .......... .......... .......... .......... 17% 74.7M 14s 47150K .......... .......... .......... .......... .......... 18% 111M 14s 47200K .......... .......... .......... .......... .......... 18% 132M 14s 47250K .......... .......... .......... .......... .......... 18% 195M 14s 47300K .......... .......... .......... .......... .......... 18% 238M 14s 47350K .......... .......... .......... .......... .......... 18% 163M 14s 47400K .......... .......... .......... .......... .......... 18% 219M 14s 47450K .......... .......... .......... .......... .......... 18% 200M 14s 47500K .......... .......... .......... .......... .......... 18% 208M 14s 47550K .......... .......... .......... .......... .......... 18% 217M 14s 47600K .......... .......... .......... .......... .......... 18% 188M 14s 47650K .......... .......... .......... .......... .......... 18% 213M 14s 47700K .......... .......... .......... .......... .......... 18% 149M 14s 47750K .......... .......... .......... .......... .......... 18% 202M 14s 47800K .......... .......... .......... .......... .......... 18% 234M 14s 47850K .......... .......... .......... .......... .......... 18% 204M 14s 47900K .......... .......... .......... .......... .......... 18% 184M 14s 47950K .......... .......... .......... .......... .......... 18% 156M 14s 48000K .......... .......... .......... .......... .......... 18% 206M 14s 48050K .......... .......... .......... .......... .......... 18% 229M 14s 48100K .......... .......... .......... .......... .......... 18% 703K 14s 48150K .......... .......... .......... .......... .......... 18% 243M 14s 48200K .......... .......... .......... .......... .......... 18% 99.0M 14s 48250K .......... .......... .......... .......... .......... 18% 156M 14s 48300K .......... .......... .......... .......... .......... 18% 184M 14s 48350K .......... .......... .......... .......... .......... 18% 163M 14s 48400K .......... .......... .......... .......... .......... 18% 132M 14s 48450K .......... .......... .......... .......... .......... 18% 140M 14s 48500K .......... .......... .......... .......... .......... 18% 198M 14s 48550K .......... .......... .......... .......... .......... 18% 183M 14s 48600K .......... .......... .......... .......... .......... 18% 79.9M 14s 48650K .......... .......... .......... .......... .......... 18% 130M 14s 48700K .......... .......... .......... .......... .......... 18% 139M 14s 48750K .......... .......... .......... .......... .......... 18% 140M 14s 48800K .......... .......... .......... .......... .......... 18% 121M 14s 48850K .......... .......... .......... .......... .......... 18% 101M 14s 48900K .......... .......... .......... .......... .......... 18% 108M 14s 48950K .......... .......... .......... .......... .......... 18% 193M 14s 49000K .......... .......... .......... .......... .......... 18% 74.5M 14s 49050K .......... .......... .......... .......... .......... 18% 118M 14s 49100K .......... .......... .......... .......... .......... 18% 167M 14s 49150K .......... .......... .......... .......... .......... 18% 82.3M 14s 49200K .......... .......... .......... .......... .......... 18% 78.3M 14s 49250K .......... .......... .......... .......... .......... 18% 159M 14s 49300K .......... .......... .......... .......... .......... 18% 121M 14s 49350K .......... .......... .......... .......... .......... 18% 139M 14s 49400K .......... .......... .......... .......... .......... 18% 201M 14s 49450K .......... .......... .......... .......... .......... 18% 90.3M 14s 49500K .......... .......... .......... .......... .......... 18% 114M 14s 49550K .......... .......... .......... .......... .......... 18% 104M 14s 49600K .......... .......... .......... .......... .......... 18% 252M 14s 49650K .......... .......... .......... .......... .......... 18% 177M 14s 49700K .......... .......... .......... .......... .......... 18% 116M 14s 49750K .......... .......... .......... .......... .......... 18% 166M 14s 49800K .......... .......... .......... .......... .......... 19% 151M 14s 49850K .......... .......... .......... .......... .......... 19% 179M 14s 49900K .......... .......... .......... .......... .......... 19% 94.6M 14s 49950K .......... .......... .......... .......... .......... 19% 112M 14s 50000K .......... .......... .......... .......... .......... 19% 138M 14s 50050K .......... .......... .......... .......... .......... 19% 326M 14s 50100K .......... .......... .......... .......... .......... 19% 130M 14s 50150K .......... .......... .......... .......... .......... 19% 418K 14s 50200K .......... .......... .......... .......... .......... 19% 110M 14s 50250K .......... .......... .......... .......... .......... 19% 174M 14s 50300K .......... .......... .......... .......... .......... 19% 201M 14s 50350K .......... .......... .......... .......... .......... 19% 42.8M 14s 50400K .......... .......... .......... .......... .......... 19% 206M 14s 50450K .......... .......... .......... .......... .......... 19% 126M 14s 50500K .......... .......... .......... .......... .......... 19% 298M 14s 50550K .......... .......... .......... .......... .......... 19% 263M 14s 50600K .......... .......... .......... .......... .......... 19% 264M 14s 50650K .......... .......... .......... .......... .......... 19% 276M 14s 50700K .......... .......... .......... .......... .......... 19% 131M 14s 50750K .......... .......... .......... .......... .......... 19% 78.5M 14s 50800K .......... .......... .......... .......... .......... 19% 138M 14s 50850K .......... .......... .......... .......... .......... 19% 130M 14s 50900K .......... .......... .......... .......... .......... 19% 124M 14s 50950K .......... .......... .......... .......... .......... 19% 143M 14s 51000K .......... .......... .......... .......... .......... 19% 194M 14s 51050K .......... .......... .......... .......... .......... 19% 171M 14s 51100K .......... .......... .......... .......... .......... 19% 141M 14s 51150K .......... .......... .......... .......... .......... 19% 127M 14s 51200K .......... .......... .......... .......... .......... 19% 372K 14s 51250K .......... .......... .......... .......... .......... 19% 96.1M 14s 51300K .......... .......... .......... .......... .......... 19% 126M 14s 51350K .......... .......... .......... .......... .......... 19% 118M 14s 51400K .......... .......... .......... .......... .......... 19% 105M 14s 51450K .......... .......... .......... .......... .......... 19% 117M 14s 51500K .......... .......... .......... .......... .......... 19% 90.1M 14s 51550K .......... .......... .......... .......... .......... 19% 76.1M 14s 51600K .......... .......... .......... .......... .......... 19% 136M 14s 51650K .......... .......... .......... .......... .......... 19% 84.2M 14s 51700K .......... .......... .......... .......... .......... 19% 133M 14s 51750K .......... .......... .......... .......... .......... 19% 107M 14s 51800K .......... .......... .......... .......... .......... 19% 132M 14s 51850K .......... .......... .......... .......... .......... 19% 156M 14s 51900K .......... .......... .......... .......... .......... 19% 198M 14s 51950K .......... .......... .......... .......... .......... 19% 153M 14s 52000K .......... .......... .......... .......... .......... 19% 68.5M 14s 52050K .......... .......... .......... .......... .......... 19% 68.3M 14s 52100K .......... .......... .......... .......... .......... 19% 70.3M 14s 52150K .......... .......... .......... .......... .......... 19% 162M 14s 52200K .......... .......... .......... .......... .......... 19% 89.4M 14s 52250K .......... .......... .......... .......... .......... 19% 198M 14s 52300K .......... .......... .......... .......... .......... 19% 84.6M 14s 52350K .......... .......... .......... .......... .......... 19% 157M 14s 52400K .......... .......... .......... .......... .......... 20% 224M 14s 52450K .......... .......... .......... .......... .......... 20% 192M 14s 52500K .......... .......... .......... .......... .......... 20% 183M 14s 52550K .......... .......... .......... .......... .......... 20% 273M 14s 52600K .......... .......... .......... .......... .......... 20% 258M 14s 52650K .......... .......... .......... .......... .......... 20% 163M 14s 52700K .......... .......... .......... .......... .......... 20% 133M 14s 52750K .......... .......... .......... .......... .......... 20% 159M 14s 52800K .......... .......... .......... .......... .......... 20% 132M 14s 52850K .......... .......... .......... .......... .......... 20% 124M 14s 52900K .......... .......... .......... .......... .......... 20% 130M 14s 52950K .......... .......... .......... .......... .......... 20% 141M 14s 53000K .......... .......... .......... .......... .......... 20% 224M 14s 53050K .......... .......... .......... .......... .......... 20% 92.0M 14s 53100K .......... .......... .......... .......... .......... 20% 178M 14s 53150K .......... .......... .......... .......... .......... 20% 218M 14s 53200K .......... .......... .......... .......... .......... 20% 173K 15s 53250K .......... .......... .......... .......... .......... 20% 158M 15s 53300K .......... .......... .......... .......... .......... 20% 54.1M 15s 53350K .......... .......... .......... .......... .......... 20% 132M 15s 53400K .......... .......... .......... .......... .......... 20% 65.7M 15s 53450K .......... .......... .......... .......... .......... 20% 72.1M 15s 53500K .......... .......... .......... .......... .......... 20% 156M 15s 53550K .......... .......... .......... .......... .......... 20% 202M 15s 53600K .......... .......... .......... .......... .......... 20% 57.2M 15s 53650K .......... .......... .......... .......... .......... 20% 163M 15s 53700K .......... .......... .......... .......... .......... 20% 36.7M 15s 53750K .......... .......... .......... .......... .......... 20% 110M 15s 53800K .......... .......... .......... .......... .......... 20% 192M 15s 53850K .......... .......... .......... .......... .......... 20% 139M 15s 53900K .......... .......... .......... .......... .......... 20% 216M 15s 53950K .......... .......... .......... .......... .......... 20% 172M 15s 54000K .......... .......... .......... .......... .......... 20% 168M 15s 54050K .......... .......... .......... .......... .......... 20% 190M 15s 54100K .......... .......... .......... .......... .......... 20% 117M 15s 54150K .......... .......... .......... .......... .......... 20% 145M 15s 54200K .......... .......... .......... .......... .......... 20% 38.7M 15s 54250K .......... .......... .......... .......... .......... 20% 1.28M 15s 54300K .......... .......... .......... .......... .......... 20% 48.6M 15s 54350K .......... .......... .......... .......... .......... 20% 128M 15s 54400K .......... .......... .......... .......... .......... 20% 87.0M 15s 54450K .......... .......... .......... .......... .......... 20% 277M 15s 54500K .......... .......... .......... .......... .......... 20% 332M 15s 54550K .......... .......... .......... .......... .......... 20% 330M 15s 54600K .......... .......... .......... .......... .......... 20% 225M 15s 54650K .......... .......... .......... .......... .......... 20% 219M 15s 54700K .......... .......... .......... .......... .......... 20% 184M 15s 54750K .......... .......... .......... .......... .......... 20% 116M 15s 54800K .......... .......... .......... .......... .......... 20% 135M 15s 54850K .......... .......... .......... .......... .......... 20% 218M 15s 54900K .......... .......... .......... .......... .......... 20% 119M 14s 54950K .......... .......... .......... .......... .......... 20% 209M 14s 55000K .......... .......... .......... .......... .......... 20% 190M 14s 55050K .......... .......... .......... .......... .......... 21% 162M 14s 55100K .......... .......... .......... .......... .......... 21% 142M 14s 55150K .......... .......... .......... .......... .......... 21% 119M 14s 55200K .......... .......... .......... .......... .......... 21% 175M 14s 55250K .......... .......... .......... .......... .......... 21% 163M 14s 55300K .......... .......... .......... .......... .......... 21% 221M 14s 55350K .......... .......... .......... .......... .......... 21% 184M 14s 55400K .......... .......... .......... .......... .......... 21% 198M 14s 55450K .......... .......... .......... .......... .......... 21% 172M 14s 55500K .......... .......... .......... .......... .......... 21% 198M 14s 55550K .......... .......... .......... .......... .......... 21% 196M 14s 55600K .......... .......... .......... .......... .......... 21% 175M 14s 55650K .......... .......... .......... .......... .......... 21% 186M 14s 55700K .......... .......... .......... .......... .......... 21% 176M 14s 55750K .......... .......... .......... .......... .......... 21% 207M 14s 55800K .......... .......... .......... .......... .......... 21% 205M 14s 55850K .......... .......... .......... .......... .......... 21% 176M 14s 55900K .......... .......... .......... .......... .......... 21% 190M 14s 55950K .......... .......... .......... .......... .......... 21% 277M 14s 56000K .......... .......... .......... .......... .......... 21% 323M 14s 56050K .......... .......... .......... .......... .......... 21% 330M 14s 56100K .......... .......... .......... .......... .......... 21% 282M 14s 56150K .......... .......... .......... .......... .......... 21% 334M 14s 56200K .......... .......... .......... .......... .......... 21% 163M 14s 56250K .......... .......... .......... .......... .......... 21% 156M 14s 56300K .......... .......... .......... .......... .......... 21% 1.83M 14s 56350K .......... .......... .......... .......... .......... 21% 81.7M 14s 56400K .......... .......... .......... .......... .......... 21% 176M 14s 56450K .......... .......... .......... .......... .......... 21% 166M 14s 56500K .......... .......... .......... .......... .......... 21% 178M 14s 56550K .......... .......... .......... .......... .......... 21% 166M 14s 56600K .......... .......... .......... .......... .......... 21% 153M 14s 56650K .......... .......... .......... .......... .......... 21% 256M 14s 56700K .......... .......... .......... .......... .......... 21% 213M 14s 56750K .......... .......... .......... .......... .......... 21% 171M 14s 56800K .......... .......... .......... .......... .......... 21% 305M 14s 56850K .......... .......... .......... .......... .......... 21% 274M 14s 56900K .......... .......... .......... .......... .......... 21% 300M 14s 56950K .......... .......... .......... .......... .......... 21% 198M 14s 57000K .......... .......... .......... .......... .......... 21% 303M 14s 57050K .......... .......... .......... .......... .......... 21% 315M 14s 57100K .......... .......... .......... .......... .......... 21% 265M 14s 57150K .......... .......... .......... .......... .......... 21% 303M 14s 57200K .......... .......... .......... .......... .......... 21% 191M 14s 57250K .......... .......... .......... .......... .......... 21% 321M 14s 57300K .......... .......... .......... .......... .......... 21% 252M 14s 57350K .......... .......... .......... .......... .......... 21% 183M 14s 57400K .......... .......... .......... .......... .......... 21% 326M 14s 57450K .......... .......... .......... .......... .......... 21% 287M 14s 57500K .......... .......... .......... .......... .......... 21% 337M 14s 57550K .......... .......... .......... .......... .......... 21% 334M 14s 57600K .......... .......... .......... .......... .......... 21% 284M 14s 57650K .......... .......... .......... .......... .......... 22% 326M 14s 57700K .......... .......... .......... .......... .......... 22% 292M 14s 57750K .......... .......... .......... .......... .......... 22% 339M 14s 57800K .......... .......... .......... .......... .......... 22% 334M 14s 57850K .......... .......... .......... .......... .......... 22% 289M 14s 57900K .......... .......... .......... .......... .......... 22% 330M 14s 57950K .......... .......... .......... .......... .......... 22% 291M 14s 58000K .......... .......... .......... .......... .......... 22% 341M 14s 58050K .......... .......... .......... .......... .......... 22% 317M 14s 58100K .......... .......... .......... .......... .......... 22% 282M 14s 58150K .......... .......... .......... .......... .......... 22% 328M 14s 58200K .......... .......... .......... .......... .......... 22% 289M 14s 58250K .......... .......... .......... .......... .......... 22% 337M 14s 58300K .......... .......... .......... .......... .......... 22% 332M 14s 58350K .......... .......... .......... .......... .......... 22% 5.82M 14s 58400K .......... .......... .......... .......... .......... 22% 126M 14s 58450K .......... .......... .......... .......... .......... 22% 163M 14s 58500K .......... .......... .......... .......... .......... 22% 147M 14s 58550K .......... .......... .......... .......... .......... 22% 234M 14s 58600K .......... .......... .......... .......... .......... 22% 88.9M 14s 58650K .......... .......... .......... .......... .......... 22% 133M 13s 58700K .......... .......... .......... .......... .......... 22% 99.0M 13s 58750K .......... .......... .......... .......... .......... 22% 234M 13s 58800K .......... .......... .......... .......... .......... 22% 195M 13s 58850K .......... .......... .......... .......... .......... 22% 82.2M 13s 58900K .......... .......... .......... .......... .......... 22% 257M 13s 58950K .......... .......... .......... .......... .......... 22% 139M 13s 59000K .......... .......... .......... .......... .......... 22% 160M 13s 59050K .......... .......... .......... .......... .......... 22% 284M 13s 59100K .......... .......... .......... .......... .......... 22% 119M 13s 59150K .......... .......... .......... .......... .......... 22% 161M 13s 59200K .......... .......... .......... .......... .......... 22% 162M 13s 59250K .......... .......... .......... .......... .......... 22% 193M 13s 59300K .......... .......... .......... .......... .......... 22% 213M 13s 59350K .......... .......... .......... .......... .......... 22% 1.75M 13s 59400K .......... .......... .......... .......... .......... 22% 147M 13s 59450K .......... .......... .......... .......... .......... 22% 230M 13s 59500K .......... .......... .......... .......... .......... 22% 134M 13s 59550K .......... .......... .......... .......... .......... 22% 72.9M 13s 59600K .......... .......... .......... .......... .......... 22% 180M 13s 59650K .......... .......... .......... .......... .......... 22% 177M 13s 59700K .......... .......... .......... .......... .......... 22% 155M 13s 59750K .......... .......... .......... .......... .......... 22% 166M 13s 59800K .......... .......... .......... .......... .......... 22% 171M 13s 59850K .......... .......... .......... .......... .......... 22% 167M 13s 59900K .......... .......... .......... .......... .......... 22% 157M 13s 59950K .......... .......... .......... .......... .......... 22% 186M 13s 60000K .......... .......... .......... .......... .......... 22% 217M 13s 60050K .......... .......... .......... .......... .......... 22% 233M 13s 60100K .......... .......... .......... .......... .......... 22% 200M 13s 60150K .......... .......... .......... .......... .......... 22% 235M 13s 60200K .......... .......... .......... .......... .......... 22% 203M 13s 60250K .......... .......... .......... .......... .......... 22% 207M 13s 60300K .......... .......... .......... .......... .......... 23% 206M 13s 60350K .......... .......... .......... .......... .......... 23% 176M 13s 60400K .......... .......... .......... .......... .......... 23% 147M 13s 60450K .......... .......... .......... .......... .......... 23% 180M 13s 60500K .......... .......... .......... .......... .......... 23% 211M 13s 60550K .......... .......... .......... .......... .......... 23% 210M 13s 60600K .......... .......... .......... .......... .......... 23% 176M 13s 60650K .......... .......... .......... .......... .......... 23% 210M 13s 60700K .......... .......... .......... .......... .......... 23% 182M 13s 60750K .......... .......... .......... .......... .......... 23% 5.36M 13s 60800K .......... .......... .......... .......... .......... 23% 87.7M 13s 60850K .......... .......... .......... .......... .......... 23% 170M 13s 60900K .......... .......... .......... .......... .......... 23% 161M 13s 60950K .......... .......... .......... .......... .......... 23% 110M 13s 61000K .......... .......... .......... .......... .......... 23% 192M 13s 61050K .......... .......... .......... .......... .......... 23% 244M 13s 61100K .......... .......... .......... .......... .......... 23% 229M 13s 61150K .......... .......... .......... .......... .......... 23% 284M 13s 61200K .......... .......... .......... .......... .......... 23% 198M 13s 61250K .......... .......... .......... .......... .......... 23% 132M 13s 61300K .......... .......... .......... .......... .......... 23% 209M 13s 61350K .......... .......... .......... .......... .......... 23% 171M 13s 61400K .......... .......... .......... .......... .......... 23% 95.0M 13s 61450K .......... .......... .......... .......... .......... 23% 221M 13s 61500K .......... .......... .......... .......... .......... 23% 234M 13s 61550K .......... .......... .......... .......... .......... 23% 210M 13s 61600K .......... .......... .......... .......... .......... 23% 213M 13s 61650K .......... .......... .......... .......... .......... 23% 146M 13s 61700K .......... .......... .......... .......... .......... 23% 108M 13s 61750K .......... .......... .......... .......... .......... 23% 151M 13s 61800K .......... .......... .......... .......... .......... 23% 1.86M 13s 61850K .......... .......... .......... .......... .......... 23% 99.2M 13s 61900K .......... .......... .......... .......... .......... 23% 313M 13s 61950K .......... .......... .......... .......... .......... 23% 268M 13s 62000K .......... .......... .......... .......... .......... 23% 134M 13s 62050K .......... .......... .......... .......... .......... 23% 249M 13s 62100K .......... .......... .......... .......... .......... 23% 298M 13s 62150K .......... .......... .......... .......... .......... 23% 344M 13s 62200K .......... .......... .......... .......... .......... 23% 298M 13s 62250K .......... .......... .......... .......... .......... 23% 349M 13s 62300K .......... .......... .......... .......... .......... 23% 337M 13s 62350K .......... .......... .......... .......... .......... 23% 300M 13s 62400K .......... .......... .......... .......... .......... 23% 346M 13s 62450K .......... .......... .......... .......... .......... 23% 224M 13s 62500K .......... .......... .......... .......... .......... 23% 332M 13s 62550K .......... .......... .......... .......... .......... 23% 252M 13s 62600K .......... .......... .......... .......... .......... 23% 296M 13s 62650K .......... .......... .......... .......... .......... 23% 349M 13s 62700K .......... .......... .......... .......... .......... 23% 300M 13s 62750K .......... .......... .......... .......... .......... 23% 349M 13s 62800K .......... .......... .......... .......... .......... 23% 6.17M 13s 62850K .......... .......... .......... .......... .......... 23% 89.9M 13s 62900K .......... .......... .......... .......... .......... 24% 94.1M 13s 62950K .......... .......... .......... .......... .......... 24% 149M 13s 63000K .......... .......... .......... .......... .......... 24% 124M 13s 63050K .......... .......... .......... .......... .......... 24% 178M 13s 63100K .......... .......... .......... .......... .......... 24% 173M 13s 63150K .......... .......... .......... .......... .......... 24% 212M 13s 63200K .......... .......... .......... .......... .......... 24% 113M 13s 63250K .......... .......... .......... .......... .......... 24% 1.78M 13s 63300K .......... .......... .......... .......... .......... 24% 109M 13s 63350K .......... .......... .......... .......... .......... 24% 157M 13s 63400K .......... .......... .......... .......... .......... 24% 182M 13s 63450K .......... .......... .......... .......... .......... 24% 467K 13s 63500K .......... .......... .......... .......... .......... 24% 233M 13s 63550K .......... .......... .......... .......... .......... 24% 284M 13s 63600K .......... .......... .......... .......... .......... 24% 260M 13s 63650K .......... .......... .......... .......... .......... 24% 321M 13s 63700K .......... .......... .......... .......... .......... 24% 60.7M 13s 63750K .......... .......... .......... .......... .......... 24% 101M 13s 63800K .......... .......... .......... .......... .......... 24% 160M 13s 63850K .......... .......... .......... .......... .......... 24% 125M 13s 63900K .......... .......... .......... .......... .......... 24% 134M 13s 63950K .......... .......... .......... .......... .......... 24% 174M 13s 64000K .......... .......... .......... .......... .......... 24% 155M 13s 64050K .......... .......... .......... .......... .......... 24% 68.6M 13s 64100K .......... .......... .......... .......... .......... 24% 184M 13s 64150K .......... .......... .......... .......... .......... 24% 319M 13s 64200K .......... .......... .......... .......... .......... 24% 277M 13s 64250K .......... .......... .......... .......... .......... 24% 233M 13s 64300K .......... .......... .......... .......... .......... 24% 328M 13s 64350K .......... .......... .......... .......... .......... 24% 205M 13s 64400K .......... .......... .......... .......... .......... 24% 242M 13s 64450K .......... .......... .......... .......... .......... 24% 267M 13s 64500K .......... .......... .......... .......... .......... 24% 67.0M 13s 64550K .......... .......... .......... .......... .......... 24% 110M 13s 64600K .......... .......... .......... .......... .......... 24% 74.2M 13s 64650K .......... .......... .......... .......... .......... 24% 115M 13s 64700K .......... .......... .......... .......... .......... 24% 129M 13s 64750K .......... .......... .......... .......... .......... 24% 61.0M 13s 64800K .......... .......... .......... .......... .......... 24% 153M 13s 64850K .......... .......... .......... .......... .......... 24% 92.7M 13s 64900K .......... .......... .......... .......... .......... 24% 157M 13s 64950K .......... .......... .......... .......... .......... 24% 80.6M 13s 65000K .......... .......... .......... .......... .......... 24% 108M 13s 65050K .......... .......... .......... .......... .......... 24% 173M 13s 65100K .......... .......... .......... .......... .......... 24% 233M 13s 65150K .......... .......... .......... .......... .......... 24% 214M 12s 65200K .......... .......... .......... .......... .......... 24% 192M 12s 65250K .......... .......... .......... .......... .......... 24% 80.8M 12s 65300K .......... .......... .......... .......... .......... 24% 260M 12s 65350K .......... .......... .......... .......... .......... 24% 147M 12s 65400K .......... .......... .......... .......... .......... 24% 136M 12s 65450K .......... .......... .......... .......... .......... 24% 158M 12s 65500K .......... .......... .......... .......... .......... 24% 108M 12s 65550K .......... .......... .......... .......... .......... 25% 92.3M 12s 65600K .......... .......... .......... .......... .......... 25% 169M 12s 65650K .......... .......... .......... .......... .......... 25% 249M 12s 65700K .......... .......... .......... .......... .......... 25% 128M 12s 65750K .......... .......... .......... .......... .......... 25% 170M 12s 65800K .......... .......... .......... .......... .......... 25% 192M 12s 65850K .......... .......... .......... .......... .......... 25% 168M 12s 65900K .......... .......... .......... .......... .......... 25% 163M 12s 65950K .......... .......... .......... .......... .......... 25% 221M 12s 66000K .......... .......... .......... .......... .......... 25% 346M 12s 66050K .......... .......... .......... .......... .......... 25% 341M 12s 66100K .......... .......... .......... .......... .......... 25% 294M 12s 66150K .......... .......... .......... .......... .......... 25% 344M 12s 66200K .......... .......... .......... .......... .......... 25% 292M 12s 66250K .......... .......... .......... .......... .......... 25% 344M 12s 66300K .......... .......... .......... .......... .......... 25% 344M 12s 66350K .......... .......... .......... .......... .......... 25% 300M 12s 66400K .......... .......... .......... .......... .......... 25% 344M 12s 66450K .......... .......... .......... .......... .......... 25% 298M 12s 66500K .......... .......... .......... .......... .......... 25% 337M 12s 66550K .......... .......... .......... .......... .......... 25% 207K 13s 66600K .......... .......... .......... .......... .......... 25% 147M 13s 66650K .......... .......... .......... .......... .......... 25% 180M 13s 66700K .......... .......... .......... .......... .......... 25% 108M 13s 66750K .......... .......... .......... .......... .......... 25% 101M 13s 66800K .......... .......... .......... .......... .......... 25% 172M 13s 66850K .......... .......... .......... .......... .......... 25% 198M 13s 66900K .......... .......... .......... .......... .......... 25% 231M 13s 66950K .......... .......... .......... .......... .......... 25% 198M 13s 67000K .......... .......... .......... .......... .......... 25% 231M 13s 67050K .......... .......... .......... .......... .......... 25% 234M 13s 67100K .......... .......... .......... .......... .......... 25% 202M 13s 67150K .......... .......... .......... .......... .......... 25% 238M 13s 67200K .......... .......... .......... .......... .......... 25% 201M 13s 67250K .......... .......... .......... .......... .......... 25% 234M 13s 67300K .......... .......... .......... .......... .......... 25% 237M 13s 67350K .......... .......... .......... .......... .......... 25% 203M 13s 67400K .......... .......... .......... .......... .......... 25% 230M 13s 67450K .......... .......... .......... .......... .......... 25% 189M 13s 67500K .......... .......... .......... .......... .......... 25% 111M 13s 67550K .......... .......... .......... .......... .......... 25% 70.3M 13s 67600K .......... .......... .......... .......... .......... 25% 118M 13s 67650K .......... .......... .......... .......... .......... 25% 195M 13s 67700K .......... .......... .......... .......... .......... 25% 189M 13s 67750K .......... .......... .......... .......... .......... 25% 192M 13s 67800K .......... .......... .......... .......... .......... 25% 212M 13s 67850K .......... .......... .......... .......... .......... 25% 163M 13s 67900K .......... .......... .......... .......... .......... 25% 224M 13s 67950K .......... .......... .......... .......... .......... 25% 203M 13s 68000K .......... .......... .......... .......... .......... 25% 233M 13s 68050K .......... .......... .......... .......... .......... 25% 235M 13s 68100K .......... .......... .......... .......... .......... 25% 200M 13s 68150K .......... .......... .......... .......... .......... 26% 235M 12s 68200K .......... .......... .......... .......... .......... 26% 163M 12s 68250K .......... .......... .......... .......... .......... 26% 230M 12s 68300K .......... .......... .......... .......... .......... 26% 164M 12s 68350K .......... .......... .......... .......... .......... 26% 173M 12s 68400K .......... .......... .......... .......... .......... 26% 218M 12s 68450K .......... .......... .......... .......... .......... 26% 199M 12s 68500K .......... .......... .......... .......... .......... 26% 198M 12s 68550K .......... .......... .......... .......... .......... 26% 224M 12s 68600K .......... .......... .......... .......... .......... 26% 393K 13s 68650K .......... .......... .......... .......... .......... 26% 219M 13s 68700K .......... .......... .......... .......... .......... 26% 198M 13s 68750K .......... .......... .......... .......... .......... 26% 194M 13s 68800K .......... .......... .......... .......... .......... 26% 174M 13s 68850K .......... .......... .......... .......... .......... 26% 135M 13s 68900K .......... .......... .......... .......... .......... 26% 106M 13s 68950K .......... .......... .......... .......... .......... 26% 100M 13s 69000K .......... .......... .......... .......... .......... 26% 80.0M 13s 69050K .......... .......... .......... .......... .......... 26% 58.4M 13s 69100K .......... .......... .......... .......... .......... 26% 44.5M 13s 69150K .......... .......... .......... .......... .......... 26% 77.3M 13s 69200K .......... .......... .......... .......... .......... 26% 73.1M 13s 69250K .......... .......... .......... .......... .......... 26% 110M 13s 69300K .......... .......... .......... .......... .......... 26% 47.6M 13s 69350K .......... .......... .......... .......... .......... 26% 188M 13s 69400K .......... .......... .......... .......... .......... 26% 238M 13s 69450K .......... .......... .......... .......... .......... 26% 205M 13s 69500K .......... .......... .......... .......... .......... 26% 239M 13s 69550K .......... .......... .......... .......... .......... 26% 238M 13s 69600K .......... .......... .......... .......... .......... 26% 133M 13s 69650K .......... .......... .......... .......... .......... 26% 189M 13s 69700K .......... .......... .......... .......... .......... 26% 203M 13s 69750K .......... .......... .......... .......... .......... 26% 326M 12s 69800K .......... .......... .......... .......... .......... 26% 119M 12s 69850K .......... .......... .......... .......... .......... 26% 106M 12s 69900K .......... .......... .......... .......... .......... 26% 202M 12s 69950K .......... .......... .......... .......... .......... 26% 180M 12s 70000K .......... .......... .......... .......... .......... 26% 184M 12s 70050K .......... .......... .......... .......... .......... 26% 243M 12s 70100K .......... .......... .......... .......... .......... 26% 241M 12s 70150K .......... .......... .......... .......... .......... 26% 230M 12s 70200K .......... .......... .......... .......... .......... 26% 181M 12s 70250K .......... .......... .......... .......... .......... 26% 184M 12s 70300K .......... .......... .......... .......... .......... 26% 182M 12s 70350K .......... .......... .......... .......... .......... 26% 198M 12s 70400K .......... .......... .......... .......... .......... 26% 214M 12s 70450K .......... .......... .......... .......... .......... 26% 192M 12s 70500K .......... .......... .......... .......... .......... 26% 198M 12s 70550K .......... .......... .......... .......... .......... 26% 184M 12s 70600K .......... .......... .......... .......... .......... 26% 153M 12s 70650K .......... .......... .......... .......... .......... 26% 131M 12s 70700K .......... .......... .......... .......... .......... 26% 161M 12s 70750K .......... .......... .......... .......... .......... 27% 120M 12s 70800K .......... .......... .......... .......... .......... 27% 217M 12s 70850K .......... .......... .......... .......... .......... 27% 161M 12s 70900K .......... .......... .......... .......... .......... 27% 174M 12s 70950K .......... .......... .......... .......... .......... 27% 120M 12s 71000K .......... .......... .......... .......... .......... 27% 104M 12s 71050K .......... .......... .......... .......... .......... 27% 85.4M 12s 71100K .......... .......... .......... .......... .......... 27% 82.3M 12s 71150K .......... .......... .......... .......... .......... 27% 101M 12s 71200K .......... .......... .......... .......... .......... 27% 172M 12s 71250K .......... .......... .......... .......... .......... 27% 244M 12s 71300K .......... .......... .......... .......... .......... 27% 256M 12s 71350K .......... .......... .......... .......... .......... 27% 224M 12s 71400K .......... .......... .......... .......... .......... 27% 256M 12s 71450K .......... .......... .......... .......... .......... 27% 220M 12s 71500K .......... .......... .......... .......... .......... 27% 245M 12s 71550K .......... .......... .......... .......... .......... 27% 337M 12s 71600K .......... .......... .......... .......... .......... 27% 150M 12s 71650K .......... .......... .......... .......... .......... 27% 647K 12s 71700K .......... .......... .......... .......... .......... 27% 163M 12s 71750K .......... .......... .......... .......... .......... 27% 207M 12s 71800K .......... .......... .......... .......... .......... 27% 223M 12s 71850K .......... .......... .......... .......... .......... 27% 196M 12s 71900K .......... .......... .......... .......... .......... 27% 194M 12s 71950K .......... .......... .......... .......... .......... 27% 123M 12s 72000K .......... .......... .......... .......... .......... 27% 166M 12s 72050K .......... .......... .......... .......... .......... 27% 207M 12s 72100K .......... .......... .......... .......... .......... 27% 233M 12s 72150K .......... .......... .......... .......... .......... 27% 224M 12s 72200K .......... .......... .......... .......... .......... 27% 203M 12s 72250K .......... .......... .......... .......... .......... 27% 282M 12s 72300K .......... .......... .......... .......... .......... 27% 223M 12s 72350K .......... .......... .......... .......... .......... 27% 181M 12s 72400K .......... .......... .......... .......... .......... 27% 241M 12s 72450K .......... .......... .......... .......... .......... 27% 164M 12s 72500K .......... .......... .......... .......... .......... 27% 210M 12s 72550K .......... .......... .......... .......... .......... 27% 210M 12s 72600K .......... .......... .......... .......... .......... 27% 178M 12s 72650K .......... .......... .......... .......... .......... 27% 161M 12s 72700K .......... .......... .......... .......... .......... 27% 60.6M 12s 72750K .......... .......... .......... .......... .......... 27% 323M 12s 72800K .......... .......... .......... .......... .......... 27% 332M 12s 72850K .......... .......... .......... .......... .......... 27% 291M 12s 72900K .......... .......... .......... .......... .......... 27% 339M 12s 72950K .......... .......... .......... .......... .......... 27% 289M 12s 73000K .......... .......... .......... .......... .......... 27% 344M 12s 73050K .......... .......... .......... .......... .......... 27% 344M 12s 73100K .......... .......... .......... .......... .......... 27% 296M 12s 73150K .......... .......... .......... .......... .......... 27% 339M 12s 73200K .......... .......... .......... .......... .......... 27% 282M 12s 73250K .......... .......... .......... .......... .......... 27% 326M 12s 73300K .......... .......... .......... .......... .......... 27% 346M 12s 73350K .......... .......... .......... .......... .......... 27% 298M 12s 73400K .......... .......... .......... .......... .......... 28% 344M 12s 73450K .......... .......... .......... .......... .......... 28% 289M 12s 73500K .......... .......... .......... .......... .......... 28% 346M 12s 73550K .......... .......... .......... .......... .......... 28% 344M 12s 73600K .......... .......... .......... .......... .......... 28% 298M 12s 73650K .......... .......... .......... .......... .......... 28% 239M 12s 73700K .......... .......... .......... .......... .......... 28% 6.06M 12s 73750K .......... .......... .......... .......... .......... 28% 118M 12s 73800K .......... .......... .......... .......... .......... 28% 160M 12s 73850K .......... .......... .......... .......... .......... 28% 176M 12s 73900K .......... .......... .......... .......... .......... 28% 173M 12s 73950K .......... .......... .......... .......... .......... 28% 139M 12s 74000K .......... .......... .......... .......... .......... 28% 167M 12s 74050K .......... .......... .......... .......... .......... 28% 170M 12s 74100K .......... .......... .......... .......... .......... 28% 180M 12s 74150K .......... .......... .......... .......... .......... 28% 143M 12s 74200K .......... .......... .......... .......... .......... 28% 101M 12s 74250K .......... .......... .......... .......... .......... 28% 136M 12s 74300K .......... .......... .......... .......... .......... 28% 186M 12s 74350K .......... .......... .......... .......... .......... 28% 157M 12s 74400K .......... .......... .......... .......... .......... 28% 164M 12s 74450K .......... .......... .......... .......... .......... 28% 129M 12s 74500K .......... .......... .......... .......... .......... 28% 193M 12s 74550K .......... .......... .......... .......... .......... 28% 155M 12s 74600K .......... .......... .......... .......... .......... 28% 130M 12s 74650K .......... .......... .......... .......... .......... 28% 176M 12s 74700K .......... .......... .......... .......... .......... 28% 1.82M 12s 74750K .......... .......... .......... .......... .......... 28% 1.38M 12s 74800K .......... .......... .......... .......... .......... 28% 62.4M 12s 74850K .......... .......... .......... .......... .......... 28% 182M 12s 74900K .......... .......... .......... .......... .......... 28% 328M 12s 74950K .......... .......... .......... .......... .......... 28% 282M 12s 75000K .......... .......... .......... .......... .......... 28% 159M 12s 75050K .......... .......... .......... .......... .......... 28% 227M 12s 75100K .......... .......... .......... .......... .......... 28% 145M 12s 75150K .......... .......... .......... .......... .......... 28% 195M 12s 75200K .......... .......... .......... .......... .......... 28% 173M 12s 75250K .......... .......... .......... .......... .......... 28% 218M 12s 75300K .......... .......... .......... .......... .......... 28% 142M 12s 75350K .......... .......... .......... .......... .......... 28% 204M 12s 75400K .......... .......... .......... .......... .......... 28% 166M 12s 75450K .......... .......... .......... .......... .......... 28% 182M 12s 75500K .......... .......... .......... .......... .......... 28% 224M 12s 75550K .......... .......... .......... .......... .......... 28% 161M 12s 75600K .......... .......... .......... .......... .......... 28% 195M 12s 75650K .......... .......... .......... .......... .......... 28% 187M 12s 75700K .......... .......... .......... .......... .......... 28% 148M 12s 75750K .......... .......... .......... .......... .......... 28% 290K 12s 75800K .......... .......... .......... .......... .......... 28% 185M 12s 75850K .......... .......... .......... .......... .......... 28% 103M 12s 75900K .......... .......... .......... .......... .......... 28% 133M 12s 75950K .......... .......... .......... .......... .......... 28% 79.3M 12s 76000K .......... .......... .......... .......... .......... 29% 68.3M 12s 76050K .......... .......... .......... .......... .......... 29% 188M 12s 76100K .......... .......... .......... .......... .......... 29% 61.2M 12s 76150K .......... .......... .......... .......... .......... 29% 93.2M 12s 76200K .......... .......... .......... .......... .......... 29% 166M 12s 76250K .......... .......... .......... .......... .......... 29% 197M 12s 76300K .......... .......... .......... .......... .......... 29% 217M 12s 76350K .......... .......... .......... .......... .......... 29% 192M 12s 76400K .......... .......... .......... .......... .......... 29% 211M 12s 76450K .......... .......... .......... .......... .......... 29% 174M 12s 76500K .......... .......... .......... .......... .......... 29% 211M 12s 76550K .......... .......... .......... .......... .......... 29% 192M 12s 76600K .......... .......... .......... .......... .......... 29% 128M 12s 76650K .......... .......... .......... .......... .......... 29% 228M 12s 76700K .......... .......... .......... .......... .......... 29% 58.2M 12s 76750K .......... .......... .......... .......... .......... 29% 27.6M 12s 76800K .......... .......... .......... .......... .......... 29% 73.2M 12s 76850K .......... .......... .......... .......... .......... 29% 1.51M 12s 76900K .......... .......... .......... .......... .......... 29% 207M 12s 76950K .......... .......... .......... .......... .......... 29% 173M 12s 77000K .......... .......... .......... .......... .......... 29% 150M 12s 77050K .......... .......... .......... .......... .......... 29% 61.0M 12s 77100K .......... .......... .......... .......... .......... 29% 173M 12s 77150K .......... .......... .......... .......... .......... 29% 187M 12s 77200K .......... .......... .......... .......... .......... 29% 182M 12s 77250K .......... .......... .......... .......... .......... 29% 257M 12s 77300K .......... .......... .......... .......... .......... 29% 270M 12s 77350K .......... .......... .......... .......... .......... 29% 184M 12s 77400K .......... .......... .......... .......... .......... 29% 216M 12s 77450K .......... .......... .......... .......... .......... 29% 207M 12s 77500K .......... .......... .......... .......... .......... 29% 309M 12s 77550K .......... .......... .......... .......... .......... 29% 256M 12s 77600K .......... .......... .......... .......... .......... 29% 284M 12s 77650K .......... .......... .......... .......... .......... 29% 233M 12s 77700K .......... .......... .......... .......... .......... 29% 181M 12s 77750K .......... .......... .......... .......... .......... 29% 250M 12s 77800K .......... .......... .......... .......... .......... 29% 233M 12s 77850K .......... .......... .......... .......... .......... 29% 190M 12s 77900K .......... .......... .......... .......... .......... 29% 210M 12s 77950K .......... .......... .......... .......... .......... 29% 190M 12s 78000K .......... .......... .......... .......... .......... 29% 206M 12s 78050K .......... .......... .......... .......... .......... 29% 101M 12s 78100K .......... .......... .......... .......... .......... 29% 114M 12s 78150K .......... .......... .......... .......... .......... 29% 217M 12s 78200K .......... .......... .......... .......... .......... 29% 135M 12s 78250K .......... .......... .......... .......... .......... 29% 205M 12s 78300K .......... .......... .......... .......... .......... 29% 199M 12s 78350K .......... .......... .......... .......... .......... 29% 219M 12s 78400K .......... .......... .......... .......... .......... 29% 219M 12s 78450K .......... .......... .......... .......... .......... 29% 176M 12s 78500K .......... .......... .......... .......... .......... 29% 237M 12s 78550K .......... .......... .......... .......... .......... 29% 221M 12s 78600K .......... .......... .......... .......... .......... 29% 114M 12s 78650K .......... .......... .......... .......... .......... 30% 209M 12s 78700K .......... .......... .......... .......... .......... 30% 237M 11s 78750K .......... .......... .......... .......... .......... 30% 231M 11s 78800K .......... .......... .......... .......... .......... 30% 257M 11s 78850K .......... .......... .......... .......... .......... 30% 93.4M 11s 78900K .......... .......... .......... .......... .......... 30% 292M 11s 78950K .......... .......... .......... .......... .......... 30% 261M 11s 79000K .......... .......... .......... .......... .......... 30% 271M 11s 79050K .......... .......... .......... .......... .......... 30% 122M 11s 79100K .......... .......... .......... .......... .......... 30% 2.11M 11s 79150K .......... .......... .......... .......... .......... 30% 185M 11s 79200K .......... .......... .......... .......... .......... 30% 117M 11s 79250K .......... .......... .......... .......... .......... 30% 317M 11s 79300K .......... .......... .......... .......... .......... 30% 326M 11s 79350K .......... .......... .......... .......... .......... 30% 253M 11s 79400K .......... .......... .......... .......... .......... 30% 2.03M 11s 79450K .......... .......... .......... .......... .......... 30% 172M 11s 79500K .......... .......... .......... .......... .......... 30% 170M 11s 79550K .......... .......... .......... .......... .......... 30% 130M 11s 79600K .......... .......... .......... .......... .......... 30% 100M 11s 79650K .......... .......... .......... .......... .......... 30% 136M 11s 79700K .......... .......... .......... .......... .......... 30% 137M 11s 79750K .......... .......... .......... .......... .......... 30% 177M 11s 79800K .......... .......... .......... .......... .......... 30% 138M 11s 79850K .......... .......... .......... .......... .......... 30% 5.74M 11s 79900K .......... .......... .......... .......... .......... 30% 77.8M 11s 79950K .......... .......... .......... .......... .......... 30% 37.9M 11s 80000K .......... .......... .......... .......... .......... 30% 11.9M 11s 80050K .......... .......... .......... .......... .......... 30% 17.2M 11s 80100K .......... .......... .......... .......... .......... 30% 17.3M 11s 80150K .......... .......... .......... .......... .......... 30% 29.4M 11s 80200K .......... .......... .......... .......... .......... 30% 26.1M 11s 80250K .......... .......... .......... .......... .......... 30% 81.0M 11s 80300K .......... .......... .......... .......... .......... 30% 330M 11s 80350K .......... .......... .......... .......... .......... 30% 292M 11s 80400K .......... .......... .......... .......... .......... 30% 337M 11s 80450K .......... .......... .......... .......... .......... 30% 292M 11s 80500K .......... .......... .......... .......... .......... 30% 344M 11s 80550K .......... .......... .......... .......... .......... 30% 341M 11s 80600K .......... .......... .......... .......... .......... 30% 49.3M 11s 80650K .......... .......... .......... .......... .......... 30% 68.0M 11s 80700K .......... .......... .......... .......... .......... 30% 77.0M 11s 80750K .......... .......... .......... .......... .......... 30% 173M 11s 80800K .......... .......... .......... .......... .......... 30% 210M 11s 80850K .......... .......... .......... .......... .......... 30% 2.14M 11s 80900K .......... .......... .......... .......... .......... 30% 69.7M 11s 80950K .......... .......... .......... .......... .......... 30% 82.2M 11s 81000K .......... .......... .......... .......... .......... 30% 156M 11s 81050K .......... .......... .......... .......... .......... 30% 108M 11s 81100K .......... .......... .......... .......... .......... 30% 142M 11s 81150K .......... .......... .......... .......... .......... 30% 315M 11s 81200K .......... .......... .......... .......... .......... 30% 217M 11s 81250K .......... .......... .......... .......... .......... 31% 268M 11s 81300K .......... .......... .......... .......... .......... 31% 221M 11s 81350K .......... .......... .......... .......... .......... 31% 101M 11s 81400K .......... .......... .......... .......... .......... 31% 292M 11s 81450K .......... .......... .......... .......... .......... 31% 252M 11s 81500K .......... .......... .......... .......... .......... 31% 206M 11s 81550K .......... .......... .......... .......... .......... 31% 243M 11s 81600K .......... .......... .......... .......... .......... 31% 184M 11s 81650K .......... .......... .......... .......... .......... 31% 294M 11s 81700K .......... .......... .......... .......... .......... 31% 207M 11s 81750K .......... .......... .......... .......... .......... 31% 210M 11s 81800K .......... .......... .......... .......... .......... 31% 222M 11s 81850K .......... .......... .......... .......... .......... 31% 243M 11s 81900K .......... .......... .......... .......... .......... 31% 7.17M 11s 81950K .......... .......... .......... .......... .......... 31% 1.90M 11s 82000K .......... .......... .......... .......... .......... 31% 298M 11s 82050K .......... .......... .......... .......... .......... 31% 47.6M 11s 82100K .......... .......... .......... .......... .......... 31% 10.9M 11s 82150K .......... .......... .......... .......... .......... 31% 38.2M 11s 82200K .......... .......... .......... .......... .......... 31% 173M 11s 82250K .......... .......... .......... .......... .......... 31% 328M 11s 82300K .......... .......... .......... .......... .......... 31% 174M 11s 82350K .......... .......... .......... .......... .......... 31% 115M 11s 82400K .......... .......... .......... .......... .......... 31% 194M 11s 82450K .......... .......... .......... .......... .......... 31% 172M 11s 82500K .......... .......... .......... .......... .......... 31% 46.8M 11s 82550K .......... .......... .......... .......... .......... 31% 294M 11s 82600K .......... .......... .......... .......... .......... 31% 165M 11s 82650K .......... .......... .......... .......... .......... 31% 305M 11s 82700K .......... .......... .......... .......... .......... 31% 212M 11s 82750K .......... .......... .......... .......... .......... 31% 187M 11s 82800K .......... .......... .......... .......... .......... 31% 300M 11s 82850K .......... .......... .......... .......... .......... 31% 270M 11s 82900K .......... .......... .......... .......... .......... 31% 234M 11s 82950K .......... .......... .......... .......... .......... 31% 289M 11s 83000K .......... .......... .......... .......... .......... 31% 337M 11s 83050K .......... .......... .......... .......... .......... 31% 339M 11s 83100K .......... .......... .......... .......... .......... 31% 296M 11s 83150K .......... .......... .......... .......... .......... 31% 346M 11s 83200K .......... .......... .......... .......... .......... 31% 294M 11s 83250K .......... .......... .......... .......... .......... 31% 337M 11s 83300K .......... .......... .......... .......... .......... 31% 344M 11s 83350K .......... .......... .......... .......... .......... 31% 282M 11s 83400K .......... .......... .......... .......... .......... 31% 341M 11s 83450K .......... .......... .......... .......... .......... 31% 282M 11s 83500K .......... .......... .......... .......... .......... 31% 48.8M 11s 83550K .......... .......... .......... .......... .......... 31% 202M 11s 83600K .......... .......... .......... .......... .......... 31% 174M 11s 83650K .......... .......... .......... .......... .......... 31% 209M 11s 83700K .......... .......... .......... .......... .......... 31% 109M 11s 83750K .......... .......... .......... .......... .......... 31% 258M 11s 83800K .......... .......... .......... .......... .......... 31% 188M 11s 83850K .......... .......... .......... .......... .......... 31% 174M 11s 83900K .......... .......... .......... .......... .......... 32% 301M 11s 83950K .......... .......... .......... .......... .......... 32% 182K 11s 84000K .......... .......... .......... .......... .......... 32% 121M 11s 84050K .......... .......... .......... .......... .......... 32% 158M 11s 84100K .......... .......... .......... .......... .......... 32% 129M 11s 84150K .......... .......... .......... .......... .......... 32% 121M 11s 84200K .......... .......... .......... .......... .......... 32% 101M 11s 84250K .......... .......... .......... .......... .......... 32% 239M 11s 84300K .......... .......... .......... .......... .......... 32% 70.6M 11s 84350K .......... .......... .......... .......... .......... 32% 116M 11s 84400K .......... .......... .......... .......... .......... 32% 153M 11s 84450K .......... .......... .......... .......... .......... 32% 170M 11s 84500K .......... .......... .......... .......... .......... 32% 131M 11s 84550K .......... .......... .......... .......... .......... 32% 78.4M 11s 84600K .......... .......... .......... .......... .......... 32% 66.8M 11s 84650K .......... .......... .......... .......... .......... 32% 268M 11s 84700K .......... .......... .......... .......... .......... 32% 245M 11s 84750K .......... .......... .......... .......... .......... 32% 48.5M 11s 84800K .......... .......... .......... .......... .......... 32% 135M 11s 84850K .......... .......... .......... .......... .......... 32% 61.3M 11s 84900K .......... .......... .......... .......... .......... 32% 149M 11s 84950K .......... .......... .......... .......... .......... 32% 79.0M 11s 85000K .......... .......... .......... .......... .......... 32% 195M 11s 85050K .......... .......... .......... .......... .......... 32% 215M 11s 85100K .......... .......... .......... .......... .......... 32% 143M 11s 85150K .......... .......... .......... .......... .......... 32% 201M 11s 85200K .......... .......... .......... .......... .......... 32% 182M 11s 85250K .......... .......... .......... .......... .......... 32% 218M 11s 85300K .......... .......... .......... .......... .......... 32% 214M 11s 85350K .......... .......... .......... .......... .......... 32% 130M 11s 85400K .......... .......... .......... .......... .......... 32% 82.3M 11s 85450K .......... .......... .......... .......... .......... 32% 77.9M 11s 85500K .......... .......... .......... .......... .......... 32% 83.0M 11s 85550K .......... .......... .......... .......... .......... 32% 128M 11s 85600K .......... .......... .......... .......... .......... 32% 132M 11s 85650K .......... .......... .......... .......... .......... 32% 179M 11s 85700K .......... .......... .......... .......... .......... 32% 267M 11s 85750K .......... .......... .......... .......... .......... 32% 91.1M 11s 85800K .......... .......... .......... .......... .......... 32% 71.4M 11s 85850K .......... .......... .......... .......... .......... 32% 70.6M 11s 85900K .......... .......... .......... .......... .......... 32% 120M 11s 85950K .......... .......... .......... .......... .......... 32% 112M 11s 86000K .......... .......... .......... .......... .......... 32% 427K 11s 86050K .......... .......... .......... .......... .......... 32% 132M 11s 86100K .......... .......... .......... .......... .......... 32% 121M 11s 86150K .......... .......... .......... .......... .......... 32% 88.9M 11s 86200K .......... .......... .......... .......... .......... 32% 54.3M 11s 86250K .......... .......... .......... .......... .......... 32% 61.7M 11s 86300K .......... .......... .......... .......... .......... 32% 101M 11s 86350K .......... .......... .......... .......... .......... 32% 157M 11s 86400K .......... .......... .......... .......... .......... 32% 192M 11s 86450K .......... .......... .......... .......... .......... 32% 178M 11s 86500K .......... .......... .......... .......... .......... 33% 181M 11s 86550K .......... .......... .......... .......... .......... 33% 151M 11s 86600K .......... .......... .......... .......... .......... 33% 96.3M 11s 86650K .......... .......... .......... .......... .......... 33% 177M 11s 86700K .......... .......... .......... .......... .......... 33% 108M 11s 86750K .......... .......... .......... .......... .......... 33% 210M 11s 86800K .......... .......... .......... .......... .......... 33% 205M 11s 86850K .......... .......... .......... .......... .......... 33% 85.7M 11s 86900K .......... .......... .......... .......... .......... 33% 157M 11s 86950K .......... .......... .......... .......... .......... 33% 162M 11s 87000K .......... .......... .......... .......... .......... 33% 62.4M 11s 87050K .......... .......... .......... .......... .......... 33% 189M 11s 87100K .......... .......... .......... .......... .......... 33% 110M 11s 87150K .......... .......... .......... .......... .......... 33% 145M 11s 87200K .......... .......... .......... .......... .......... 33% 148M 11s 87250K .......... .......... .......... .......... .......... 33% 164M 11s 87300K .......... .......... .......... .......... .......... 33% 190M 11s 87350K .......... .......... .......... .......... .......... 33% 234M 11s 87400K .......... .......... .......... .......... .......... 33% 248M 11s 87450K .......... .......... .......... .......... .......... 33% 139M 11s 87500K .......... .......... .......... .......... .......... 33% 137M 11s 87550K .......... .......... .......... .......... .......... 33% 142M 11s 87600K .......... .......... .......... .......... .......... 33% 139M 11s 87650K .......... .......... .......... .......... .......... 33% 123M 11s 87700K .......... .......... .......... .......... .......... 33% 173M 11s 87750K .......... .......... .......... .......... .......... 33% 245M 11s 87800K .......... .......... .......... .......... .......... 33% 205M 11s 87850K .......... .......... .......... .......... .......... 33% 114M 11s 87900K .......... .......... .......... .......... .......... 33% 196M 11s 87950K .......... .......... .......... .......... .......... 33% 173M 11s 88000K .......... .......... .......... .......... .......... 33% 195M 11s 88050K .......... .......... .......... .......... .......... 33% 82.3M 11s 88100K .......... .......... .......... .......... .......... 33% 225M 11s 88150K .......... .......... .......... .......... .......... 33% 330M 11s 88200K .......... .......... .......... .......... .......... 33% 174M 11s 88250K .......... .......... .......... .......... .......... 33% 135M 11s 88300K .......... .......... .......... .......... .......... 33% 171M 11s 88350K .......... .......... .......... .......... .......... 33% 241M 11s 88400K .......... .......... .......... .......... .......... 33% 211M 11s 88450K .......... .......... .......... .......... .......... 33% 105M 11s 88500K .......... .......... .......... .......... .......... 33% 243M 11s 88550K .......... .......... .......... .......... .......... 33% 263M 11s 88600K .......... .......... .......... .......... .......... 33% 222M 11s 88650K .......... .......... .......... .......... .......... 33% 258M 11s 88700K .......... .......... .......... .......... .......... 33% 199M 11s 88750K .......... .......... .......... .......... .......... 33% 187M 11s 88800K .......... .......... .......... .......... .......... 33% 120M 11s 88850K .......... .......... .......... .......... .......... 33% 222M 11s 88900K .......... .......... .......... .......... .......... 33% 214M 11s 88950K .......... .......... .......... .......... .......... 33% 292M 11s 89000K .......... .......... .......... .......... .......... 33% 292M 11s 89050K .......... .......... .......... .......... .......... 33% 199K 11s 89100K .......... .......... .......... .......... .......... 33% 92.1M 11s 89150K .......... .......... .......... .......... .......... 34% 54.4M 11s 89200K .......... .......... .......... .......... .......... 34% 195M 11s 89250K .......... .......... .......... .......... .......... 34% 199M 11s 89300K .......... .......... .......... .......... .......... 34% 203M 11s 89350K .......... .......... .......... .......... .......... 34% 174M 11s 89400K .......... .......... .......... .......... .......... 34% 153M 11s 89450K .......... .......... .......... .......... .......... 34% 228M 11s 89500K .......... .......... .......... .......... .......... 34% 311M 11s 89550K .......... .......... .......... .......... .......... 34% 186M 11s 89600K .......... .......... .......... .......... .......... 34% 150M 11s 89650K .......... .......... .......... .......... .......... 34% 140M 11s 89700K .......... .......... .......... .......... .......... 34% 197M 11s 89750K .......... .......... .......... .......... .......... 34% 230M 11s 89800K .......... .......... .......... .......... .......... 34% 224M 11s 89850K .......... .......... .......... .......... .......... 34% 134M 11s 89900K .......... .......... .......... .......... .......... 34% 115M 11s 89950K .......... .......... .......... .......... .......... 34% 137M 11s 90000K .......... .......... .......... .......... .......... 34% 175M 11s 90050K .......... .......... .......... .......... .......... 34% 52.2M 11s 90100K .......... .......... .......... .......... .......... 34% 1.25M 11s 90150K .......... .......... .......... .......... .......... 34% 84.3M 11s 90200K .......... .......... .......... .......... .......... 34% 117M 11s 90250K .......... .......... .......... .......... .......... 34% 77.8M 11s 90300K .......... .......... .......... .......... .......... 34% 109M 11s 90350K .......... .......... .......... .......... .......... 34% 73.9M 11s 90400K .......... .......... .......... .......... .......... 34% 156M 11s 90450K .......... .......... .......... .......... .......... 34% 105M 11s 90500K .......... .......... .......... .......... .......... 34% 72.1M 11s 90550K .......... .......... .......... .......... .......... 34% 136M 11s 90600K .......... .......... .......... .......... .......... 34% 196M 11s 90650K .......... .......... .......... .......... .......... 34% 162M 11s 90700K .......... .......... .......... .......... .......... 34% 154M 11s 90750K .......... .......... .......... .......... .......... 34% 194M 11s 90800K .......... .......... .......... .......... .......... 34% 204M 11s 90850K .......... .......... .......... .......... .......... 34% 228M 11s 90900K .......... .......... .......... .......... .......... 34% 113M 11s 90950K .......... .......... .......... .......... .......... 34% 144M 11s 91000K .......... .......... .......... .......... .......... 34% 104M 11s 91050K .......... .......... .......... .......... .......... 34% 137M 11s 91100K .......... .......... .......... .......... .......... 34% 106M 11s 91150K .......... .......... .......... .......... .......... 34% 198M 11s 91200K .......... .......... .......... .......... .......... 34% 139M 11s 91250K .......... .......... .......... .......... .......... 34% 215M 11s 91300K .......... .......... .......... .......... .......... 34% 211M 11s 91350K .......... .......... .......... .......... .......... 34% 250M 11s 91400K .......... .......... .......... .......... .......... 34% 224M 11s 91450K .......... .......... .......... .......... .......... 34% 161M 11s 91500K .......... .......... .......... .......... .......... 34% 217M 11s 91550K .......... .......... .......... .......... .......... 34% 194M 11s 91600K .......... .......... .......... .......... .......... 34% 189M 11s 91650K .......... .......... .......... .......... .......... 34% 238M 11s 91700K .......... .......... .......... .......... .......... 34% 198M 11s 91750K .......... .......... .......... .......... .......... 35% 216M 11s 91800K .......... .......... .......... .......... .......... 35% 159M 11s 91850K .......... .......... .......... .......... .......... 35% 67.4M 11s 91900K .......... .......... .......... .......... .......... 35% 184M 11s 91950K .......... .......... .......... .......... .......... 35% 173M 11s 92000K .......... .......... .......... .......... .......... 35% 203M 11s 92050K .......... .......... .......... .......... .......... 35% 203M 11s 92100K .......... .......... .......... .......... .......... 35% 111M 11s 92150K .......... .......... .......... .......... .......... 35% 345K 11s 92200K .......... .......... .......... .......... .......... 35% 54.0M 11s 92250K .......... .......... .......... .......... .......... 35% 219M 11s 92300K .......... .......... .......... .......... .......... 35% 223M 11s 92350K .......... .......... .......... .......... .......... 35% 189M 11s 92400K .......... .......... .......... .......... .......... 35% 222M 11s 92450K .......... .......... .......... .......... .......... 35% 71.9M 11s 92500K .......... .......... .......... .......... .......... 35% 205M 11s 92550K .......... .......... .......... .......... .......... 35% 52.2M 11s 92600K .......... .......... .......... .......... .......... 35% 182M 11s 92650K .......... .......... .......... .......... .......... 35% 330M 11s 92700K .......... .......... .......... .......... .......... 35% 276M 11s 92750K .......... .......... .......... .......... .......... 35% 305M 11s 92800K .......... .......... .......... .......... .......... 35% 271M 11s 92850K .......... .......... .......... .......... .......... 35% 200M 11s 92900K .......... .......... .......... .......... .......... 35% 234M 11s 92950K .......... .......... .......... .......... .......... 35% 117M 11s 93000K .......... .......... .......... .......... .......... 35% 190M 11s 93050K .......... .......... .......... .......... .......... 35% 276M 11s 93100K .......... .......... .......... .......... .......... 35% 143M 11s 93150K .......... .......... .......... .......... .......... 35% 55.7M 11s 93200K .......... .......... .......... .......... .......... 35% 143M 11s 93250K .......... .......... .......... .......... .......... 35% 140M 11s 93300K .......... .......... .......... .......... .......... 35% 199M 11s 93350K .......... .......... .......... .......... .......... 35% 168M 11s 93400K .......... .......... .......... .......... .......... 35% 215M 11s 93450K .......... .......... .......... .......... .......... 35% 184M 11s 93500K .......... .......... .......... .......... .......... 35% 186M 11s 93550K .......... .......... .......... .......... .......... 35% 192M 11s 93600K .......... .......... .......... .......... .......... 35% 135M 11s 93650K .......... .......... .......... .......... .......... 35% 194M 11s 93700K .......... .......... .......... .......... .......... 35% 155M 11s 93750K .......... .......... .......... .......... .......... 35% 208M 11s 93800K .......... .......... .......... .......... .......... 35% 204M 11s 93850K .......... .......... .......... .......... .......... 35% 186M 11s 93900K .......... .......... .......... .......... .......... 35% 223M 11s 93950K .......... .......... .......... .......... .......... 35% 198M 11s 94000K .......... .......... .......... .......... .......... 35% 241M 11s 94050K .......... .......... .......... .......... .......... 35% 241M 11s 94100K .......... .......... .......... .......... .......... 35% 126M 11s 94150K .......... .......... .......... .......... .......... 35% 132M 11s 94200K .......... .......... .......... .......... .......... 35% 1.55M 11s 94250K .......... .......... .......... .......... .......... 35% 205M 11s 94300K .......... .......... .......... .......... .......... 35% 128M 11s 94350K .......... .......... .......... .......... .......... 36% 132M 11s 94400K .......... .......... .......... .......... .......... 36% 134M 11s 94450K .......... .......... .......... .......... .......... 36% 119M 11s 94500K .......... .......... .......... .......... .......... 36% 144M 11s 94550K .......... .......... .......... .......... .......... 36% 195M 11s 94600K .......... .......... .......... .......... .......... 36% 111M 11s 94650K .......... .......... .......... .......... .......... 36% 136M 11s 94700K .......... .......... .......... .......... .......... 36% 178M 11s 94750K .......... .......... .......... .......... .......... 36% 194M 11s 94800K .......... .......... .......... .......... .......... 36% 110M 11s 94850K .......... .......... .......... .......... .......... 36% 145M 11s 94900K .......... .......... .......... .......... .......... 36% 186M 11s 94950K .......... .......... .......... .......... .......... 36% 169M 11s 95000K .......... .......... .......... .......... .......... 36% 194M 11s 95050K .......... .......... .......... .......... .......... 36% 196M 11s 95100K .......... .......... .......... .......... .......... 36% 157M 11s 95150K .......... .......... .......... .......... .......... 36% 185M 11s 95200K .......... .......... .......... .......... .......... 36% 114M 11s 95250K .......... .......... .......... .......... .......... 36% 195M 11s 95300K .......... .......... .......... .......... .......... 36% 298M 11s 95350K .......... .......... .......... .......... .......... 36% 191M 11s 95400K .......... .......... .......... .......... .......... 36% 207M 11s 95450K .......... .......... .......... .......... .......... 36% 267M 11s 95500K .......... .......... .......... .......... .......... 36% 294M 11s 95550K .......... .......... .......... .......... .......... 36% 138M 11s 95600K .......... .......... .......... .......... .......... 36% 137M 11s 95650K .......... .......... .......... .......... .......... 36% 228M 10s 95700K .......... .......... .......... .......... .......... 36% 200M 10s 95750K .......... .......... .......... .......... .......... 36% 235M 10s 95800K .......... .......... .......... .......... .......... 36% 235M 10s 95850K .......... .......... .......... .......... .......... 36% 203M 10s 95900K .......... .......... .......... .......... .......... 36% 236M 10s 95950K .......... .......... .......... .......... .......... 36% 202M 10s 96000K .......... .......... .......... .......... .......... 36% 239M 10s 96050K .......... .......... .......... .......... .......... 36% 237M 10s 96100K .......... .......... .......... .......... .......... 36% 204M 10s 96150K .......... .......... .......... .......... .......... 36% 233M 10s 96200K .......... .......... .......... .......... .......... 36% 161M 10s 96250K .......... .......... .......... .......... .......... 36% 101M 10s 96300K .......... .......... .......... .......... .......... 36% 330M 10s 96350K .......... .......... .......... .......... .......... 36% 296M 10s 96400K .......... .......... .......... .......... .......... 36% 344M 10s 96450K .......... .......... .......... .......... .......... 36% 291M 10s 96500K .......... .......... .......... .......... .......... 36% 346M 10s 96550K .......... .......... .......... .......... .......... 36% 344M 10s 96600K .......... .......... .......... .......... .......... 36% 294M 10s 96650K .......... .......... .......... .......... .......... 36% 346M 10s 96700K .......... .......... .......... .......... .......... 36% 294M 10s 96750K .......... .......... .......... .......... .......... 36% 337M 10s 96800K .......... .......... .......... .......... .......... 36% 158M 10s 96850K .......... .......... .......... .......... .......... 36% 289M 10s 96900K .......... .......... .......... .......... .......... 36% 346M 10s 96950K .......... .......... .......... .......... .......... 36% 294M 10s 97000K .......... .......... .......... .......... .......... 37% 346M 10s 97050K .......... .......... .......... .......... .......... 37% 341M 10s 97100K .......... .......... .......... .......... .......... 37% 294M 10s 97150K .......... .......... .......... .......... .......... 37% 346M 10s 97200K .......... .......... .......... .......... .......... 37% 292M 10s 97250K .......... .......... .......... .......... .......... 37% 255K 11s 97300K .......... .......... .......... .......... .......... 37% 287M 11s 97350K .......... .......... .......... .......... .......... 37% 247M 11s 97400K .......... .......... .......... .......... .......... 37% 267M 11s 97450K .......... .......... .......... .......... .......... 37% 84.0M 11s 97500K .......... .......... .......... .......... .......... 37% 89.6M 11s 97550K .......... .......... .......... .......... .......... 37% 176M 11s 97600K .......... .......... .......... .......... .......... 37% 108M 11s 97650K .......... .......... .......... .......... .......... 37% 161M 11s 97700K .......... .......... .......... .......... .......... 37% 189M 10s 97750K .......... .......... .......... .......... .......... 37% 233M 10s 97800K .......... .......... .......... .......... .......... 37% 233M 10s 97850K .......... .......... .......... .......... .......... 37% 203M 10s 97900K .......... .......... .......... .......... .......... 37% 177M 10s 97950K .......... .......... .......... .......... .......... 37% 181M 10s 98000K .......... .......... .......... .......... .......... 37% 215M 10s 98050K .......... .......... .......... .......... .......... 37% 215M 10s 98100K .......... .......... .......... .......... .......... 37% 186M 10s 98150K .......... .......... .......... .......... .......... 37% 216M 10s 98200K .......... .......... .......... .......... .......... 37% 198M 10s 98250K .......... .......... .......... .......... .......... 37% 210M 10s 98300K .......... .......... .......... .......... .......... 37% 57.0M 10s 98350K .......... .......... .......... .......... .......... 37% 99.4M 10s 98400K .......... .......... .......... .......... .......... 37% 105M 10s 98450K .......... .......... .......... .......... .......... 37% 136M 10s 98500K .......... .......... .......... .......... .......... 37% 199M 10s 98550K .......... .......... .......... .......... .......... 37% 207M 10s 98600K .......... .......... .......... .......... .......... 37% 148M 10s 98650K .......... .......... .......... .......... .......... 37% 166M 10s 98700K .......... .......... .......... .......... .......... 37% 158M 10s 98750K .......... .......... .......... .......... .......... 37% 190M 10s 98800K .......... .......... .......... .......... .......... 37% 210M 10s 98850K .......... .......... .......... .......... .......... 37% 218M 10s 98900K .......... .......... .......... .......... .......... 37% 155M 10s 98950K .......... .......... .......... .......... .......... 37% 208M 10s 99000K .......... .......... .......... .......... .......... 37% 186M 10s 99050K .......... .......... .......... .......... .......... 37% 187M 10s 99100K .......... .......... .......... .......... .......... 37% 170M 10s 99150K .......... .......... .......... .......... .......... 37% 189M 10s 99200K .......... .......... .......... .......... .......... 37% 95.9M 10s 99250K .......... .......... .......... .......... .......... 37% 198M 10s 99300K .......... .......... .......... .......... .......... 37% 712K 10s 99350K .......... .......... .......... .......... .......... 37% 74.7M 10s 99400K .......... .......... .......... .......... .......... 37% 227M 10s 99450K .......... .......... .......... .......... .......... 37% 197M 10s 99500K .......... .......... .......... .......... .......... 37% 234M 10s 99550K .......... .......... .......... .......... .......... 37% 210M 10s 99600K .......... .......... .......... .......... .......... 38% 92.1M 10s 99650K .......... .......... .......... .......... .......... 38% 315M 10s 99700K .......... .......... .......... .......... .......... 38% 282M 10s 99750K .......... .......... .......... .......... .......... 38% 334M 10s 99800K .......... .......... .......... .......... .......... 38% 334M 10s 99850K .......... .......... .......... .......... .......... 38% 236M 10s 99900K .......... .......... .......... .......... .......... 38% 242M 10s 99950K .......... .......... .......... .......... .......... 38% 111M 10s 100000K .......... .......... .......... .......... .......... 38% 218M 10s 100050K .......... .......... .......... .......... .......... 38% 183M 10s 100100K .......... .......... .......... .......... .......... 38% 157M 10s 100150K .......... .......... .......... .......... .......... 38% 279M 10s 100200K .......... .......... .......... .......... .......... 38% 187M 10s 100250K .......... .......... .......... .......... .......... 38% 291M 10s 100300K .......... .......... .......... .......... .......... 38% 206M 10s 100350K .......... .......... .......... .......... .......... 38% 4.77M 10s 100400K .......... .......... .......... .......... .......... 38% 221M 10s 100450K .......... .......... .......... .......... .......... 38% 209M 10s 100500K .......... .......... .......... .......... .......... 38% 239M 10s 100550K .......... .......... .......... .......... .......... 38% 243M 10s 100600K .......... .......... .......... .......... .......... 38% 207M 10s 100650K .......... .......... .......... .......... .......... 38% 209M 10s 100700K .......... .......... .......... .......... .......... 38% 167M 10s 100750K .......... .......... .......... .......... .......... 38% 167M 10s 100800K .......... .......... .......... .......... .......... 38% 210M 10s 100850K .......... .......... .......... .......... .......... 38% 206M 10s 100900K .......... .......... .......... .......... .......... 38% 189M 10s 100950K .......... .......... .......... .......... .......... 38% 133M 10s 101000K .......... .......... .......... .......... .......... 38% 167M 10s 101050K .......... .......... .......... .......... .......... 38% 144M 10s 101100K .......... .......... .......... .......... .......... 38% 186M 10s 101150K .......... .......... .......... .......... .......... 38% 224M 10s 101200K .......... .......... .......... .......... .......... 38% 191M 10s 101250K .......... .......... .......... .......... .......... 38% 161M 10s 101300K .......... .......... .......... .......... .......... 38% 273M 10s 101350K .......... .......... .......... .......... .......... 38% 2.31M 10s 101400K .......... .......... .......... .......... .......... 38% 100M 10s 101450K .......... .......... .......... .......... .......... 38% 126M 10s 101500K .......... .......... .......... .......... .......... 38% 152M 10s 101550K .......... .......... .......... .......... .......... 38% 184M 10s 101600K .......... .......... .......... .......... .......... 38% 167M 10s 101650K .......... .......... .......... .......... .......... 38% 187M 10s 101700K .......... .......... .......... .......... .......... 38% 185M 10s 101750K .......... .......... .......... .......... .......... 38% 218M 10s 101800K .......... .......... .......... .......... .......... 38% 151M 10s 101850K .......... .......... .......... .......... .......... 38% 185M 10s 101900K .......... .......... .......... .......... .......... 38% 210M 10s 101950K .......... .......... .......... .......... .......... 38% 143M 10s 102000K .......... .......... .......... .......... .......... 38% 179M 10s 102050K .......... .......... .......... .......... .......... 38% 159M 10s 102100K .......... .......... .......... .......... .......... 38% 194M 10s 102150K .......... .......... .......... .......... .......... 38% 226M 10s 102200K .......... .......... .......... .......... .......... 38% 193M 10s 102250K .......... .......... .......... .......... .......... 39% 194M 10s 102300K .......... .......... .......... .......... .......... 39% 160M 10s 102350K .......... .......... .......... .......... .......... 39% 195M 10s 102400K .......... .......... .......... .......... .......... 39% 1.88M 10s 102450K .......... .......... .......... .......... .......... 39% 74.7M 10s 102500K .......... .......... .......... .......... .......... 39% 1.72M 10s 102550K .......... .......... .......... .......... .......... 39% 330M 10s 102600K .......... .......... .......... .......... .......... 39% 286M 10s 102650K .......... .......... .......... .......... .......... 39% 33.4M 10s 102700K .......... .......... .......... .......... .......... 39% 5.52M 10s 102750K .......... .......... .......... .......... .......... 39% 201M 10s 102800K .......... .......... .......... .......... .......... 39% 110M 10s 102850K .......... .......... .......... .......... .......... 39% 160M 10s 102900K .......... .......... .......... .......... .......... 39% 122M 10s 102950K .......... .......... .......... .......... .......... 39% 103M 10s 103000K .......... .......... .......... .......... .......... 39% 11.6M 10s 103050K .......... .......... .......... .......... .......... 39% 91.3M 10s 103100K .......... .......... .......... .......... .......... 39% 4.57M 10s 103150K .......... .......... .......... .......... .......... 39% 17.6M 10s 103200K .......... .......... .......... .......... .......... 39% 81.0M 10s 103250K .......... .......... .......... .......... .......... 39% 151M 10s 103300K .......... .......... .......... .......... .......... 39% 138M 10s 103350K .......... .......... .......... .......... .......... 39% 161M 10s 103400K .......... .......... .......... .......... .......... 39% 32.7M 10s 103450K .......... .......... .......... .......... .......... 39% 6.09M 10s 103500K .......... .......... .......... .......... .......... 39% 21.8M 10s 103550K .......... .......... .......... .......... .......... 39% 42.8M 10s 103600K .......... .......... .......... .......... .......... 39% 9.35M 10s 103650K .......... .......... .......... .......... .......... 39% 65.3M 10s 103700K .......... .......... .......... .......... .......... 39% 144M 10s 103750K .......... .......... .......... .......... .......... 39% 287M 10s 103800K .......... .......... .......... .......... .......... 39% 305M 10s 103850K .......... .......... .......... .......... .......... 39% 271M 10s 103900K .......... .......... .......... .......... .......... 39% 317M 10s 103950K .......... .......... .......... .......... .......... 39% 291M 10s 104000K .......... .......... .......... .......... .......... 39% 341M 10s 104050K .......... .......... .......... .......... .......... 39% 339M 10s 104100K .......... .......... .......... .......... .......... 39% 85.7M 10s 104150K .......... .......... .......... .......... .......... 39% 254M 10s 104200K .......... .......... .......... .......... .......... 39% 270M 10s 104250K .......... .......... .......... .......... .......... 39% 127M 10s 104300K .......... .......... .......... .......... .......... 39% 167M 10s 104350K .......... .......... .......... .......... .......... 39% 182M 10s 104400K .......... .......... .......... .......... .......... 39% 276M 10s 104450K .......... .......... .......... .......... .......... 39% 1.43M 10s 104500K .......... .......... .......... .......... .......... 39% 75.7M 10s 104550K .......... .......... .......... .......... .......... 39% 133M 10s 104600K .......... .......... .......... .......... .......... 39% 55.2M 10s 104650K .......... .......... .......... .......... .......... 39% 139M 10s 104700K .......... .......... .......... .......... .......... 39% 94.1M 10s 104750K .......... .......... .......... .......... .......... 39% 127M 10s 104800K .......... .......... .......... .......... .......... 39% 102M 10s 104850K .......... .......... .......... .......... .......... 40% 62.7M 10s 104900K .......... .......... .......... .......... .......... 40% 72.7M 10s 104950K .......... .......... .......... .......... .......... 40% 43.8M 10s 105000K .......... .......... .......... .......... .......... 40% 68.5M 10s 105050K .......... .......... .......... .......... .......... 40% 67.3M 10s 105100K .......... .......... .......... .......... .......... 40% 47.5M 10s 105150K .......... .......... .......... .......... .......... 40% 68.8M 10s 105200K .......... .......... .......... .......... .......... 40% 121M 10s 105250K .......... .......... .......... .......... .......... 40% 69.0M 10s 105300K .......... .......... .......... .......... .......... 40% 42.5M 10s 105350K .......... .......... .......... .......... .......... 40% 117M 10s 105400K .......... .......... .......... .......... .......... 40% 59.8M 10s 105450K .......... .......... .......... .......... .......... 40% 70.9M 10s 105500K .......... .......... .......... .......... .......... 40% 159M 10s 105550K .......... .......... .......... .......... .......... 40% 1.70M 10s 105600K .......... .......... .......... .......... .......... 40% 58.5M 10s 105650K .......... .......... .......... .......... .......... 40% 64.2M 10s 105700K .......... .......... .......... .......... .......... 40% 125M 10s 105750K .......... .......... .......... .......... .......... 40% 123M 10s 105800K .......... .......... .......... .......... .......... 40% 95.6M 10s 105850K .......... .......... .......... .......... .......... 40% 184M 10s 105900K .......... .......... .......... .......... .......... 40% 219M 10s 105950K .......... .......... .......... .......... .......... 40% 199M 10s 106000K .......... .......... .......... .......... .......... 40% 221M 10s 106050K .......... .......... .......... .......... .......... 40% 151M 10s 106100K .......... .......... .......... .......... .......... 40% 190M 10s 106150K .......... .......... .......... .......... .......... 40% 143M 10s 106200K .......... .......... .......... .......... .......... 40% 190M 10s 106250K .......... .......... .......... .......... .......... 40% 292M 10s 106300K .......... .......... .......... .......... .......... 40% 208M 10s 106350K .......... .......... .......... .......... .......... 40% 252M 10s 106400K .......... .......... .......... .......... .......... 40% 300M 10s 106450K .......... .......... .......... .......... .......... 40% 29.0M 10s 106500K .......... .......... .......... .......... .......... 40% 71.0M 10s 106550K .......... .......... .......... .......... .......... 40% 245M 10s 106600K .......... .......... .......... .......... .......... 40% 118M 10s 106650K .......... .......... .......... .......... .......... 40% 18.1M 10s 106700K .......... .......... .......... .......... .......... 40% 165M 10s 106750K .......... .......... .......... .......... .......... 40% 219M 10s 106800K .......... .......... .......... .......... .......... 40% 173M 10s 106850K .......... .......... .......... .......... .......... 40% 205M 10s 106900K .......... .......... .......... .......... .......... 40% 107M 10s 106950K .......... .......... .......... .......... .......... 40% 142M 10s 107000K .......... .......... .......... .......... .......... 40% 193M 10s 107050K .......... .......... .......... .......... .......... 40% 236M 10s 107100K .......... .......... .......... .......... .......... 40% 250M 10s 107150K .......... .......... .......... .......... .......... 40% 223M 9s 107200K .......... .......... .......... .......... .......... 40% 148M 9s 107250K .......... .......... .......... .......... .......... 40% 174M 9s 107300K .......... .......... .......... .......... .......... 40% 129M 9s 107350K .......... .......... .......... .......... .......... 40% 183M 9s 107400K .......... .......... .......... .......... .......... 40% 163M 9s 107450K .......... .......... .......... .......... .......... 40% 161M 9s 107500K .......... .......... .......... .......... .......... 41% 3.76M 9s 107550K .......... .......... .......... .......... .......... 41% 45.8M 9s 107600K .......... .......... .......... .......... .......... 41% 286M 9s 107650K .......... .......... .......... .......... .......... 41% 279M 9s 107700K .......... .......... .......... .......... .......... 41% 282M 9s 107750K .......... .......... .......... .......... .......... 41% 291M 9s 107800K .......... .......... .......... .......... .......... 41% 305M 9s 107850K .......... .......... .......... .......... .......... 41% 248M 9s 107900K .......... .......... .......... .......... .......... 41% 305M 9s 107950K .......... .......... .......... .......... .......... 41% 11.8M 9s 108000K .......... .......... .......... .......... .......... 41% 18.5M 9s 108050K .......... .......... .......... .......... .......... 41% 188M 9s 108100K .......... .......... .......... .......... .......... 41% 4.05M 9s 108150K .......... .......... .......... .......... .......... 41% 233M 9s 108200K .......... .......... .......... .......... .......... 41% 127M 9s 108250K .......... .......... .......... .......... .......... 41% 227M 9s 108300K .......... .......... .......... .......... .......... 41% 182M 9s 108350K .......... .......... .......... .......... .......... 41% 188M 9s 108400K .......... .......... .......... .......... .......... 41% 223M 9s 108450K .......... .......... .......... .......... .......... 41% 9.27M 9s 108500K .......... .......... .......... .......... .......... 41% 8.08M 9s 108550K .......... .......... .......... .......... .......... 41% 173M 9s 108600K .......... .......... .......... .......... .......... 41% 62.0M 9s 108650K .......... .......... .......... .......... .......... 41% 20.8M 9s 108700K .......... .......... .......... .......... .......... 41% 188M 9s 108750K .......... .......... .......... .......... .......... 41% 155M 9s 108800K .......... .......... .......... .......... .......... 41% 164M 9s 108850K .......... .......... .......... .......... .......... 41% 202M 9s 108900K .......... .......... .......... .......... .......... 41% 182M 9s 108950K .......... .......... .......... .......... .......... 41% 151M 9s 109000K .......... .......... .......... .......... .......... 41% 236M 9s 109050K .......... .......... .......... .......... .......... 41% 236M 9s 109100K .......... .......... .......... .......... .......... 41% 151M 9s 109150K .......... .......... .......... .......... .......... 41% 207M 9s 109200K .......... .......... .......... .......... .......... 41% 200M 9s 109250K .......... .......... .......... .......... .......... 41% 230M 9s 109300K .......... .......... .......... .......... .......... 41% 148M 9s 109350K .......... .......... .......... .......... .......... 41% 121M 9s 109400K .......... .......... .......... .......... .......... 41% 102M 9s 109450K .......... .......... .......... .......... .......... 41% 184M 9s 109500K .......... .......... .......... .......... .......... 41% 238M 9s 109550K .......... .......... .......... .......... .......... 41% 206K 10s 109600K .......... .......... .......... .......... .......... 41% 152M 10s 109650K .......... .......... .......... .......... .......... 41% 198M 10s 109700K .......... .......... .......... .......... .......... 41% 108M 10s 109750K .......... .......... .......... .......... .......... 41% 129M 10s 109800K .......... .......... .......... .......... .......... 41% 149M 10s 109850K .......... .......... .......... .......... .......... 41% 178M 10s 109900K .......... .......... .......... .......... .......... 41% 154M 10s 109950K .......... .......... .......... .......... .......... 41% 136M 10s 110000K .......... .......... .......... .......... .......... 41% 48.9M 9s 110050K .......... .......... .......... .......... .......... 41% 167M 9s 110100K .......... .......... .......... .......... .......... 42% 81.5M 9s 110150K .......... .......... .......... .......... .......... 42% 214M 9s 110200K .......... .......... .......... .......... .......... 42% 196M 9s 110250K .......... .......... .......... .......... .......... 42% 138M 9s 110300K .......... .......... .......... .......... .......... 42% 175M 9s 110350K .......... .......... .......... .......... .......... 42% 194M 9s 110400K .......... .......... .......... .......... .......... 42% 221M 9s 110450K .......... .......... .......... .......... .......... 42% 198M 9s 110500K .......... .......... .......... .......... .......... 42% 148M 9s 110550K .......... .......... .......... .......... .......... 42% 128M 9s 110600K .......... .......... .......... .......... .......... 42% 154M 9s 110650K .......... .......... .......... .......... .......... 42% 224M 9s 110700K .......... .......... .......... .......... .......... 42% 2.29M 9s 110750K .......... .......... .......... .......... .......... 42% 238M 9s 110800K .......... .......... .......... .......... .......... 42% 267M 9s 110850K .......... .......... .......... .......... .......... 42% 159M 9s 110900K .......... .......... .......... .......... .......... 42% 264M 9s 110950K .......... .......... .......... .......... .......... 42% 182M 9s 111000K .......... .......... .......... .......... .......... 42% 237M 9s 111050K .......... .......... .......... .......... .......... 42% 152M 9s 111100K .......... .......... .......... .......... .......... 42% 212M 9s 111150K .......... .......... .......... .......... .......... 42% 131M 9s 111200K .......... .......... .......... .......... .......... 42% 216M 9s 111250K .......... .......... .......... .......... .......... 42% 225M 9s 111300K .......... .......... .......... .......... .......... 42% 93.9M 9s 111350K .......... .......... .......... .......... .......... 42% 109M 9s 111400K .......... .......... .......... .......... .......... 42% 175M 9s 111450K .......... .......... .......... .......... .......... 42% 126M 9s 111500K .......... .......... .......... .......... .......... 42% 180M 9s 111550K .......... .......... .......... .......... .......... 42% 207M 9s 111600K .......... .......... .......... .......... .......... 42% 151M 9s 111650K .......... .......... .......... .......... .......... 42% 210M 9s 111700K .......... .......... .......... .......... .......... 42% 166M 9s 111750K .......... .......... .......... .......... .......... 42% 222M 9s 111800K .......... .......... .......... .......... .......... 42% 153M 9s 111850K .......... .......... .......... .......... .......... 42% 169M 9s 111900K .......... .......... .......... .......... .......... 42% 237M 9s 111950K .......... .......... .......... .......... .......... 42% 122M 9s 112000K .......... .......... .......... .......... .......... 42% 179M 9s 112050K .......... .......... .......... .......... .......... 42% 237M 9s 112100K .......... .......... .......... .......... .......... 42% 125M 9s 112150K .......... .......... .......... .......... .......... 42% 135M 9s 112200K .......... .......... .......... .......... .......... 42% 114M 9s 112250K .......... .......... .......... .......... .......... 42% 119M 9s 112300K .......... .......... .......... .......... .......... 42% 122M 9s 112350K .......... .......... .......... .......... .......... 42% 136M 9s 112400K .......... .......... .......... .......... .......... 42% 132M 9s 112450K .......... .......... .......... .......... .......... 42% 91.1M 9s 112500K .......... .......... .......... .......... .......... 42% 163M 9s 112550K .......... .......... .......... .......... .......... 42% 180M 9s 112600K .......... .......... .......... .......... .......... 42% 30.2M 9s 112650K .......... .......... .......... .......... .......... 42% 89.9M 9s 112700K .......... .......... .......... .......... .......... 43% 149M 9s 112750K .......... .......... .......... .......... .......... 43% 115M 9s 112800K .......... .......... .......... .......... .......... 43% 228M 9s 112850K .......... .......... .......... .......... .......... 43% 196M 9s 112900K .......... .......... .......... .......... .......... 43% 234M 9s 112950K .......... .......... .......... .......... .......... 43% 111M 9s 113000K .......... .......... .......... .......... .......... 43% 231M 9s 113050K .......... .......... .......... .......... .......... 43% 200M 9s 113100K .......... .......... .......... .......... .......... 43% 148M 9s 113150K .......... .......... .......... .......... .......... 43% 142M 9s 113200K .......... .......... .......... .......... .......... 43% 187M 9s 113250K .......... .......... .......... .......... .......... 43% 227M 9s 113300K .......... .......... .......... .......... .......... 43% 221M 9s 113350K .......... .......... .......... .......... .......... 43% 197M 9s 113400K .......... .......... .......... .......... .......... 43% 224M 9s 113450K .......... .......... .......... .......... .......... 43% 202M 9s 113500K .......... .......... .......... .......... .......... 43% 230M 9s 113550K .......... .......... .......... .......... .......... 43% 227M 9s 113600K .......... .......... .......... .......... .......... 43% 196M 9s 113650K .......... .......... .......... .......... .......... 43% 148M 9s 113700K .......... .......... .......... .......... .......... 43% 192M 9s 113750K .......... .......... .......... .......... .......... 43% 228M 9s 113800K .......... .......... .......... .......... .......... 43% 222M 9s 113850K .......... .......... .......... .......... .......... 43% 201M 9s 113900K .......... .......... .......... .......... .......... 43% 216M 9s 113950K .......... .......... .......... .......... .......... 43% 150M 9s 114000K .......... .......... .......... .......... .......... 43% 186M 9s 114050K .......... .......... .......... .......... .......... 43% 326M 9s 114100K .......... .......... .......... .......... .......... 43% 294M 9s 114150K .......... .......... .......... .......... .......... 43% 346M 9s 114200K .......... .......... .......... .......... .......... 43% 298M 9s 114250K .......... .......... .......... .......... .......... 43% 334M 9s 114300K .......... .......... .......... .......... .......... 43% 344M 9s 114350K .......... .......... .......... .......... .......... 43% 296M 9s 114400K .......... .......... .......... .......... .......... 43% 344M 9s 114450K .......... .......... .......... .......... .......... 43% 300M 9s 114500K .......... .......... .......... .......... .......... 43% 326M 9s 114550K .......... .......... .......... .......... .......... 43% 346M 9s 114600K .......... .......... .......... .......... .......... 43% 298M 9s 114650K .......... .......... .......... .......... .......... 43% 234K 9s 114700K .......... .......... .......... .......... .......... 43% 27.9M 9s 114750K .......... .......... .......... .......... .......... 43% 186M 9s 114800K .......... .......... .......... .......... .......... 43% 203M 9s 114850K .......... .......... .......... .......... .......... 43% 76.1M 9s 114900K .......... .......... .......... .......... .......... 43% 165M 9s 114950K .......... .......... .......... .......... .......... 43% 28.7M 9s 115000K .......... .......... .......... .......... .......... 43% 139M 9s 115050K .......... .......... .......... .......... .......... 43% 72.2M 9s 115100K .......... .......... .......... .......... .......... 43% 48.3M 9s 115150K .......... .......... .......... .......... .......... 43% 173M 9s 115200K .......... .......... .......... .......... .......... 43% 140M 9s 115250K .......... .......... .......... .......... .......... 43% 49.6M 9s 115300K .......... .......... .......... .......... .......... 43% 103M 9s 115350K .......... .......... .......... .......... .......... 44% 60.8M 9s 115400K .......... .......... .......... .......... .......... 44% 135M 9s 115450K .......... .......... .......... .......... .......... 44% 86.0M 9s 115500K .......... .......... .......... .......... .......... 44% 64.9M 9s 115550K .......... .......... .......... .......... .......... 44% 140M 9s 115600K .......... .......... .......... .......... .......... 44% 86.6M 9s 115650K .......... .......... .......... .......... .......... 44% 90.1M 9s 115700K .......... .......... .......... .......... .......... 44% 90.1M 9s 115750K .......... .......... .......... .......... .......... 44% 200M 9s 115800K .......... .......... .......... .......... .......... 44% 213M 9s 115850K .......... .......... .......... .......... .......... 44% 193M 9s 115900K .......... .......... .......... .......... .......... 44% 165M 9s 115950K .......... .......... .......... .......... .......... 44% 136M 9s 116000K .......... .......... .......... .......... .......... 44% 163M 9s 116050K .......... .......... .......... .......... .......... 44% 155M 9s 116100K .......... .......... .......... .......... .......... 44% 144M 9s 116150K .......... .......... .......... .......... .......... 44% 204M 9s 116200K .......... .......... .......... .......... .......... 44% 162M 9s 116250K .......... .......... .......... .......... .......... 44% 228M 9s 116300K .......... .......... .......... .......... .......... 44% 225M 9s 116350K .......... .......... .......... .......... .......... 44% 166M 9s 116400K .......... .......... .......... .......... .......... 44% 173M 9s 116450K .......... .......... .......... .......... .......... 44% 138M 9s 116500K .......... .......... .......... .......... .......... 44% 132M 9s 116550K .......... .......... .......... .......... .......... 44% 231M 9s 116600K .......... .......... .......... .......... .......... 44% 180M 9s 116650K .......... .......... .......... .......... .......... 44% 211M 9s 116700K .......... .......... .......... .......... .......... 44% 2.36M 9s 116750K .......... .......... .......... .......... .......... 44% 77.0M 9s 116800K .......... .......... .......... .......... .......... 44% 282M 9s 116850K .......... .......... .......... .......... .......... 44% 129M 9s 116900K .......... .......... .......... .......... .......... 44% 174M 9s 116950K .......... .......... .......... .......... .......... 44% 256M 9s 117000K .......... .......... .......... .......... .......... 44% 204M 9s 117050K .......... .......... .......... .......... .......... 44% 121M 9s 117100K .......... .......... .......... .......... .......... 44% 164M 9s 117150K .......... .......... .......... .......... .......... 44% 236M 9s 117200K .......... .......... .......... .......... .......... 44% 105M 9s 117250K .......... .......... .......... .......... .......... 44% 149M 9s 117300K .......... .......... .......... .......... .......... 44% 165M 9s 117350K .......... .......... .......... .......... .......... 44% 271M 9s 117400K .......... .......... .......... .......... .......... 44% 330M 9s 117450K .......... .......... .......... .......... .......... 44% 273M 9s 117500K .......... .......... .......... .......... .......... 44% 332M 9s 117550K .......... .......... .......... .......... .......... 44% 344M 9s 117600K .......... .......... .......... .......... .......... 44% 263M 9s 117650K .......... .......... .......... .......... .......... 44% 321M 9s 117700K .......... .......... .......... .......... .......... 44% 279M 9s 117750K .......... .......... .......... .......... .......... 44% 195M 9s 117800K .......... .......... .......... .......... .......... 44% 191M 9s 117850K .......... .......... .......... .......... .......... 44% 149M 9s 117900K .......... .......... .......... .......... .......... 44% 226M 9s 117950K .......... .......... .......... .......... .......... 45% 252M 9s 118000K .......... .......... .......... .......... .......... 45% 346M 9s 118050K .......... .......... .......... .......... .......... 45% 225M 9s 118100K .......... .......... .......... .......... .......... 45% 273M 9s 118150K .......... .......... .......... .......... .......... 45% 96.3M 9s 118200K .......... .......... .......... .......... .......... 45% 148M 9s 118250K .......... .......... .......... .......... .......... 45% 191M 9s 118300K .......... .......... .......... .......... .......... 45% 196M 9s 118350K .......... .......... .......... .......... .......... 45% 301M 9s 118400K .......... .......... .......... .......... .......... 45% 243M 9s 118450K .......... .......... .......... .......... .......... 45% 303M 9s 118500K .......... .......... .......... .......... .......... 45% 233M 9s 118550K .......... .......... .......... .......... .......... 45% 222M 9s 118600K .......... .......... .......... .......... .......... 45% 187M 9s 118650K .......... .......... .......... .......... .......... 45% 219M 9s 118700K .......... .......... .......... .......... .......... 45% 203M 9s 118750K .......... .......... .......... .......... .......... 45% 6.03M 9s 118800K .......... .......... .......... .......... .......... 45% 123M 9s 118850K .......... .......... .......... .......... .......... 45% 162M 9s 118900K .......... .......... .......... .......... .......... 45% 180M 9s 118950K .......... .......... .......... .......... .......... 45% 164M 9s 119000K .......... .......... .......... .......... .......... 45% 309M 9s 119050K .......... .......... .......... .......... .......... 45% 341M 9s 119100K .......... .......... .......... .......... .......... 45% 291M 9s 119150K .......... .......... .......... .......... .......... 45% 136M 9s 119200K .......... .......... .......... .......... .......... 45% 136M 9s 119250K .......... .......... .......... .......... .......... 45% 2.39M 9s 119300K .......... .......... .......... .......... .......... 45% 187M 9s 119350K .......... .......... .......... .......... .......... 45% 164M 9s 119400K .......... .......... .......... .......... .......... 45% 228M 9s 119450K .......... .......... .......... .......... .......... 45% 126M 9s 119500K .......... .......... .......... .......... .......... 45% 144M 9s 119550K .......... .......... .......... .......... .......... 45% 236M 9s 119600K .......... .......... .......... .......... .......... 45% 155M 9s 119650K .......... .......... .......... .......... .......... 45% 166M 9s 119700K .......... .......... .......... .......... .......... 45% 193M 9s 119750K .......... .......... .......... .......... .......... 45% 141M 9s 119800K .......... .......... .......... .......... .......... 45% 276K 9s 119850K .......... .......... .......... .......... .......... 45% 125M 9s 119900K .......... .......... .......... .......... .......... 45% 143M 9s 119950K .......... .......... .......... .......... .......... 45% 59.4M 9s 120000K .......... .......... .......... .......... .......... 45% 116M 9s 120050K .......... .......... .......... .......... .......... 45% 78.9M 9s 120100K .......... .......... .......... .......... .......... 45% 139M 9s 120150K .......... .......... .......... .......... .......... 45% 59.8M 9s 120200K .......... .......... .......... .......... .......... 45% 71.7M 9s 120250K .......... .......... .......... .......... .......... 45% 130M 9s 120300K .......... .......... .......... .......... .......... 45% 235M 9s 120350K .......... .......... .......... .......... .......... 45% 131M 9s 120400K .......... .......... .......... .......... .......... 45% 143M 9s 120450K .......... .......... .......... .......... .......... 45% 95.7M 9s 120500K .......... .......... .......... .......... .......... 45% 150M 9s 120550K .......... .......... .......... .......... .......... 45% 144M 9s 120600K .......... .......... .......... .......... .......... 46% 116M 9s 120650K .......... .......... .......... .......... .......... 46% 93.9M 9s 120700K .......... .......... .......... .......... .......... 46% 108M 9s 120750K .......... .......... .......... .......... .......... 46% 139M 9s 120800K .......... .......... .......... .......... .......... 46% 68.0M 9s 120850K .......... .......... .......... .......... .......... 46% 2.08M 9s 120900K .......... .......... .......... .......... .......... 46% 78.6M 9s 120950K .......... .......... .......... .......... .......... 46% 174M 9s 121000K .......... .......... .......... .......... .......... 46% 214M 9s 121050K .......... .......... .......... .......... .......... 46% 225M 9s 121100K .......... .......... .......... .......... .......... 46% 162M 9s 121150K .......... .......... .......... .......... .......... 46% 206M 9s 121200K .......... .......... .......... .......... .......... 46% 154M 9s 121250K .......... .......... .......... .......... .......... 46% 108M 9s 121300K .......... .......... .......... .......... .......... 46% 196M 9s 121350K .......... .......... .......... .......... .......... 46% 178M 9s 121400K .......... .......... .......... .......... .......... 46% 209M 9s 121450K .......... .......... .......... .......... .......... 46% 148M 9s 121500K .......... .......... .......... .......... .......... 46% 196M 9s 121550K .......... .......... .......... .......... .......... 46% 179M 9s 121600K .......... .......... .......... .......... .......... 46% 206M 9s 121650K .......... .......... .......... .......... .......... 46% 243M 9s 121700K .......... .......... .......... .......... .......... 46% 210M 9s 121750K .......... .......... .......... .......... .......... 46% 238M 9s 121800K .......... .......... .......... .......... .......... 46% 245M 9s 121850K .......... .......... .......... .......... .......... 46% 106M 9s 121900K .......... .......... .......... .......... .......... 46% 242M 9s 121950K .......... .......... .......... .......... .......... 46% 8.90M 9s 122000K .......... .......... .......... .......... .......... 46% 157M 9s 122050K .......... .......... .......... .......... .......... 46% 185M 9s 122100K .......... .......... .......... .......... .......... 46% 149M 9s 122150K .......... .......... .......... .......... .......... 46% 140M 9s 122200K .......... .......... .......... .......... .......... 46% 137M 9s 122250K .......... .......... .......... .......... .......... 46% 277M 9s 122300K .......... .......... .......... .......... .......... 46% 273M 9s 122350K .......... .......... .......... .......... .......... 46% 245M 8s 122400K .......... .......... .......... .......... .......... 46% 123M 8s 122450K .......... .......... .......... .......... .......... 46% 180M 8s 122500K .......... .......... .......... .......... .......... 46% 239M 8s 122550K .......... .......... .......... .......... .......... 46% 237M 8s 122600K .......... .......... .......... .......... .......... 46% 224M 8s 122650K .......... .......... .......... .......... .......... 46% 202M 8s 122700K .......... .......... .......... .......... .......... 46% 169M 8s 122750K .......... .......... .......... .......... .......... 46% 209M 8s 122800K .......... .......... .......... .......... .......... 46% 271M 8s 122850K .......... .......... .......... .......... .......... 46% 191M 8s 122900K .......... .......... .......... .......... .......... 46% 313M 8s 122950K .......... .......... .......... .......... .......... 46% 227M 8s 123000K .......... .......... .......... .......... .......... 46% 154M 8s 123050K .......... .......... .......... .......... .......... 46% 183M 8s 123100K .......... .......... .......... .......... .......... 46% 228M 8s 123150K .......... .......... .......... .......... .......... 46% 309M 8s 123200K .......... .......... .......... .......... .......... 47% 287M 8s 123250K .......... .......... .......... .......... .......... 47% 256M 8s 123300K .......... .......... .......... .......... .......... 47% 303M 8s 123350K .......... .......... .......... .......... .......... 47% 289M 8s 123400K .......... .......... .......... .......... .......... 47% 337M 8s 123450K .......... .......... .......... .......... .......... 47% 300M 8s 123500K .......... .......... .......... .......... .......... 47% 349M 8s 123550K .......... .......... .......... .......... .......... 47% 344M 8s 123600K .......... .......... .......... .......... .......... 47% 292M 8s 123650K .......... .......... .......... .......... .......... 47% 339M 8s 123700K .......... .......... .......... .......... .......... 47% 301M 8s 123750K .......... .......... .......... .......... .......... 47% 346M 8s 123800K .......... .......... .......... .......... .......... 47% 341M 8s 123850K .......... .......... .......... .......... .......... 47% 301M 8s 123900K .......... .......... .......... .......... .......... 47% 252M 8s 123950K .......... .......... .......... .......... .......... 47% 300M 8s 124000K .......... .......... .......... .......... .......... 47% 317M 8s 124050K .......... .......... .......... .......... .......... 47% 346M 8s 124100K .......... .......... .......... .......... .......... 47% 289M 8s 124150K .......... .......... .......... .......... .......... 47% 341M 8s 124200K .......... .......... .......... .......... .......... 47% 300M 8s 124250K .......... .......... .......... .......... .......... 47% 326M 8s 124300K .......... .......... .......... .......... .......... 47% 279M 8s 124350K .......... .......... .......... .......... .......... 47% 227M 8s 124400K .......... .......... .......... .......... .......... 47% 243M 8s 124450K .......... .......... .......... .......... .......... 47% 212M 8s 124500K .......... .......... .......... .......... .......... 47% 252M 8s 124550K .......... .......... .......... .......... .......... 47% 250M 8s 124600K .......... .......... .......... .......... .......... 47% 257M 8s 124650K .......... .......... .......... .......... .......... 47% 247M 8s 124700K .......... .......... .......... .......... .......... 47% 239M 8s 124750K .......... .......... .......... .......... .......... 47% 267M 8s 124800K .......... .......... .......... .......... .......... 47% 268M 8s 124850K .......... .......... .......... .......... .......... 47% 233M 8s 124900K .......... .......... .......... .......... .......... 47% 4.70M 8s 124950K .......... .......... .......... .......... .......... 47% 93.4M 8s 125000K .......... .......... .......... .......... .......... 47% 261M 8s 125050K .......... .......... .......... .......... .......... 47% 228M 8s 125100K .......... .......... .......... .......... .......... 47% 274M 8s 125150K .......... .......... .......... .......... .......... 47% 317M 8s 125200K .......... .......... .......... .......... .......... 47% 213M 8s 125250K .......... .......... .......... .......... .......... 47% 217M 8s 125300K .......... .......... .......... .......... .......... 47% 224M 8s 125350K .......... .......... .......... .......... .......... 47% 197M 8s 125400K .......... .......... .......... .......... .......... 47% 229M 8s 125450K .......... .......... .......... .......... .......... 47% 197M 8s 125500K .......... .......... .......... .......... .......... 47% 230M 8s 125550K .......... .......... .......... .......... .......... 47% 230M 8s 125600K .......... .......... .......... .......... .......... 47% 200M 8s 125650K .......... .......... .......... .......... .......... 47% 231M 8s 125700K .......... .......... .......... .......... .......... 47% 198M 8s 125750K .......... .......... .......... .......... .......... 47% 137M 8s 125800K .......... .......... .......... .......... .......... 47% 1.71M 8s 125850K .......... .......... .......... .......... .......... 48% 157M 8s 125900K .......... .......... .......... .......... .......... 48% 97.5M 8s 125950K .......... .......... .......... .......... .......... 48% 202M 8s 126000K .......... .......... .......... .......... .......... 48% 206M 8s 126050K .......... .......... .......... .......... .......... 48% 90.3M 8s 126100K .......... .......... .......... .......... .......... 48% 128M 8s 126150K .......... .......... .......... .......... .......... 48% 166M 8s 126200K .......... .......... .......... .......... .......... 48% 100M 8s 126250K .......... .......... .......... .......... .......... 48% 84.3M 8s 126300K .......... .......... .......... .......... .......... 48% 126M 8s 126350K .......... .......... .......... .......... .......... 48% 159M 8s 126400K .......... .......... .......... .......... .......... 48% 184M 8s 126450K .......... .......... .......... .......... .......... 48% 2.63M 8s 126500K .......... .......... .......... .......... .......... 48% 200M 8s 126550K .......... .......... .......... .......... .......... 48% 92.8M 8s 126600K .......... .......... .......... .......... .......... 48% 26.7M 8s 126650K .......... .......... .......... .......... .......... 48% 119M 8s 126700K .......... .......... .......... .......... .......... 48% 105M 8s 126750K .......... .......... .......... .......... .......... 48% 159M 8s 126800K .......... .......... .......... .......... .......... 48% 253M 8s 126850K .......... .......... .......... .......... .......... 48% 268M 8s 126900K .......... .......... .......... .......... .......... 48% 164M 8s 126950K .......... .......... .......... .......... .......... 48% 132M 8s 127000K .......... .......... .......... .......... .......... 48% 291M 8s 127050K .......... .......... .......... .......... .......... 48% 307M 8s 127100K .......... .......... .......... .......... .......... 48% 107M 8s 127150K .......... .......... .......... .......... .......... 48% 151M 8s 127200K .......... .......... .......... .......... .......... 48% 86.3M 8s 127250K .......... .......... .......... .......... .......... 48% 254M 8s 127300K .......... .......... .......... .......... .......... 48% 307M 8s 127350K .......... .......... .......... .......... .......... 48% 164M 8s 127400K .......... .......... .......... .......... .......... 48% 180M 8s 127450K .......... .......... .......... .......... .......... 48% 3.05M 8s 127500K .......... .......... .......... .......... .......... 48% 85.1M 8s 127550K .......... .......... .......... .......... .......... 48% 235M 8s 127600K .......... .......... .......... .......... .......... 48% 202M 8s 127650K .......... .......... .......... .......... .......... 48% 238M 8s 127700K .......... .......... .......... .......... .......... 48% 170M 8s 127750K .......... .......... .......... .......... .......... 48% 210M 8s 127800K .......... .......... .......... .......... .......... 48% 211M 8s 127850K .......... .......... .......... .......... .......... 48% 203M 8s 127900K .......... .......... .......... .......... .......... 48% 213M 8s 127950K .......... .......... .......... .......... .......... 48% 154M 8s 128000K .......... .......... .......... .......... .......... 48% 180M 8s 128050K .......... .......... .......... .......... .......... 48% 238M 8s 128100K .......... .......... .......... .......... .......... 48% 202M 8s 128150K .......... .......... .......... .......... .......... 48% 238M 8s 128200K .......... .......... .......... .......... .......... 48% 208M 8s 128250K .......... .......... .......... .......... .......... 48% 2.73M 8s 128300K .......... .......... .......... .......... .......... 48% 140M 8s 128350K .......... .......... .......... .......... .......... 48% 162M 8s 128400K .......... .......... .......... .......... .......... 48% 221M 8s 128450K .......... .......... .......... .......... .......... 49% 182M 8s 128500K .......... .......... .......... .......... .......... 49% 168M 8s 128550K .......... .......... .......... .......... .......... 49% 169M 8s 128600K .......... .......... .......... .......... .......... 49% 204M 8s 128650K .......... .......... .......... .......... .......... 49% 243M 8s 128700K .......... .......... .......... .......... .......... 49% 185M 8s 128750K .......... .......... .......... .......... .......... 49% 263M 8s 128800K .......... .......... .......... .......... .......... 49% 217M 8s 128850K .......... .......... .......... .......... .......... 49% 204M 8s 128900K .......... .......... .......... .......... .......... 49% 155M 8s 128950K .......... .......... .......... .......... .......... 49% 109M 8s 129000K .......... .......... .......... .......... .......... 49% 226M 8s 129050K .......... .......... .......... .......... .......... 49% 257M 8s 129100K .......... .......... .......... .......... .......... 49% 2.06M 8s 129150K .......... .......... .......... .......... .......... 49% 122M 8s 129200K .......... .......... .......... .......... .......... 49% 76.3M 8s 129250K .......... .......... .......... .......... .......... 49% 182M 8s 129300K .......... .......... .......... .......... .......... 49% 217M 8s 129350K .......... .......... .......... .......... .......... 49% 154M 8s 129400K .......... .......... .......... .......... .......... 49% 211M 8s 129450K .......... .......... .......... .......... .......... 49% 171M 8s 129500K .......... .......... .......... .......... .......... 49% 172M 8s 129550K .......... .......... .......... .......... .......... 49% 225M 8s 129600K .......... .......... .......... .......... .......... 49% 203M 8s 129650K .......... .......... .......... .......... .......... 49% 241M 8s 129700K .......... .......... .......... .......... .......... 49% 206M 8s 129750K .......... .......... .......... .......... .......... 49% 242M 8s 129800K .......... .......... .......... .......... .......... 49% 243M 8s 129850K .......... .......... .......... .......... .......... 49% 184M 8s 129900K .......... .......... .......... .......... .......... 49% 1.93M 8s 129950K .......... .......... .......... .......... .......... 49% 96.9M 8s 130000K .......... .......... .......... .......... .......... 49% 194M 8s 130050K .......... .......... .......... .......... .......... 49% 73.1M 8s 130100K .......... .......... .......... .......... .......... 49% 95.9M 8s 130150K .......... .......... .......... .......... .......... 49% 160M 8s 130200K .......... .......... .......... .......... .......... 49% 151M 8s 130250K .......... .......... .......... .......... .......... 49% 143M 8s 130300K .......... .......... .......... .......... .......... 49% 166M 8s 130350K .......... .......... .......... .......... .......... 49% 186M 8s 130400K .......... .......... .......... .......... .......... 49% 185M 8s 130450K .......... .......... .......... .......... .......... 49% 156M 8s 130500K .......... .......... .......... .......... .......... 49% 146M 8s 130550K .......... .......... .......... .......... .......... 49% 2.18M 8s 130600K .......... .......... .......... .......... .......... 49% 93.7M 8s 130650K .......... .......... .......... .......... .......... 49% 140M 8s 130700K .......... .......... .......... .......... .......... 49% 211M 8s 130750K .......... .......... .......... .......... .......... 49% 218M 8s 130800K .......... .......... .......... .......... .......... 49% 131M 8s 130850K .......... .......... .......... .......... .......... 49% 176M 8s 130900K .......... .......... .......... .......... .......... 49% 109M 8s 130950K .......... .......... .......... .......... .......... 49% 95.0M 8s 131000K .......... .......... .......... .......... .......... 49% 226M 8s 131050K .......... .......... .......... .......... .......... 49% 195M 8s 131100K .......... .......... .......... .......... .......... 50% 286M 8s 131150K .......... .......... .......... .......... .......... 50% 183M 8s 131200K .......... .......... .......... .......... .......... 50% 221M 8s 131250K .......... .......... .......... .......... .......... 50% 173M 8s 131300K .......... .......... .......... .......... .......... 50% 133M 8s 131350K .......... .......... .......... .......... .......... 50% 164M 8s 131400K .......... .......... .......... .......... .......... 50% 274M 8s 131450K .......... .......... .......... .......... .......... 50% 276M 8s 131500K .......... .......... .......... .......... .......... 50% 334M 8s 131550K .......... .......... .......... .......... .......... 50% 2.85M 8s 131600K .......... .......... .......... .......... .......... 50% 131M 8s 131650K .......... .......... .......... .......... .......... 50% 124M 8s 131700K .......... .......... .......... .......... .......... 50% 150M 8s 131750K .......... .......... .......... .......... .......... 50% 188M 8s 131800K .......... .......... .......... .......... .......... 50% 217M 8s 131850K .......... .......... .......... .......... .......... 50% 121M 8s 131900K .......... .......... .......... .......... .......... 50% 236M 8s 131950K .......... .......... .......... .......... .......... 50% 126M 8s 132000K .......... .......... .......... .......... .......... 50% 178M 8s 132050K .......... .......... .......... .......... .......... 50% 204M 8s 132100K .......... .......... .......... .......... .......... 50% 455K 8s 132150K .......... .......... .......... .......... .......... 50% 180M 8s 132200K .......... .......... .......... .......... .......... 50% 121M 8s 132250K .......... .......... .......... .......... .......... 50% 102M 8s 132300K .......... .......... .......... .......... .......... 50% 119M 8s 132350K .......... .......... .......... .......... .......... 50% 138M 8s 132400K .......... .......... .......... .......... .......... 50% 235M 8s 132450K .......... .......... .......... .......... .......... 50% 99.2M 8s 132500K .......... .......... .......... .......... .......... 50% 96.9M 8s 132550K .......... .......... .......... .......... .......... 50% 138M 8s 132600K .......... .......... .......... .......... .......... 50% 131M 8s 132650K .......... .......... .......... .......... .......... 50% 212M 8s 132700K .......... .......... .......... .......... .......... 50% 160M 8s 132750K .......... .......... .......... .......... .......... 50% 83.8M 8s 132800K .......... .......... .......... .......... .......... 50% 228M 8s 132850K .......... .......... .......... .......... .......... 50% 201M 8s 132900K .......... .......... .......... .......... .......... 50% 236M 8s 132950K .......... .......... .......... .......... .......... 50% 197M 8s 133000K .......... .......... .......... .......... .......... 50% 218M 8s 133050K .......... .......... .......... .......... .......... 50% 238M 8s 133100K .......... .......... .......... .......... .......... 50% 132M 8s 133150K .......... .......... .......... .......... .......... 50% 174M 8s 133200K .......... .......... .......... .......... .......... 50% 199M 8s 133250K .......... .......... .......... .......... .......... 50% 186M 8s 133300K .......... .......... .......... .......... .......... 50% 148M 8s 133350K .......... .......... .......... .......... .......... 50% 120M 8s 133400K .......... .......... .......... .......... .......... 50% 253M 8s 133450K .......... .......... .......... .......... .......... 50% 167M 8s 133500K .......... .......... .......... .......... .......... 50% 219M 8s 133550K .......... .......... .......... .......... .......... 50% 211M 8s 133600K .......... .......... .......... .......... .......... 50% 178M 7s 133650K .......... .......... .......... .......... .......... 50% 236M 7s 133700K .......... .......... .......... .......... .......... 51% 99.6M 7s 133750K .......... .......... .......... .......... .......... 51% 192M 7s 133800K .......... .......... .......... .......... .......... 51% 182M 7s 133850K .......... .......... .......... .......... .......... 51% 161M 7s 133900K .......... .......... .......... .......... .......... 51% 267M 7s 133950K .......... .......... .......... .......... .......... 51% 183M 7s 134000K .......... .......... .......... .......... .......... 51% 182M 7s 134050K .......... .......... .......... .......... .......... 51% 228M 7s 134100K .......... .......... .......... .......... .......... 51% 263K 8s 134150K .......... .......... .......... .......... .......... 51% 80.2M 8s 134200K .......... .......... .......... .......... .......... 51% 145M 8s 134250K .......... .......... .......... .......... .......... 51% 189M 8s 134300K .......... .......... .......... .......... .......... 51% 179M 8s 134350K .......... .......... .......... .......... .......... 51% 113M 8s 134400K .......... .......... .......... .......... .......... 51% 56.6M 8s 134450K .......... .......... .......... .......... .......... 51% 136M 8s 134500K .......... .......... .......... .......... .......... 51% 166M 8s 134550K .......... .......... .......... .......... .......... 51% 162M 8s 134600K .......... .......... .......... .......... .......... 51% 155M 8s 134650K .......... .......... .......... .......... .......... 51% 176M 8s 134700K .......... .......... .......... .......... .......... 51% 157M 8s 134750K .......... .......... .......... .......... .......... 51% 169M 8s 134800K .......... .......... .......... .......... .......... 51% 192M 8s 134850K .......... .......... .......... .......... .......... 51% 191M 8s 134900K .......... .......... .......... .......... .......... 51% 206M 8s 134950K .......... .......... .......... .......... .......... 51% 198M 8s 135000K .......... .......... .......... .......... .......... 51% 225M 8s 135050K .......... .......... .......... .......... .......... 51% 224M 8s 135100K .......... .......... .......... .......... .......... 51% 130M 8s 135150K .......... .......... .......... .......... .......... 51% 117M 8s 135200K .......... .......... .......... .......... .......... 51% 155M 8s 135250K .......... .......... .......... .......... .......... 51% 260M 7s 135300K .......... .......... .......... .......... .......... 51% 161M 7s 135350K .......... .......... .......... .......... .......... 51% 144M 7s 135400K .......... .......... .......... .......... .......... 51% 175M 7s 135450K .......... .......... .......... .......... .......... 51% 151M 7s 135500K .......... .......... .......... .......... .......... 51% 229M 7s 135550K .......... .......... .......... .......... .......... 51% 237M 7s 135600K .......... .......... .......... .......... .......... 51% 202M 7s 135650K .......... .......... .......... .......... .......... 51% 243M 7s 135700K .......... .......... .......... .......... .......... 51% 204M 7s 135750K .......... .......... .......... .......... .......... 51% 239M 7s 135800K .......... .......... .......... .......... .......... 51% 243M 7s 135850K .......... .......... .......... .......... .......... 51% 165M 7s 135900K .......... .......... .......... .......... .......... 51% 141M 7s 135950K .......... .......... .......... .......... .......... 51% 191M 7s 136000K .......... .......... .......... .......... .......... 51% 224M 7s 136050K .......... .......... .......... .......... .......... 51% 195M 7s 136100K .......... .......... .......... .......... .......... 51% 173M 7s 136150K .......... .......... .......... .......... .......... 51% 2.14M 7s 136200K .......... .......... .......... .......... .......... 51% 62.4M 7s 136250K .......... .......... .......... .......... .......... 51% 112M 7s 136300K .......... .......... .......... .......... .......... 52% 210M 7s 136350K .......... .......... .......... .......... .......... 52% 243M 7s 136400K .......... .......... .......... .......... .......... 52% 83.6M 7s 136450K .......... .......... .......... .......... .......... 52% 277M 7s 136500K .......... .......... .......... .......... .......... 52% 296M 7s 136550K .......... .......... .......... .......... .......... 52% 247M 7s 136600K .......... .......... .......... .......... .......... 52% 294M 7s 136650K .......... .......... .......... .......... .......... 52% 287M 7s 136700K .......... .......... .......... .......... .......... 52% 236M 7s 136750K .......... .......... .......... .......... .......... 52% 334M 7s 136800K .......... .......... .......... .......... .......... 52% 273M 7s 136850K .......... .......... .......... .......... .......... 52% 205M 7s 136900K .......... .......... .......... .......... .......... 52% 298M 7s 136950K .......... .......... .......... .......... .......... 52% 296M 7s 137000K .......... .......... .......... .......... .......... 52% 222M 7s 137050K .......... .......... .......... .......... .......... 52% 281M 7s 137100K .......... .......... .......... .......... .......... 52% 236M 7s 137150K .......... .......... .......... .......... .......... 52% 229M 7s 137200K .......... .......... .......... .......... .......... 52% 229K 8s 137250K .......... .......... .......... .......... .......... 52% 112M 7s 137300K .......... .......... .......... .......... .......... 52% 117M 7s 137350K .......... .......... .......... .......... .......... 52% 149M 7s 137400K .......... .......... .......... .......... .......... 52% 41.2M 7s 137450K .......... .......... .......... .......... .......... 52% 104M 7s 137500K .......... .......... .......... .......... .......... 52% 216M 7s 137550K .......... .......... .......... .......... .......... 52% 144M 7s 137600K .......... .......... .......... .......... .......... 52% 148M 7s 137650K .......... .......... .......... .......... .......... 52% 208M 7s 137700K .......... .......... .......... .......... .......... 52% 180M 7s 137750K .......... .......... .......... .......... .......... 52% 158M 7s 137800K .......... .......... .......... .......... .......... 52% 152M 7s 137850K .......... .......... .......... .......... .......... 52% 59.0M 7s 137900K .......... .......... .......... .......... .......... 52% 203M 7s 137950K .......... .......... .......... .......... .......... 52% 131M 7s 138000K .......... .......... .......... .......... .......... 52% 79.9M 7s 138050K .......... .......... .......... .......... .......... 52% 197M 7s 138100K .......... .......... .......... .......... .......... 52% 180M 7s 138150K .......... .......... .......... .......... .......... 52% 203M 7s 138200K .......... .......... .......... .......... .......... 52% 76.3M 7s 138250K .......... .......... .......... .......... .......... 52% 93.0M 7s 138300K .......... .......... .......... .......... .......... 52% 76.3M 7s 138350K .......... .......... .......... .......... .......... 52% 124M 7s 138400K .......... .......... .......... .......... .......... 52% 66.1M 7s 138450K .......... .......... .......... .......... .......... 52% 117M 7s 138500K .......... .......... .......... .......... .......... 52% 201M 7s 138550K .......... .......... .......... .......... .......... 52% 99.4M 7s 138600K .......... .......... .......... .......... .......... 52% 56.9M 7s 138650K .......... .......... .......... .......... .......... 52% 128M 7s 138700K .......... .......... .......... .......... .......... 52% 92.5M 7s 138750K .......... .......... .......... .......... .......... 52% 174M 7s 138800K .......... .......... .......... .......... .......... 52% 119M 7s 138850K .......... .......... .......... .......... .......... 52% 116M 7s 138900K .......... .......... .......... .......... .......... 52% 92.1M 7s 138950K .......... .......... .......... .......... .......... 53% 89.9M 7s 139000K .......... .......... .......... .......... .......... 53% 99.4M 7s 139050K .......... .......... .......... .......... .......... 53% 89.1M 7s 139100K .......... .......... .......... .......... .......... 53% 73.1M 7s 139150K .......... .......... .......... .......... .......... 53% 143M 7s 139200K .......... .......... .......... .......... .......... 53% 128M 7s 139250K .......... .......... .......... .......... .......... 53% 75.1M 7s 139300K .......... .......... .......... .......... .......... 53% 170M 7s 139350K .......... .......... .......... .......... .......... 53% 73.1M 7s 139400K .......... .......... .......... .......... .......... 53% 131M 7s 139450K .......... .......... .......... .......... .......... 53% 120M 7s 139500K .......... .......... .......... .......... .......... 53% 204M 7s 139550K .......... .......... .......... .......... .......... 53% 207M 7s 139600K .......... .......... .......... .......... .......... 53% 186M 7s 139650K .......... .......... .......... .......... .......... 53% 206M 7s 139700K .......... .......... .......... .......... .......... 53% 182M 7s 139750K .......... .......... .......... .......... .......... 53% 213M 7s 139800K .......... .......... .......... .......... .......... 53% 204M 7s 139850K .......... .......... .......... .......... .......... 53% 177M 7s 139900K .......... .......... .......... .......... .......... 53% 187M 7s 139950K .......... .......... .......... .......... .......... 53% 148M 7s 140000K .......... .......... .......... .......... .......... 53% 264M 7s 140050K .......... .......... .......... .......... .......... 53% 270M 7s 140100K .......... .......... .......... .......... .......... 53% 231M 7s 140150K .......... .......... .......... .......... .......... 53% 185M 7s 140200K .......... .......... .......... .......... .......... 53% 193M 7s 140250K .......... .......... .......... .......... .......... 53% 3.93M 7s 140300K .......... .......... .......... .......... .......... 53% 174M 7s 140350K .......... .......... .......... .......... .......... 53% 113M 7s 140400K .......... .......... .......... .......... .......... 53% 210M 7s 140450K .......... .......... .......... .......... .......... 53% 187M 7s 140500K .......... .......... .......... .......... .......... 53% 106M 7s 140550K .......... .......... .......... .......... .......... 53% 131M 7s 140600K .......... .......... .......... .......... .......... 53% 123M 7s 140650K .......... .......... .......... .......... .......... 53% 162M 7s 140700K .......... .......... .......... .......... .......... 53% 177M 7s 140750K .......... .......... .......... .......... .......... 53% 218M 7s 140800K .......... .......... .......... .......... .......... 53% 170M 7s 140850K .......... .......... .......... .......... .......... 53% 189M 7s 140900K .......... .......... .......... .......... .......... 53% 216M 7s 140950K .......... .......... .......... .......... .......... 53% 184M 7s 141000K .......... .......... .......... .......... .......... 53% 209M 7s 141050K .......... .......... .......... .......... .......... 53% 216M 7s 141100K .......... .......... .......... .......... .......... 53% 191M 7s 141150K .......... .......... .......... .......... .......... 53% 211M 7s 141200K .......... .......... .......... .......... .......... 53% 199M 7s 141250K .......... .......... .......... .......... .......... 53% 235M 7s 141300K .......... .......... .......... .......... .......... 53% 2.02M 7s 141350K .......... .......... .......... .......... .......... 53% 68.6M 7s 141400K .......... .......... .......... .......... .......... 53% 4.81M 7s 141450K .......... .......... .......... .......... .......... 53% 3.25M 7s 141500K .......... .......... .......... .......... .......... 53% 28.3M 7s 141550K .......... .......... .......... .......... .......... 54% 300M 7s 141600K .......... .......... .......... .......... .......... 54% 267M 7s 141650K .......... .......... .......... .......... .......... 54% 258M 7s 141700K .......... .......... .......... .......... .......... 54% 191M 7s 141750K .......... .......... .......... .......... .......... 54% 108M 7s 141800K .......... .......... .......... .......... .......... 54% 258M 7s 141850K .......... .......... .......... .......... .......... 54% 163M 7s 141900K .......... .......... .......... .......... .......... 54% 303M 7s 141950K .......... .......... .......... .......... .......... 54% 281M 7s 142000K .......... .......... .......... .......... .......... 54% 301M 7s 142050K .......... .......... .......... .......... .......... 54% 341M 7s 142100K .......... .......... .......... .......... .......... 54% 231M 7s 142150K .......... .......... .......... .......... .......... 54% 344M 7s 142200K .......... .......... .......... .......... .......... 54% 289M 7s 142250K .......... .......... .......... .......... .......... 54% 257M 7s 142300K .......... .......... .......... .......... .......... 54% 3.79M 7s 142350K .......... .......... .......... .......... .......... 54% 11.7M 7s 142400K .......... .......... .......... .......... .......... 54% 20.1M 7s 142450K .......... .......... .......... .......... .......... 54% 12.1M 7s 142500K .......... .......... .......... .......... .......... 54% 26.1M 7s 142550K .......... .......... .......... .......... .......... 54% 53.8M 7s 142600K .......... .......... .......... .......... .......... 54% 2.76M 7s 142650K .......... .......... .......... .......... .......... 54% 16.7M 7s 142700K .......... .......... .......... .......... .......... 54% 22.9M 7s 142750K .......... .......... .......... .......... .......... 54% 28.3M 7s 142800K .......... .......... .......... .......... .......... 54% 172M 7s 142850K .......... .......... .......... .......... .......... 54% 174M 7s 142900K .......... .......... .......... .......... .......... 54% 142M 7s 142950K .......... .......... .......... .......... .......... 54% 140M 7s 143000K .......... .......... .......... .......... .......... 54% 209M 7s 143050K .......... .......... .......... .......... .......... 54% 211M 7s 143100K .......... .......... .......... .......... .......... 54% 153M 7s 143150K .......... .......... .......... .......... .......... 54% 214M 7s 143200K .......... .......... .......... .......... .......... 54% 187M 7s 143250K .......... .......... .......... .......... .......... 54% 332M 7s 143300K .......... .......... .......... .......... .......... 54% 349M 7s 143350K .......... .......... .......... .......... .......... 54% 215M 7s 143400K .......... .......... .......... .......... .......... 54% 341M 7s 143450K .......... .......... .......... .......... .......... 54% 300M 7s 143500K .......... .......... .......... .......... .......... 54% 346M 7s 143550K .......... .......... .......... .......... .......... 54% 349M 7s 143600K .......... .......... .......... .......... .......... 54% 292M 7s 143650K .......... .......... .......... .......... .......... 54% 351M 7s 143700K .......... .......... .......... .......... .......... 54% 282M 7s 143750K .......... .......... .......... .......... .......... 54% 344M 7s 143800K .......... .......... .......... .......... .......... 54% 349M 7s 143850K .......... .......... .......... .......... .......... 54% 301M 7s 143900K .......... .......... .......... .......... .......... 54% 341M 7s 143950K .......... .......... .......... .......... .......... 54% 301M 7s 144000K .......... .......... .......... .......... .......... 54% 351M 7s 144050K .......... .......... .......... .......... .......... 54% 344M 7s 144100K .......... .......... .......... .......... .......... 54% 296M 7s 144150K .......... .......... .......... .......... .......... 54% 344M 7s 144200K .......... .......... .......... .......... .......... 55% 303M 7s 144250K .......... .......... .......... .......... .......... 55% 349M 7s 144300K .......... .......... .......... .......... .......... 55% 351M 7s 144350K .......... .......... .......... .......... .......... 55% 12.8M 7s 144400K .......... .......... .......... .......... .......... 55% 160M 7s 144450K .......... .......... .......... .......... .......... 55% 5.47M 7s 144500K .......... .......... .......... .......... .......... 55% 109M 7s 144550K .......... .......... .......... .......... .......... 55% 175M 7s 144600K .......... .......... .......... .......... .......... 55% 220M 7s 144650K .......... .......... .......... .......... .......... 55% 277M 7s 144700K .......... .......... .......... .......... .......... 55% 271M 7s 144750K .......... .......... .......... .......... .......... 55% 286M 7s 144800K .......... .......... .......... .......... .......... 55% 138M 7s 144850K .......... .......... .......... .......... .......... 55% 182M 7s 144900K .......... .......... .......... .......... .......... 55% 221M 7s 144950K .......... .......... .......... .......... .......... 55% 193M 7s 145000K .......... .......... .......... .......... .......... 55% 193M 7s 145050K .......... .......... .......... .......... .......... 55% 210M 7s 145100K .......... .......... .......... .......... .......... 55% 237M 7s 145150K .......... .......... .......... .......... .......... 55% 189M 7s 145200K .......... .......... .......... .......... .......... 55% 174M 7s 145250K .......... .......... .......... .......... .......... 55% 210M 7s 145300K .......... .......... .......... .......... .......... 55% 238M 7s 145350K .......... .......... .......... .......... .......... 55% 206M 7s 145400K .......... .......... .......... .......... .......... 55% 3.00M 7s 145450K .......... .......... .......... .......... .......... 55% 204M 7s 145500K .......... .......... .......... .......... .......... 55% 292M 7s 145550K .......... .......... .......... .......... .......... 55% 223M 7s 145600K .......... .......... .......... .......... .......... 55% 140M 7s 145650K .......... .......... .......... .......... .......... 55% 131M 7s 145700K .......... .......... .......... .......... .......... 55% 128M 7s 145750K .......... .......... .......... .......... .......... 55% 235M 7s 145800K .......... .......... .......... .......... .......... 55% 257M 7s 145850K .......... .......... .......... .......... .......... 55% 252M 7s 145900K .......... .......... .......... .......... .......... 55% 334M 7s 145950K .......... .......... .......... .......... .......... 55% 292M 7s 146000K .......... .......... .......... .......... .......... 55% 344M 7s 146050K .......... .......... .......... .......... .......... 55% 346M 7s 146100K .......... .......... .......... .......... .......... 55% 298M 7s 146150K .......... .......... .......... .......... .......... 55% 339M 7s 146200K .......... .......... .......... .......... .......... 55% 298M 7s 146250K .......... .......... .......... .......... .......... 55% 344M 7s 146300K .......... .......... .......... .......... .......... 55% 346M 7s 146350K .......... .......... .......... .......... .......... 55% 296M 7s 146400K .......... .......... .......... .......... .......... 55% 224M 7s 146450K .......... .......... .......... .......... .......... 55% 289M 7s 146500K .......... .......... .......... .......... .......... 55% 115M 7s 146550K .......... .......... .......... .......... .......... 55% 178M 7s 146600K .......... .......... .......... .......... .......... 55% 67.7M 7s 146650K .......... .......... .......... .......... .......... 55% 205M 7s 146700K .......... .......... .......... .......... .......... 55% 163M 7s 146750K .......... .......... .......... .......... .......... 55% 238M 7s 146800K .......... .......... .......... .......... .......... 56% 226M 7s 146850K .......... .......... .......... .......... .......... 56% 1.63M 7s 146900K .......... .......... .......... .......... .......... 56% 89.4M 7s 146950K .......... .......... .......... .......... .......... 56% 128M 7s 147000K .......... .......... .......... .......... .......... 56% 148M 7s 147050K .......... .......... .......... .......... .......... 56% 145M 7s 147100K .......... .......... .......... .......... .......... 56% 82.1M 7s 147150K .......... .......... .......... .......... .......... 56% 149M 7s 147200K .......... .......... .......... .......... .......... 56% 177M 7s 147250K .......... .......... .......... .......... .......... 56% 55.3M 7s 147300K .......... .......... .......... .......... .......... 56% 260M 7s 147350K .......... .......... .......... .......... .......... 56% 136M 7s 147400K .......... .......... .......... .......... .......... 56% 81.2M 7s 147450K .......... .......... .......... .......... .......... 56% 2.03M 7s 147500K .......... .......... .......... .......... .......... 56% 282M 7s 147550K .......... .......... .......... .......... .......... 56% 263M 7s 147600K .......... .......... .......... .......... .......... 56% 189M 7s 147650K .......... .......... .......... .......... .......... 56% 190M 7s 147700K .......... .......... .......... .......... .......... 56% 182M 7s 147750K .......... .......... .......... .......... .......... 56% 215M 7s 147800K .......... .......... .......... .......... .......... 56% 110M 7s 147850K .......... .......... .......... .......... .......... 56% 182M 7s 147900K .......... .......... .......... .......... .......... 56% 119M 7s 147950K .......... .......... .......... .......... .......... 56% 93.7M 7s 148000K .......... .......... .......... .......... .......... 56% 210M 7s 148050K .......... .......... .......... .......... .......... 56% 88.8M 7s 148100K .......... .......... .......... .......... .......... 56% 86.4M 7s 148150K .......... .......... .......... .......... .......... 56% 156M 7s 148200K .......... .......... .......... .......... .......... 56% 171M 7s 148250K .......... .......... .......... .......... .......... 56% 328M 7s 148300K .......... .......... .......... .......... .......... 56% 339M 7s 148350K .......... .......... .......... .......... .......... 56% 97.7M 7s 148400K .......... .......... .......... .......... .......... 56% 37.2M 7s 148450K .......... .......... .......... .......... .......... 56% 2.35M 7s 148500K .......... .......... .......... .......... .......... 56% 153M 7s 148550K .......... .......... .......... .......... .......... 56% 152M 7s 148600K .......... .......... .......... .......... .......... 56% 186M 7s 148650K .......... .......... .......... .......... .......... 56% 137M 7s 148700K .......... .......... .......... .......... .......... 56% 292M 7s 148750K .......... .......... .......... .......... .......... 56% 344M 6s 148800K .......... .......... .......... .......... .......... 56% 344M 6s 148850K .......... .......... .......... .......... .......... 56% 296M 6s 148900K .......... .......... .......... .......... .......... 56% 207M 6s 148950K .......... .......... .......... .......... .......... 56% 188M 6s 149000K .......... .......... .......... .......... .......... 56% 187M 6s 149050K .......... .......... .......... .......... .......... 56% 2.23M 6s 149100K .......... .......... .......... .......... .......... 56% 193M 6s 149150K .......... .......... .......... .......... .......... 56% 194M 6s 149200K .......... .......... .......... .......... .......... 56% 64.8M 6s 149250K .......... .......... .......... .......... .......... 56% 120M 6s 149300K .......... .......... .......... .......... .......... 56% 36.0M 6s 149350K .......... .......... .......... .......... .......... 56% 148M 6s 149400K .......... .......... .......... .......... .......... 56% 150M 6s 149450K .......... .......... .......... .......... .......... 57% 225M 6s 149500K .......... .......... .......... .......... .......... 57% 374K 7s 149550K .......... .......... .......... .......... .......... 57% 200M 7s 149600K .......... .......... .......... .......... .......... 57% 80.2M 7s 149650K .......... .......... .......... .......... .......... 57% 106M 7s 149700K .......... .......... .......... .......... .......... 57% 109M 7s 149750K .......... .......... .......... .......... .......... 57% 80.2M 7s 149800K .......... .......... .......... .......... .......... 57% 108M 7s 149850K .......... .......... .......... .......... .......... 57% 171M 7s 149900K .......... .......... .......... .......... .......... 57% 92.7M 7s 149950K .......... .......... .......... .......... .......... 57% 133M 6s 150000K .......... .......... .......... .......... .......... 57% 189M 6s 150050K .......... .......... .......... .......... .......... 57% 199M 6s 150100K .......... .......... .......... .......... .......... 57% 130M 6s 150150K .......... .......... .......... .......... .......... 57% 196M 6s 150200K .......... .......... .......... .......... .......... 57% 197M 6s 150250K .......... .......... .......... .......... .......... 57% 216M 6s 150300K .......... .......... .......... .......... .......... 57% 225M 6s 150350K .......... .......... .......... .......... .......... 57% 68.8M 6s 150400K .......... .......... .......... .......... .......... 57% 43.6M 6s 150450K .......... .......... .......... .......... .......... 57% 150M 6s 150500K .......... .......... .......... .......... .......... 57% 2.46M 6s 150550K .......... .......... .......... .......... .......... 57% 200M 6s 150600K .......... .......... .......... .......... .......... 57% 72.9M 6s 150650K .......... .......... .......... .......... .......... 57% 141M 6s 150700K .......... .......... .......... .......... .......... 57% 132M 6s 150750K .......... .......... .......... .......... .......... 57% 276M 6s 150800K .......... .......... .......... .......... .......... 57% 188M 6s 150850K .......... .......... .......... .......... .......... 57% 170M 6s 150900K .......... .......... .......... .......... .......... 57% 140M 6s 150950K .......... .......... .......... .......... .......... 57% 110M 6s 151000K .......... .......... .......... .......... .......... 57% 65.0M 6s 151050K .......... .......... .......... .......... .......... 57% 167M 6s 151100K .......... .......... .......... .......... .......... 57% 1.79M 6s 151150K .......... .......... .......... .......... .......... 57% 106M 6s 151200K .......... .......... .......... .......... .......... 57% 119M 6s 151250K .......... .......... .......... .......... .......... 57% 189M 6s 151300K .......... .......... .......... .......... .......... 57% 130M 6s 151350K .......... .......... .......... .......... .......... 57% 121M 6s 151400K .......... .......... .......... .......... .......... 57% 178M 6s 151450K .......... .......... .......... .......... .......... 57% 123M 6s 151500K .......... .......... .......... .......... .......... 57% 191M 6s 151550K .......... .......... .......... .......... .......... 57% 409K 6s 151600K .......... .......... .......... .......... .......... 57% 138M 6s 151650K .......... .......... .......... .......... .......... 57% 178M 6s 151700K .......... .......... .......... .......... .......... 57% 124M 6s 151750K .......... .......... .......... .......... .......... 57% 179M 6s 151800K .......... .......... .......... .......... .......... 57% 264M 6s 151850K .......... .......... .......... .......... .......... 57% 244M 6s 151900K .......... .......... .......... .......... .......... 57% 69.0M 6s 151950K .......... .......... .......... .......... .......... 57% 142M 6s 152000K .......... .......... .......... .......... .......... 57% 140M 6s 152050K .......... .......... .......... .......... .......... 58% 167M 6s 152100K .......... .......... .......... .......... .......... 58% 179M 6s 152150K .......... .......... .......... .......... .......... 58% 226M 6s 152200K .......... .......... .......... .......... .......... 58% 193M 6s 152250K .......... .......... .......... .......... .......... 58% 152M 6s 152300K .......... .......... .......... .......... .......... 58% 124M 6s 152350K .......... .......... .......... .......... .......... 58% 138M 6s 152400K .......... .......... .......... .......... .......... 58% 105M 6s 152450K .......... .......... .......... .......... .......... 58% 85.8M 6s 152500K .......... .......... .......... .......... .......... 58% 178M 6s 152550K .......... .......... .......... .......... .......... 58% 1.71M 6s 152600K .......... .......... .......... .......... .......... 58% 175M 6s 152650K .......... .......... .......... .......... .......... 58% 215M 6s 152700K .......... .......... .......... .......... .......... 58% 186M 6s 152750K .......... .......... .......... .......... .......... 58% 217M 6s 152800K .......... .......... .......... .......... .......... 58% 45.0M 6s 152850K .......... .......... .......... .......... .......... 58% 77.5M 6s 152900K .......... .......... .......... .......... .......... 58% 205M 6s 152950K .......... .......... .......... .......... .......... 58% 57.4M 6s 153000K .......... .......... .......... .......... .......... 58% 203M 6s 153050K .......... .......... .......... .......... .......... 58% 239M 6s 153100K .......... .......... .......... .......... .......... 58% 178M 6s 153150K .......... .......... .......... .......... .......... 58% 81.4M 6s 153200K .......... .......... .......... .......... .......... 58% 1.77M 6s 153250K .......... .......... .......... .......... .......... 58% 166M 6s 153300K .......... .......... .......... .......... .......... 58% 226M 6s 153350K .......... .......... .......... .......... .......... 58% 248M 6s 153400K .......... .......... .......... .......... .......... 58% 279M 6s 153450K .......... .......... .......... .......... .......... 58% 235M 6s 153500K .......... .......... .......... .......... .......... 58% 135M 6s 153550K .......... .......... .......... .......... .......... 58% 144M 6s 153600K .......... .......... .......... .......... .......... 58% 296K 6s 153650K .......... .......... .......... .......... .......... 58% 74.7M 6s 153700K .......... .......... .......... .......... .......... 58% 158M 6s 153750K .......... .......... .......... .......... .......... 58% 110M 6s 153800K .......... .......... .......... .......... .......... 58% 170M 6s 153850K .......... .......... .......... .......... .......... 58% 133M 6s 153900K .......... .......... .......... .......... .......... 58% 147M 6s 153950K .......... .......... .......... .......... .......... 58% 139M 6s 154000K .......... .......... .......... .......... .......... 58% 287M 6s 154050K .......... .......... .......... .......... .......... 58% 214M 6s 154100K .......... .......... .......... .......... .......... 58% 176M 6s 154150K .......... .......... .......... .......... .......... 58% 303M 6s 154200K .......... .......... .......... .......... .......... 58% 261M 6s 154250K .......... .......... .......... .......... .......... 58% 68.8M 6s 154300K .......... .......... .......... .......... .......... 58% 156M 6s 154350K .......... .......... .......... .......... .......... 58% 148M 6s 154400K .......... .......... .......... .......... .......... 58% 208M 6s 154450K .......... .......... .......... .......... .......... 58% 186M 6s 154500K .......... .......... .......... .......... .......... 58% 142M 6s 154550K .......... .......... .......... .......... .......... 58% 153M 6s 154600K .......... .......... .......... .......... .......... 58% 103M 6s 154650K .......... .......... .......... .......... .......... 58% 2.16M 6s 154700K .......... .......... .......... .......... .......... 59% 257M 6s 154750K .......... .......... .......... .......... .......... 59% 244M 6s 154800K .......... .......... .......... .......... .......... 59% 104M 6s 154850K .......... .......... .......... .......... .......... 59% 82.9M 6s 154900K .......... .......... .......... .......... .......... 59% 230M 6s 154950K .......... .......... .......... .......... .......... 59% 201M 6s 155000K .......... .......... .......... .......... .......... 59% 86.4M 6s 155050K .......... .......... .......... .......... .......... 59% 223M 6s 155100K .......... .......... .......... .......... .......... 59% 191M 6s 155150K .......... .......... .......... .......... .......... 59% 218M 6s 155200K .......... .......... .......... .......... .......... 59% 32.6M 6s 155250K .......... .......... .......... .......... .......... 59% 158M 6s 155300K .......... .......... .......... .......... .......... 59% 2.47M 6s 155350K .......... .......... .......... .......... .......... 59% 92.0K 7s 155400K .......... .......... .......... .......... .......... 59% 179M 7s 155450K .......... .......... .......... .......... .......... 59% 166M 7s 155500K .......... .......... .......... .......... .......... 59% 188M 7s 155550K .......... .......... .......... .......... .......... 59% 147M 7s 155600K .......... .......... .......... .......... .......... 59% 121M 7s 155650K .......... .......... .......... .......... .......... 59% 121M 7s 155700K .......... .......... .......... .......... .......... 59% 110M 7s 155750K .......... .......... .......... .......... .......... 59% 190M 7s 155800K .......... .......... .......... .......... .......... 59% 64.0M 7s 155850K .......... .......... .......... .......... .......... 59% 183M 7s 155900K .......... .......... .......... .......... .......... 59% 225M 7s 155950K .......... .......... .......... .......... .......... 59% 107M 7s 156000K .......... .......... .......... .......... .......... 59% 197M 7s 156050K .......... .......... .......... .......... .......... 59% 213M 7s 156100K .......... .......... .......... .......... .......... 59% 182M 7s 156150K .......... .......... .......... .......... .......... 59% 28.4M 7s 156200K .......... .......... .......... .......... .......... 59% 59.6M 7s 156250K .......... .......... .......... .......... .......... 59% 204M 7s 156300K .......... .......... .......... .......... .......... 59% 203M 7s 156350K .......... .......... .......... .......... .......... 59% 124M 7s 156400K .......... .......... .......... .......... .......... 59% 162M 7s 156450K .......... .......... .......... .......... .......... 59% 168M 7s 156500K .......... .......... .......... .......... .......... 59% 131M 7s 156550K .......... .......... .......... .......... .......... 59% 195M 7s 156600K .......... .......... .......... .......... .......... 59% 185M 7s 156650K .......... .......... .......... .......... .......... 59% 219M 7s 156700K .......... .......... .......... .......... .......... 59% 183M 7s 156750K .......... .......... .......... .......... .......... 59% 214M 7s 156800K .......... .......... .......... .......... .......... 59% 178M 7s 156850K .......... .......... .......... .......... .......... 59% 108M 7s 156900K .......... .......... .......... .......... .......... 59% 144M 7s 156950K .......... .......... .......... .......... .......... 59% 185M 7s 157000K .......... .......... .......... .......... .......... 59% 231M 7s 157050K .......... .......... .......... .......... .......... 59% 2.37M 7s 157100K .......... .......... .......... .......... .......... 59% 68.3M 7s 157150K .......... .......... .......... .......... .......... 59% 147M 7s 157200K .......... .......... .......... .......... .......... 59% 140M 7s 157250K .......... .......... .......... .......... .......... 59% 144M 6s 157300K .......... .......... .......... .......... .......... 60% 140M 6s 157350K .......... .......... .......... .......... .......... 60% 127M 6s 157400K .......... .......... .......... .......... .......... 60% 157M 6s 157450K .......... .......... .......... .......... .......... 60% 127M 6s 157500K .......... .......... .......... .......... .......... 60% 163M 6s 157550K .......... .......... .......... .......... .......... 60% 145M 6s 157600K .......... .......... .......... .......... .......... 60% 164M 6s 157650K .......... .......... .......... .......... .......... 60% 178M 6s 157700K .......... .......... .......... .......... .......... 60% 120M 6s 157750K .......... .......... .......... .......... .......... 60% 115M 6s 157800K .......... .......... .......... .......... .......... 60% 160M 6s 157850K .......... .......... .......... .......... .......... 60% 151M 6s 157900K .......... .......... .......... .......... .......... 60% 149M 6s 157950K .......... .......... .......... .......... .......... 60% 144M 6s 158000K .......... .......... .......... .......... .......... 60% 133M 6s 158050K .......... .......... .......... .......... .......... 60% 184M 6s 158100K .......... .......... .......... .......... .......... 60% 128M 6s 158150K .......... .......... .......... .......... .......... 60% 166M 6s 158200K .......... .......... .......... .......... .......... 60% 172M 6s 158250K .......... .......... .......... .......... .......... 60% 164M 6s 158300K .......... .......... .......... .......... .......... 60% 245M 6s 158350K .......... .......... .......... .......... .......... 60% 169M 6s 158400K .......... .......... .......... .......... .......... 60% 144M 6s 158450K .......... .......... .......... .......... .......... 60% 166M 6s 158500K .......... .......... .......... .......... .......... 60% 186M 6s 158550K .......... .......... .......... .......... .......... 60% 127M 6s 158600K .......... .......... .......... .......... .......... 60% 110M 6s 158650K .......... .......... .......... .......... .......... 60% 185M 6s 158700K .......... .......... .......... .......... .......... 60% 158M 6s 158750K .......... .......... .......... .......... .......... 60% 31.1M 6s 158800K .......... .......... .......... .......... .......... 60% 95.7M 6s 158850K .......... .......... .......... .......... .......... 60% 117M 6s 158900K .......... .......... .......... .......... .......... 60% 110M 6s 158950K .......... .......... .......... .......... .......... 60% 116M 6s 159000K .......... .......... .......... .......... .......... 60% 66.4M 6s 159050K .......... .......... .......... .......... .......... 60% 142M 6s 159100K .......... .......... .......... .......... .......... 60% 154M 6s 159150K .......... .......... .......... .......... .......... 60% 183M 6s 159200K .......... .......... .......... .......... .......... 60% 153M 6s 159250K .......... .......... .......... .......... .......... 60% 161M 6s 159300K .......... .......... .......... .......... .......... 60% 170M 6s 159350K .......... .......... .......... .......... .......... 60% 139M 6s 159400K .......... .......... .......... .......... .......... 60% 178M 6s 159450K .......... .......... .......... .......... .......... 60% 111M 6s 159500K .......... .......... .......... .......... .......... 60% 216M 6s 159550K .......... .......... .......... .......... .......... 60% 239M 6s 159600K .......... .......... .......... .......... .......... 60% 194M 6s 159650K .......... .......... .......... .......... .......... 60% 199M 6s 159700K .......... .......... .......... .......... .......... 60% 126M 6s 159750K .......... .......... .......... .......... .......... 60% 93.0M 6s 159800K .......... .......... .......... .......... .......... 60% 105M 6s 159850K .......... .......... .......... .......... .......... 60% 96.1M 6s 159900K .......... .......... .......... .......... .......... 61% 153M 6s 159950K .......... .......... .......... .......... .......... 61% 203M 6s 160000K .......... .......... .......... .......... .......... 61% 205M 6s 160050K .......... .......... .......... .......... .......... 61% 79.4M 6s 160100K .......... .......... .......... .......... .......... 61% 7.29M 6s 160150K .......... .......... .......... .......... .......... 61% 213M 6s 160200K .......... .......... .......... .......... .......... 61% 202M 6s 160250K .......... .......... .......... .......... .......... 61% 192M 6s 160300K .......... .......... .......... .......... .......... 61% 134M 6s 160350K .......... .......... .......... .......... .......... 61% 128M 6s 160400K .......... .......... .......... .......... .......... 61% 186M 6s 160450K .......... .......... .......... .......... .......... 61% 172M 6s 160500K .......... .......... .......... .......... .......... 61% 164M 6s 160550K .......... .......... .......... .......... .......... 61% 195M 6s 160600K .......... .......... .......... .......... .......... 61% 176M 6s 160650K .......... .......... .......... .......... .......... 61% 158M 6s 160700K .......... .......... .......... .......... .......... 61% 193M 6s 160750K .......... .......... .......... .......... .......... 61% 16.9M 6s 160800K .......... .......... .......... .......... .......... 61% 182M 6s 160850K .......... .......... .......... .......... .......... 61% 150M 6s 160900K .......... .......... .......... .......... .......... 61% 176M 6s 160950K .......... .......... .......... .......... .......... 61% 160M 6s 161000K .......... .......... .......... .......... .......... 61% 6.21M 6s 161050K .......... .......... .......... .......... .......... 61% 222M 6s 161100K .......... .......... .......... .......... .......... 61% 185M 6s 161150K .......... .......... .......... .......... .......... 61% 206M 6s 161200K .......... .......... .......... .......... .......... 61% 191M 6s 161250K .......... .......... .......... .......... .......... 61% 157M 6s 161300K .......... .......... .......... .......... .......... 61% 6.46M 6s 161350K .......... .......... .......... .......... .......... 61% 241M 6s 161400K .......... .......... .......... .......... .......... 61% 319M 6s 161450K .......... .......... .......... .......... .......... 61% 291M 6s 161500K .......... .......... .......... .......... .......... 61% 34.9M 6s 161550K .......... .......... .......... .......... .......... 61% 56.9M 6s 161600K .......... .......... .......... .......... .......... 61% 12.7M 6s 161650K .......... .......... .......... .......... .......... 61% 167M 6s 161700K .......... .......... .......... .......... .......... 61% 162M 6s 161750K .......... .......... .......... .......... .......... 61% 289M 6s 161800K .......... .......... .......... .......... .......... 61% 22.6M 6s 161850K .......... .......... .......... .......... .......... 61% 111M 6s 161900K .......... .......... .......... .......... .......... 61% 9.05M 6s 161950K .......... .......... .......... .......... .......... 61% 81.0M 6s 162000K .......... .......... .......... .......... .......... 61% 163M 6s 162050K .......... .......... .......... .......... .......... 61% 161M 6s 162100K .......... .......... .......... .......... .......... 61% 268M 6s 162150K .......... .......... .......... .......... .......... 61% 23.4M 6s 162200K .......... .......... .......... .......... .......... 61% 6.78M 6s 162250K .......... .......... .......... .......... .......... 61% 131M 6s 162300K .......... .......... .......... .......... .......... 61% 200M 6s 162350K .......... .......... .......... .......... .......... 61% 195M 6s 162400K .......... .......... .......... .......... .......... 61% 212M 6s 162450K .......... .......... .......... .......... .......... 61% 46.8M 6s 162500K .......... .......... .......... .......... .......... 61% 7.28M 6s 162550K .......... .......... .......... .......... .......... 62% 112M 6s 162600K .......... .......... .......... .......... .......... 62% 50.3M 6s 162650K .......... .......... .......... .......... .......... 62% 56.4M 6s 162700K .......... .......... .......... .......... .......... 62% 103M 6s 162750K .......... .......... .......... .......... .......... 62% 294M 6s 162800K .......... .......... .......... .......... .......... 62% 5.51M 6s 162850K .......... .......... .......... .......... .......... 62% 189M 6s 162900K .......... .......... .......... .......... .......... 62% 221M 6s 162950K .......... .......... .......... .......... .......... 62% 187M 6s 163000K .......... .......... .......... .......... .......... 62% 144M 6s 163050K .......... .......... .......... .......... .......... 62% 180M 6s 163100K .......... .......... .......... .......... .......... 62% 5.13M 6s 163150K .......... .......... .......... .......... .......... 62% 71.9M 6s 163200K .......... .......... .......... .......... .......... 62% 257M 6s 163250K .......... .......... .......... .......... .......... 62% 72.8M 6s 163300K .......... .......... .......... .......... .......... 62% 34.9M 6s 163350K .......... .......... .......... .......... .......... 62% 179M 6s 163400K .......... .......... .......... .......... .......... 62% 5.70M 6s 163450K .......... .......... .......... .......... .......... 62% 185M 6s 163500K .......... .......... .......... .......... .......... 62% 330M 6s 163550K .......... .......... .......... .......... .......... 62% 3.54M 6s 163600K .......... .......... .......... .......... .......... 62% 178M 6s 163650K .......... .......... .......... .......... .......... 62% 225M 6s 163700K .......... .......... .......... .......... .......... 62% 4.96M 6s 163750K .......... .......... .......... .......... .......... 62% 102M 6s 163800K .......... .......... .......... .......... .......... 62% 230M 6s 163850K .......... .......... .......... .......... .......... 62% 212M 6s 163900K .......... .......... .......... .......... .......... 62% 200M 6s 163950K .......... .......... .......... .......... .......... 62% 198M 6s 164000K .......... .......... .......... .......... .......... 62% 203M 6s 164050K .......... .......... .......... .......... .......... 62% 3.04M 6s 164100K .......... .......... .......... .......... .......... 62% 30.7M 6s 164150K .......... .......... .......... .......... .......... 62% 87.7M 6s 164200K .......... .......... .......... .......... .......... 62% 36.7M 6s 164250K .......... .......... .......... .......... .......... 62% 162M 6s 164300K .......... .......... .......... .......... .......... 62% 22.0M 6s 164350K .......... .......... .......... .......... .......... 62% 2.26M 6s 164400K .......... .......... .......... .......... .......... 62% 138M 6s 164450K .......... .......... .......... .......... .......... 62% 149M 6s 164500K .......... .......... .......... .......... .......... 62% 186M 6s 164550K .......... .......... .......... .......... .......... 62% 136M 6s 164600K .......... .......... .......... .......... .......... 62% 186M 6s 164650K .......... .......... .......... .......... .......... 62% 217M 6s 164700K .......... .......... .......... .......... .......... 62% 4.52M 6s 164750K .......... .......... .......... .......... .......... 62% 92.7M 6s 164800K .......... .......... .......... .......... .......... 62% 209M 6s 164850K .......... .......... .......... .......... .......... 62% 90.6M 6s 164900K .......... .......... .......... .......... .......... 62% 103M 6s 164950K .......... .......... .......... .......... .......... 62% 157M 6s 165000K .......... .......... .......... .......... .......... 62% 5.79M 6s 165050K .......... .......... .......... .......... .......... 62% 203M 6s 165100K .......... .......... .......... .......... .......... 62% 162M 6s 165150K .......... .......... .......... .......... .......... 63% 115M 6s 165200K .......... .......... .......... .......... .......... 63% 141M 6s 165250K .......... .......... .......... .......... .......... 63% 99.9M 6s 165300K .......... .......... .......... .......... .......... 63% 6.25M 6s 165350K .......... .......... .......... .......... .......... 63% 120M 6s 165400K .......... .......... .......... .......... .......... 63% 153M 6s 165450K .......... .......... .......... .......... .......... 63% 129M 6s 165500K .......... .......... .......... .......... .......... 63% 74.1M 6s 165550K .......... .......... .......... .......... .......... 63% 109M 6s 165600K .......... .......... .......... .......... .......... 63% 436K 6s 165650K .......... .......... .......... .......... .......... 63% 98.2M 6s 165700K .......... .......... .......... .......... .......... 63% 182M 6s 165750K .......... .......... .......... .......... .......... 63% 195M 6s 165800K .......... .......... .......... .......... .......... 63% 128M 6s 165850K .......... .......... .......... .......... .......... 63% 48.2M 6s 165900K .......... .......... .......... .......... .......... 63% 99.2M 6s 165950K .......... .......... .......... .......... .......... 63% 50.7M 6s 166000K .......... .......... .......... .......... .......... 63% 100M 6s 166050K .......... .......... .......... .......... .......... 63% 139M 6s 166100K .......... .......... .......... .......... .......... 63% 135M 6s 166150K .......... .......... .......... .......... .......... 63% 68.8M 6s 166200K .......... .......... .......... .......... .......... 63% 4.66M 6s 166250K .......... .......... .......... .......... .......... 63% 184M 6s 166300K .......... .......... .......... .......... .......... 63% 181M 6s 166350K .......... .......... .......... .......... .......... 63% 127M 6s 166400K .......... .......... .......... .......... .......... 63% 142M 6s 166450K .......... .......... .......... .......... .......... 63% 91.4M 6s 166500K .......... .......... .......... .......... .......... 63% 3.75M 6s 166550K .......... .......... .......... .......... .......... 63% 48.1M 6s 166600K .......... .......... .......... .......... .......... 63% 967K 6s 166650K .......... .......... .......... .......... .......... 63% 223M 6s 166700K .......... .......... .......... .......... .......... 63% 148M 6s 166750K .......... .......... .......... .......... .......... 63% 174M 6s 166800K .......... .......... .......... .......... .......... 63% 114M 6s 166850K .......... .......... .......... .......... .......... 63% 5.05M 6s 166900K .......... .......... .......... .......... .......... 63% 144M 6s 166950K .......... .......... .......... .......... .......... 63% 158M 6s 167000K .......... .......... .......... .......... .......... 63% 120M 6s 167050K .......... .......... .......... .......... .......... 63% 174M 6s 167100K .......... .......... .......... .......... .......... 63% 71.8M 6s 167150K .......... .......... .......... .......... .......... 63% 4.71M 6s 167200K .......... .......... .......... .......... .......... 63% 157M 6s 167250K .......... .......... .......... .......... .......... 63% 159M 6s 167300K .......... .......... .......... .......... .......... 63% 235M 6s 167350K .......... .......... .......... .......... .......... 63% 162M 6s 167400K .......... .......... .......... .......... .......... 63% 82.8M 6s 167450K .......... .......... .......... .......... .......... 63% 114M 6s 167500K .......... .......... .......... .......... .......... 63% 4.39M 6s 167550K .......... .......... .......... .......... .......... 63% 140M 6s 167600K .......... .......... .......... .......... .......... 63% 86.4M 6s 167650K .......... .......... .......... .......... .......... 63% 108M 6s 167700K .......... .......... .......... .......... .......... 63% 77.9M 6s 167750K .......... .......... .......... .......... .......... 63% 93.9M 6s 167800K .......... .......... .......... .......... .......... 64% 6.26M 6s 167850K .......... .......... .......... .......... .......... 64% 125M 6s 167900K .......... .......... .......... .......... .......... 64% 132M 6s 167950K .......... .......... .......... .......... .......... 64% 126M 6s 168000K .......... .......... .......... .......... .......... 64% 98.2M 6s 168050K .......... .......... .......... .......... .......... 64% 74.1M 6s 168100K .......... .......... .......... .......... .......... 64% 96.3M 6s 168150K .......... .......... .......... .......... .......... 64% 5.13M 6s 168200K .......... .......... .......... .......... .......... 64% 121M 6s 168250K .......... .......... .......... .......... .......... 64% 141M 6s 168300K .......... .......... .......... .......... .......... 64% 141M 6s 168350K .......... .......... .......... .......... .......... 64% 96.3M 6s 168400K .......... .......... .......... .......... .......... 64% 76.9M 6s 168450K .......... .......... .......... .......... .......... 64% 4.69M 6s 168500K .......... .......... .......... .......... .......... 64% 199M 6s 168550K .......... .......... .......... .......... .......... 64% 157M 6s 168600K .......... .......... .......... .......... .......... 64% 173M 6s 168650K .......... .......... .......... .......... .......... 64% 394K 6s 168700K .......... .......... .......... .......... .......... 64% 179M 6s 168750K .......... .......... .......... .......... .......... 64% 66.3M 6s 168800K .......... .......... .......... .......... .......... 64% 57.0M 6s 168850K .......... .......... .......... .......... .......... 64% 62.5M 6s 168900K .......... .......... .......... .......... .......... 64% 75.6M 6s 168950K .......... .......... .......... .......... .......... 64% 83.6M 6s 169000K .......... .......... .......... .......... .......... 64% 84.9M 6s 169050K .......... .......... .......... .......... .......... 64% 81.9M 6s 169100K .......... .......... .......... .......... .......... 64% 53.4M 6s 169150K .......... .......... .......... .......... .......... 64% 130M 6s 169200K .......... .......... .......... .......... .......... 64% 124M 6s 169250K .......... .......... .......... .......... .......... 64% 134M 6s 169300K .......... .......... .......... .......... .......... 64% 120M 6s 169350K .......... .......... .......... .......... .......... 64% 4.92M 6s 169400K .......... .......... .......... .......... .......... 64% 209M 6s 169450K .......... .......... .......... .......... .......... 64% 102M 6s 169500K .......... .......... .......... .......... .......... 64% 193M 6s 169550K .......... .......... .......... .......... .......... 64% 112M 6s 169600K .......... .......... .......... .......... .......... 64% 121M 6s 169650K .......... .......... .......... .......... .......... 64% 70.5M 6s 169700K .......... .......... .......... .......... .......... 64% 4.60M 6s 169750K .......... .......... .......... .......... .......... 64% 144M 6s 169800K .......... .......... .......... .......... .......... 64% 94.8M 6s 169850K .......... .......... .......... .......... .......... 64% 119M 6s 169900K .......... .......... .......... .......... .......... 64% 136M 6s 169950K .......... .......... .......... .......... .......... 64% 61.7M 6s 170000K .......... .......... .......... .......... .......... 64% 3.70M 6s 170050K .......... .......... .......... .......... .......... 64% 180M 6s 170100K .......... .......... .......... .......... .......... 64% 153M 6s 170150K .......... .......... .......... .......... .......... 64% 186M 6s 170200K .......... .......... .......... .......... .......... 64% 138M 6s 170250K .......... .......... .......... .......... .......... 64% 197M 6s 170300K .......... .......... .......... .......... .......... 64% 222M 6s 170350K .......... .......... .......... .......... .......... 64% 2.78M 6s 170400K .......... .......... .......... .......... .......... 65% 202M 6s 170450K .......... .......... .......... .......... .......... 65% 135M 6s 170500K .......... .......... .......... .......... .......... 65% 84.5M 6s 170550K .......... .......... .......... .......... .......... 65% 148M 6s 170600K .......... .......... .......... .......... .......... 65% 174M 6s 170650K .......... .......... .......... .......... .......... 65% 178M 6s 170700K .......... .......... .......... .......... .......... 65% 100K 6s 170750K .......... .......... .......... .......... .......... 65% 51.9M 6s 170800K .......... .......... .......... .......... .......... 65% 136M 6s 170850K .......... .......... .......... .......... .......... 65% 100M 6s 170900K .......... .......... .......... .......... .......... 65% 102M 6s 170950K .......... .......... .......... .......... .......... 65% 173M 6s 171000K .......... .......... .......... .......... .......... 65% 188M 6s 171050K .......... .......... .......... .......... .......... 65% 147M 6s 171100K .......... .......... .......... .......... .......... 65% 103M 6s 171150K .......... .......... .......... .......... .......... 65% 210M 6s 171200K .......... .......... .......... .......... .......... 65% 186M 6s 171250K .......... .......... .......... .......... .......... 65% 136M 6s 171300K .......... .......... .......... .......... .......... 65% 107M 6s 171350K .......... .......... .......... .......... .......... 65% 83.8M 6s 171400K .......... .......... .......... .......... .......... 65% 132M 6s 171450K .......... .......... .......... .......... .......... 65% 94.4M 6s 171500K .......... .......... .......... .......... .......... 65% 163M 6s 171550K .......... .......... .......... .......... .......... 65% 124M 6s 171600K .......... .......... .......... .......... .......... 65% 122M 6s 171650K .......... .......... .......... .......... .......... 65% 245M 6s 171700K .......... .......... .......... .......... .......... 65% 174M 6s 171750K .......... .......... .......... .......... .......... 65% 97.5M 6s 171800K .......... .......... .......... .......... .......... 65% 178M 6s 171850K .......... .......... .......... .......... .......... 65% 143M 6s 171900K .......... .......... .......... .......... .......... 65% 186M 6s 171950K .......... .......... .......... .......... .......... 65% 175M 6s 172000K .......... .......... .......... .......... .......... 65% 237M 6s 172050K .......... .......... .......... .......... .......... 65% 100M 6s 172100K .......... .......... .......... .......... .......... 65% 177M 6s 172150K .......... .......... .......... .......... .......... 65% 142M 6s 172200K .......... .......... .......... .......... .......... 65% 87.7M 6s 172250K .......... .......... .......... .......... .......... 65% 132M 6s 172300K .......... .......... .......... .......... .......... 65% 154M 6s 172350K .......... .......... .......... .......... .......... 65% 114M 6s 172400K .......... .......... .......... .......... .......... 65% 198M 6s 172450K .......... .......... .......... .......... .......... 65% 206M 6s 172500K .......... .......... .......... .......... .......... 65% 245M 6s 172550K .......... .......... .......... .......... .......... 65% 245M 6s 172600K .......... .......... .......... .......... .......... 65% 148M 6s 172650K .......... .......... .......... .......... .......... 65% 176M 6s 172700K .......... .......... .......... .......... .......... 65% 147M 6s 172750K .......... .......... .......... .......... .......... 65% 83.6K 6s 172800K .......... .......... .......... .......... .......... 65% 203M 6s 172850K .......... .......... .......... .......... .......... 65% 113M 6s 172900K .......... .......... .......... .......... .......... 65% 124M 6s 172950K .......... .......... .......... .......... .......... 65% 81.9M 6s 173000K .......... .......... .......... .......... .......... 65% 148M 6s 173050K .......... .......... .......... .......... .......... 66% 146M 6s 173100K .......... .......... .......... .......... .......... 66% 161M 6s 173150K .......... .......... .......... .......... .......... 66% 70.1M 6s 173200K .......... .......... .......... .......... .......... 66% 142M 6s 173250K .......... .......... .......... .......... .......... 66% 36.8M 6s 173300K .......... .......... .......... .......... .......... 66% 300M 6s 173350K .......... .......... .......... .......... .......... 66% 210M 6s 173400K .......... .......... .......... .......... .......... 66% 165M 6s 173450K .......... .......... .......... .......... .......... 66% 135M 6s 173500K .......... .......... .......... .......... .......... 66% 160M 6s 173550K .......... .......... .......... .......... .......... 66% 213M 6s 173600K .......... .......... .......... .......... .......... 66% 189M 6s 173650K .......... .......... .......... .......... .......... 66% 303M 6s 173700K .......... .......... .......... .......... .......... 66% 199M 6s 173750K .......... .......... .......... .......... .......... 66% 187M 6s 173800K .......... .......... .......... .......... .......... 66% 32.5M 6s 173850K .......... .......... .......... .......... .......... 66% 127M 6s 173900K .......... .......... .......... .......... .......... 66% 110M 6s 173950K .......... .......... .......... .......... .......... 66% 186M 6s 174000K .......... .......... .......... .......... .......... 66% 86.6M 6s 174050K .......... .......... .......... .......... .......... 66% 163M 6s 174100K .......... .......... .......... .......... .......... 66% 147M 6s 174150K .......... .......... .......... .......... .......... 66% 189M 6s 174200K .......... .......... .......... .......... .......... 66% 146M 6s 174250K .......... .......... .......... .......... .......... 66% 180M 6s 174300K .......... .......... .......... .......... .......... 66% 117M 6s 174350K .......... .......... .......... .......... .......... 66% 245M 6s 174400K .......... .......... .......... .......... .......... 66% 257M 6s 174450K .......... .......... .......... .......... .......... 66% 243M 6s 174500K .......... .......... .......... .......... .......... 66% 265M 6s 174550K .......... .......... .......... .......... .......... 66% 276M 6s 174600K .......... .......... .......... .......... .......... 66% 230M 6s 174650K .......... .......... .......... .......... .......... 66% 291M 6s 174700K .......... .......... .......... .......... .......... 66% 238M 6s 174750K .......... .......... .......... .......... .......... 66% 279M 6s 174800K .......... .......... .......... .......... .......... 66% 128K 6s 174850K .......... .......... .......... .......... .......... 66% 37.2M 6s 174900K .......... .......... .......... .......... .......... 66% 124M 6s 174950K .......... .......... .......... .......... .......... 66% 145M 6s 175000K .......... .......... .......... .......... .......... 66% 222M 6s 175050K .......... .......... .......... .......... .......... 66% 226M 6s 175100K .......... .......... .......... .......... .......... 66% 197M 6s 175150K .......... .......... .......... .......... .......... 66% 56.6M 6s 175200K .......... .......... .......... .......... .......... 66% 82.6M 6s 175250K .......... .......... .......... .......... .......... 66% 49.5M 6s 175300K .......... .......... .......... .......... .......... 66% 162M 6s 175350K .......... .......... .......... .......... .......... 66% 42.1M 6s 175400K .......... .......... .......... .......... .......... 66% 9.40M 6s 175450K .......... .......... .......... .......... .......... 66% 129M 6s 175500K .......... .......... .......... .......... .......... 66% 69.4M 6s 175550K .......... .......... .......... .......... .......... 66% 145M 6s 175600K .......... .......... .......... .......... .......... 66% 154M 6s 175650K .......... .......... .......... .......... .......... 67% 99.0M 6s 175700K .......... .......... .......... .......... .......... 67% 188M 6s 175750K .......... .......... .......... .......... .......... 67% 150M 6s 175800K .......... .......... .......... .......... .......... 67% 136M 6s 175850K .......... .......... .......... .......... .......... 67% 64.8M 6s 175900K .......... .......... .......... .......... .......... 67% 28.4M 6s 175950K .......... .......... .......... .......... .......... 67% 100M 6s 176000K .......... .......... .......... .......... .......... 67% 117M 6s 176050K .......... .......... .......... .......... .......... 67% 171M 6s 176100K .......... .......... .......... .......... .......... 67% 67.1M 6s 176150K .......... .......... .......... .......... .......... 67% 96.7M 6s 176200K .......... .......... .......... .......... .......... 67% 189M 6s 176250K .......... .......... .......... .......... .......... 67% 182M 6s 176300K .......... .......... .......... .......... .......... 67% 162M 6s 176350K .......... .......... .......... .......... .......... 67% 153M 6s 176400K .......... .......... .......... .......... .......... 67% 128M 6s 176450K .......... .......... .......... .......... .......... 67% 103M 6s 176500K .......... .......... .......... .......... .......... 67% 128M 6s 176550K .......... .......... .......... .......... .......... 67% 127M 6s 176600K .......... .......... .......... .......... .......... 67% 132M 6s 176650K .......... .......... .......... .......... .......... 67% 110M 6s 176700K .......... .......... .......... .......... .......... 67% 142M 6s 176750K .......... .......... .......... .......... .......... 67% 200M 6s 176800K .......... .......... .......... .......... .......... 67% 180M 6s 176850K .......... .......... .......... .......... .......... 67% 6.32M 6s 176900K .......... .......... .......... .......... .......... 67% 149M 6s 176950K .......... .......... .......... .......... .......... 67% 173M 6s 177000K .......... .......... .......... .......... .......... 67% 133M 6s 177050K .......... .......... .......... .......... .......... 67% 216M 6s 177100K .......... .......... .......... .......... .......... 67% 188M 6s 177150K .......... .......... .......... .......... .......... 67% 118M 6s 177200K .......... .......... .......... .......... .......... 67% 184M 6s 177250K .......... .......... .......... .......... .......... 67% 132M 6s 177300K .......... .......... .......... .......... .......... 67% 24.2M 6s 177350K .......... .......... .......... .......... .......... 67% 117M 6s 177400K .......... .......... .......... .......... .......... 67% 115M 6s 177450K .......... .......... .......... .......... .......... 67% 104M 6s 177500K .......... .......... .......... .......... .......... 67% 136M 6s 177550K .......... .......... .......... .......... .......... 67% 103M 6s 177600K .......... .......... .......... .......... .......... 67% 109M 6s 177650K .......... .......... .......... .......... .......... 67% 68.5M 6s 177700K .......... .......... .......... .......... .......... 67% 4.07M 6s 177750K .......... .......... .......... .......... .......... 67% 141M 6s 177800K .......... .......... .......... .......... .......... 67% 234M 6s 177850K .......... .......... .......... .......... .......... 67% 155M 6s 177900K .......... .......... .......... .......... .......... 67% 68.9M 6s 177950K .......... .......... .......... .......... .......... 67% 85.7M 6s 178000K .......... .......... .......... .......... .......... 67% 84.8M 6s 178050K .......... .......... .......... .......... .......... 67% 59.7M 6s 178100K .......... .......... .......... .......... .......... 67% 120M 6s 178150K .......... .......... .......... .......... .......... 67% 102M 6s 178200K .......... .......... .......... .......... .......... 67% 44.3M 6s 178250K .......... .......... .......... .......... .......... 67% 63.9M 6s 178300K .......... .......... .......... .......... .......... 68% 77.1M 6s 178350K .......... .......... .......... .......... .......... 68% 85.4M 6s 178400K .......... .......... .......... .......... .......... 68% 119M 6s 178450K .......... .......... .......... .......... .......... 68% 203M 6s 178500K .......... .......... .......... .......... .......... 68% 247M 6s 178550K .......... .......... .......... .......... .......... 68% 244M 6s 178600K .......... .......... .......... .......... .......... 68% 164M 6s 178650K .......... .......... .......... .......... .......... 68% 243M 6s 178700K .......... .......... .......... .......... .......... 68% 180M 6s 178750K .......... .......... .......... .......... .......... 68% 244M 6s 178800K .......... .......... .......... .......... .......... 68% 247M 6s 178850K .......... .......... .......... .......... .......... 68% 155M 6s 178900K .......... .......... .......... .......... .......... 68% 2.17M 6s 178950K .......... .......... .......... .......... .......... 68% 17.5M 6s 179000K .......... .......... .......... .......... .......... 68% 29.4M 6s 179050K .......... .......... .......... .......... .......... 68% 40.6M 6s 179100K .......... .......... .......... .......... .......... 68% 18.7M 6s 179150K .......... .......... .......... .......... .......... 68% 33.4M 6s 179200K .......... .......... .......... .......... .......... 68% 14.3M 6s 179250K .......... .......... .......... .......... .......... 68% 21.3M 6s 179300K .......... .......... .......... .......... .......... 68% 129M 6s 179350K .......... .......... .......... .......... .......... 68% 138M 6s 179400K .......... .......... .......... .......... .......... 68% 161M 6s 179450K .......... .......... .......... .......... .......... 68% 153M 6s 179500K .......... .......... .......... .......... .......... 68% 226M 6s 179550K .......... .......... .......... .......... .......... 68% 224M 6s 179600K .......... .......... .......... .......... .......... 68% 8.59M 6s 179650K .......... .......... .......... .......... .......... 68% 13.7M 6s 179700K .......... .......... .......... .......... .......... 68% 8.10M 6s 179750K .......... .......... .......... .......... .......... 68% 14.7M 6s 179800K .......... .......... .......... .......... .......... 68% 14.9M 6s 179850K .......... .......... .......... .......... .......... 68% 14.0M 6s 179900K .......... .......... .......... .......... .......... 68% 13.0M 6s 179950K .......... .......... .......... .......... .......... 68% 14.1M 6s 180000K .......... .......... .......... .......... .......... 68% 16.7M 6s 180050K .......... .......... .......... .......... .......... 68% 31.1M 6s 180100K .......... .......... .......... .......... .......... 68% 39.6M 6s 180150K .......... .......... .......... .......... .......... 68% 36.8M 6s 180200K .......... .......... .......... .......... .......... 68% 54.6M 5s 180250K .......... .......... .......... .......... .......... 68% 112M 5s 180300K .......... .......... .......... .......... .......... 68% 61.0M 5s 180350K .......... .......... .......... .......... .......... 68% 4.35M 5s 180400K .......... .......... .......... .......... .......... 68% 231M 5s 180450K .......... .......... .......... .......... .......... 68% 191M 5s 180500K .......... .......... .......... .......... .......... 68% 151M 5s 180550K .......... .......... .......... .......... .......... 68% 217M 5s 180600K .......... .......... .......... .......... .......... 68% 140M 5s 180650K .......... .......... .......... .......... .......... 68% 198M 5s 180700K .......... .......... .......... .......... .......... 68% 4.08M 5s 180750K .......... .......... .......... .......... .......... 68% 52.4M 5s 180800K .......... .......... .......... .......... .......... 68% 81.7M 5s 180850K .......... .......... .......... .......... .......... 68% 84.8M 5s 180900K .......... .......... .......... .......... .......... 69% 123M 5s 180950K .......... .......... .......... .......... .......... 69% 80.0M 5s 181000K .......... .......... .......... .......... .......... 69% 203M 5s 181050K .......... .......... .......... .......... .......... 69% 4.71M 5s 181100K .......... .......... .......... .......... .......... 69% 270M 5s 181150K .......... .......... .......... .......... .......... 69% 346M 5s 181200K .......... .......... .......... .......... .......... 69% 238M 5s 181250K .......... .......... .......... .......... .......... 69% 337M 5s 181300K .......... .......... .......... .......... .......... 69% 337M 5s 181350K .......... .......... .......... .......... .......... 69% 300M 5s 181400K .......... .......... .......... .......... .......... 69% 4.19M 5s 181450K .......... .......... .......... .......... .......... 69% 93.4M 5s 181500K .......... .......... .......... .......... .......... 69% 301M 5s 181550K .......... .......... .......... .......... .......... 69% 328M 5s 181600K .......... .......... .......... .......... .......... 69% 298M 5s 181650K .......... .......... .......... .......... .......... 69% 337M 5s 181700K .......... .......... .......... .......... .......... 69% 303M 5s 181750K .......... .......... .......... .......... .......... 69% 349M 5s 181800K .......... .......... .......... .......... .......... 69% 3.77M 5s 181850K .......... .......... .......... .......... .......... 69% 181M 5s 181900K .......... .......... .......... .......... .......... 69% 214M 5s 181950K .......... .......... .......... .......... .......... 69% 296K 5s 182000K .......... .......... .......... .......... .......... 69% 114M 5s 182050K .......... .......... .......... .......... .......... 69% 77.6M 5s 182100K .......... .......... .......... .......... .......... 69% 48.6M 5s 182150K .......... .......... .......... .......... .......... 69% 173M 5s 182200K .......... .......... .......... .......... .......... 69% 182M 5s 182250K .......... .......... .......... .......... .......... 69% 222M 5s 182300K .......... .......... .......... .......... .......... 69% 206M 5s 182350K .......... .......... .......... .......... .......... 69% 148M 5s 182400K .......... .......... .......... .......... .......... 69% 78.9M 5s 182450K .......... .......... .......... .......... .......... 69% 175M 5s 182500K .......... .......... .......... .......... .......... 69% 253M 5s 182550K .......... .......... .......... .......... .......... 69% 253M 5s 182600K .......... .......... .......... .......... .......... 69% 220M 5s 182650K .......... .......... .......... .......... .......... 69% 78.9M 5s 182700K .......... .......... .......... .......... .......... 69% 3.80M 5s 182750K .......... .......... .......... .......... .......... 69% 176M 5s 182800K .......... .......... .......... .......... .......... 69% 208M 5s 182850K .......... .......... .......... .......... .......... 69% 182M 5s 182900K .......... .......... .......... .......... .......... 69% 128M 5s 182950K .......... .......... .......... .......... .......... 69% 178M 5s 183000K .......... .......... .......... .......... .......... 69% 142M 5s 183050K .......... .......... .......... .......... .......... 69% 202M 5s 183100K .......... .......... .......... .......... .......... 69% 4.03M 5s 183150K .......... .......... .......... .......... .......... 69% 176M 5s 183200K .......... .......... .......... .......... .......... 69% 201M 5s 183250K .......... .......... .......... .......... .......... 69% 181M 5s 183300K .......... .......... .......... .......... .......... 69% 160M 5s 183350K .......... .......... .......... .......... .......... 69% 166M 5s 183400K .......... .......... .......... .......... .......... 69% 55.9M 5s 183450K .......... .......... .......... .......... .......... 69% 3.57M 5s 183500K .......... .......... .......... .......... .......... 70% 231M 5s 183550K .......... .......... .......... .......... .......... 70% 93.4M 5s 183600K .......... .......... .......... .......... .......... 70% 103M 5s 183650K .......... .......... .......... .......... .......... 70% 174M 5s 183700K .......... .......... .......... .......... .......... 70% 171M 5s 183750K .......... .......... .......... .......... .......... 70% 202M 5s 183800K .......... .......... .......... .......... .......... 70% 4.27M 5s 183850K .......... .......... .......... .......... .......... 70% 119M 5s 183900K .......... .......... .......... .......... .......... 70% 188M 5s 183950K .......... .......... .......... .......... .......... 70% 141M 5s 184000K .......... .......... .......... .......... .......... 70% 49.3M 5s 184050K .......... .......... .......... .......... .......... 70% 193M 5s 184100K .......... .......... .......... .......... .......... 70% 151M 5s 184150K .......... .......... .......... .......... .......... 70% 4.06M 5s 184200K .......... .......... .......... .......... .......... 70% 170M 5s 184250K .......... .......... .......... .......... .......... 70% 117M 5s 184300K .......... .......... .......... .......... .......... 70% 102M 5s 184350K .......... .......... .......... .......... .......... 70% 67.1M 5s 184400K .......... .......... .......... .......... .......... 70% 82.3M 5s 184450K .......... .......... .......... .......... .......... 70% 168M 5s 184500K .......... .......... .......... .......... .......... 70% 218M 5s 184550K .......... .......... .......... .......... .......... 70% 3.99M 5s 184600K .......... .......... .......... .......... .......... 70% 103M 5s 184650K .......... .......... .......... .......... .......... 70% 100M 5s 184700K .......... .......... .......... .......... .......... 70% 81.7M 5s 184750K .......... .......... .......... .......... .......... 70% 92.8M 5s 184800K .......... .......... .......... .......... .......... 70% 202M 5s 184850K .......... .......... .......... .......... .......... 70% 130M 5s 184900K .......... .......... .......... .......... .......... 70% 3.44M 5s 184950K .......... .......... .......... .......... .......... 70% 154M 5s 185000K .......... .......... .......... .......... .......... 70% 194M 5s 185050K .......... .......... .......... .......... .......... 70% 85.5M 5s 185100K .......... .......... .......... .......... .......... 70% 147M 5s 185150K .......... .......... .......... .......... .......... 70% 225M 5s 185200K .......... .......... .......... .......... .......... 70% 233M 5s 185250K .......... .......... .......... .......... .......... 70% 1.91M 5s 185300K .......... .......... .......... .......... .......... 70% 279M 5s 185350K .......... .......... .......... .......... .......... 70% 190M 5s 185400K .......... .......... .......... .......... .......... 70% 311M 5s 185450K .......... .......... .......... .......... .......... 70% 298M 5s 185500K .......... .......... .......... .......... .......... 70% 349M 5s 185550K .......... .......... .......... .......... .......... 70% 341M 5s 185600K .......... .......... .......... .......... .......... 70% 3.25M 5s 185650K .......... .......... .......... .......... .......... 70% 168M 5s 185700K .......... .......... .......... .......... .......... 70% 51.0M 5s 185750K .......... .......... .......... .......... .......... 70% 152M 5s 185800K .......... .......... .......... .......... .......... 70% 191M 5s 185850K .......... .......... .......... .......... .......... 70% 185M 5s 185900K .......... .......... .......... .......... .......... 70% 253M 5s 185950K .......... .......... .......... .......... .......... 70% 172M 5s 186000K .......... .......... .......... .......... .......... 70% 2.69M 5s 186050K .......... .......... .......... .......... .......... 70% 121M 5s 186100K .......... .......... .......... .......... .......... 70% 127M 5s 186150K .......... .......... .......... .......... .......... 71% 136M 5s 186200K .......... .......... .......... .......... .......... 71% 38.8M 5s 186250K .......... .......... .......... .......... .......... 71% 227M 5s 186300K .......... .......... .......... .......... .......... 71% 133M 5s 186350K .......... .......... .......... .......... .......... 71% 3.07M 5s 186400K .......... .......... .......... .......... .......... 71% 229M 5s 186450K .......... .......... .......... .......... .......... 71% 197M 5s 186500K .......... .......... .......... .......... .......... 71% 292M 5s 186550K .......... .......... .......... .......... .......... 71% 300M 5s 186600K .......... .......... .......... .......... .......... 71% 158M 5s 186650K .......... .......... .......... .......... .......... 71% 145M 5s 186700K .......... .......... .......... .......... .......... 71% 2.88M 5s 186750K .......... .......... .......... .......... .......... 71% 216M 5s 186800K .......... .......... .......... .......... .......... 71% 305M 5s 186850K .......... .......... .......... .......... .......... 71% 238M 5s 186900K .......... .......... .......... .......... .......... 71% 321M 5s 186950K .......... .......... .......... .......... .......... 71% 224M 5s 187000K .......... .......... .......... .......... .......... 71% 199M 5s 187050K .......... .......... .......... .......... .......... 71% 238M 5s 187100K .......... .......... .......... .......... .......... 71% 3.02M 5s 187150K .......... .......... .......... .......... .......... 71% 181M 5s 187200K .......... .......... .......... .......... .......... 71% 162M 5s 187250K .......... .......... .......... .......... .......... 71% 166M 5s 187300K .......... .......... .......... .......... .......... 71% 160M 5s 187350K .......... .......... .......... .......... .......... 71% 71.7M 5s 187400K .......... .......... .......... .......... .......... 71% 67.1M 5s 187450K .......... .......... .......... .......... .......... 71% 2.94M 5s 187500K .......... .......... .......... .......... .......... 71% 173M 5s 187550K .......... .......... .......... .......... .......... 71% 90.1M 5s 187600K .......... .......... .......... .......... .......... 71% 108M 5s 187650K .......... .......... .......... .......... .......... 71% 91.1M 5s 187700K .......... .......... .......... .......... .......... 71% 53.8M 5s 187750K .......... .......... .......... .......... .......... 71% 160M 5s 187800K .......... .......... .......... .......... .......... 71% 147M 5s 187850K .......... .......... .......... .......... .......... 71% 2.58M 5s 187900K .......... .......... .......... .......... .......... 71% 142M 5s 187950K .......... .......... .......... .......... .......... 71% 83.2M 5s 188000K .......... .......... .......... .......... .......... 71% 139M 5s 188050K .......... .......... .......... .......... .......... 71% 134M 5s 188100K .......... .......... .......... .......... .......... 71% 41.6M 5s 188150K .......... .......... .......... .......... .......... 71% 57.0M 5s 188200K .......... .......... .......... .......... .......... 71% 3.22M 5s 188250K .......... .......... .......... .......... .......... 71% 264M 5s 188300K .......... .......... .......... .......... .......... 71% 162M 5s 188350K .......... .......... .......... .......... .......... 71% 165M 5s 188400K .......... .......... .......... .......... .......... 71% 210M 5s 188450K .......... .......... .......... .......... .......... 71% 180M 5s 188500K .......... .......... .......... .......... .......... 71% 211M 5s 188550K .......... .......... .......... .......... .......... 71% 213M 5s 188600K .......... .......... .......... .......... .......... 71% 3.92M 5s 188650K .......... .......... .......... .......... .......... 71% 296M 5s 188700K .......... .......... .......... .......... .......... 71% 217M 5s 188750K .......... .......... .......... .......... .......... 72% 332M 5s 188800K .......... .......... .......... .......... .......... 72% 315M 5s 188850K .......... .......... .......... .......... .......... 72% 215M 5s 188900K .......... .......... .......... .......... .......... 72% 317M 5s 188950K .......... .......... .......... .......... .......... 72% 2.92M 5s 189000K .......... .......... .......... .......... .......... 72% 195M 5s 189050K .......... .......... .......... .......... .......... 72% 234M 5s 189100K .......... .......... .......... .......... .......... 72% 163M 5s 189150K .......... .......... .......... .......... .......... 72% 88.5M 5s 189200K .......... .......... .......... .......... .......... 72% 192M 5s 189250K .......... .......... .......... .......... .......... 72% 115M 5s 189300K .......... .......... .......... .......... .......... 72% 4.08M 5s 189350K .......... .......... .......... .......... .......... 72% 163M 5s 189400K .......... .......... .......... .......... .......... 72% 223M 5s 189450K .......... .......... .......... .......... .......... 72% 189M 5s 189500K .......... .......... .......... .......... .......... 72% 217M 5s 189550K .......... .......... .......... .......... .......... 72% 210M 5s 189600K .......... .......... .......... .......... .......... 72% 189M 5s 189650K .......... .......... .......... .......... .......... 72% 214M 5s 189700K .......... .......... .......... .......... .......... 72% 2.57M 5s 189750K .......... .......... .......... .......... .......... 72% 303M 5s 189800K .......... .......... .......... .......... .......... 72% 303M 5s 189850K .......... .......... .......... .......... .......... 72% 273M 5s 189900K .......... .......... .......... .......... .......... 72% 326M 5s 189950K .......... .......... .......... .......... .......... 72% 237M 5s 190000K .......... .......... .......... .......... .......... 72% 166M 5s 190050K .......... .......... .......... .......... .......... 72% 3.00M 5s 190100K .......... .......... .......... .......... .......... 72% 136M 5s 190150K .......... .......... .......... .......... .......... 72% 115M 5s 190200K .......... .......... .......... .......... .......... 72% 168M 5s 190250K .......... .......... .......... .......... .......... 72% 98.4M 5s 190300K .......... .......... .......... .......... .......... 72% 164M 5s 190350K .......... .......... .......... .......... .......... 72% 141M 5s 190400K .......... .......... .......... .......... .......... 72% 128M 5s 190450K .......... .......... .......... .......... .......... 72% 3.42M 5s 190500K .......... .......... .......... .......... .......... 72% 159M 5s 190550K .......... .......... .......... .......... .......... 72% 90.3M 5s 190600K .......... .......... .......... .......... .......... 72% 132M 5s 190650K .......... .......... .......... .......... .......... 72% 168M 5s 190700K .......... .......... .......... .......... .......... 72% 72.0M 5s 190750K .......... .......... .......... .......... .......... 72% 157M 5s 190800K .......... .......... .......... .......... .......... 72% 3.70M 5s 190850K .......... .......... .......... .......... .......... 72% 105M 5s 190900K .......... .......... .......... .......... .......... 72% 112M 5s 190950K .......... .......... .......... .......... .......... 72% 166M 5s 191000K .......... .......... .......... .......... .......... 72% 189M 5s 191050K .......... .......... .......... .......... .......... 72% 328M 5s 191100K .......... .......... .......... .......... .......... 72% 245M 5s 191150K .......... .......... .......... .......... .......... 72% 326M 5s 191200K .......... .......... .......... .......... .......... 72% 2.73M 5s 191250K .......... .......... .......... .......... .......... 72% 49.2M 5s 191300K .......... .......... .......... .......... .......... 72% 41.3M 5s 191350K .......... .......... .......... .......... .......... 72% 21.2M 5s 191400K .......... .......... .......... .......... .......... 73% 36.4M 5s 191450K .......... .......... .......... .......... .......... 73% 43.1M 5s 191500K .......... .......... .......... .......... .......... 73% 69.7M 5s 191550K .......... .......... .......... .......... .......... 73% 37.4M 5s 191600K .......... .......... .......... .......... .......... 73% 3.12M 5s 191650K .......... .......... .......... .......... .......... 73% 42.5M 5s 191700K .......... .......... .......... .......... .......... 73% 113M 5s 191750K .......... .......... .......... .......... .......... 73% 56.0M 5s 191800K .......... .......... .......... .......... .......... 73% 138M 5s 191850K .......... .......... .......... .......... .......... 73% 69.0M 5s 191900K .......... .......... .......... .......... .......... 73% 148M 5s 191950K .......... .......... .......... .......... .......... 73% 3.17M 5s 192000K .......... .......... .......... .......... .......... 73% 154M 5s 192050K .......... .......... .......... .......... .......... 73% 76.2M 5s 192100K .......... .......... .......... .......... .......... 73% 25.6M 5s 192150K .......... .......... .......... .......... .......... 73% 20.7M 5s 192200K .......... .......... .......... .......... .......... 73% 24.3M 5s 192250K .......... .......... .......... .......... .......... 73% 72.6M 5s 192300K .......... .......... .......... .......... .......... 73% 185M 5s 192350K .......... .......... .......... .......... .......... 73% 3.31M 5s 192400K .......... .......... .......... .......... .......... 73% 29.9M 5s 192450K .......... .......... .......... .......... .......... 73% 43.9M 5s 192500K .......... .......... .......... .......... .......... 73% 141M 5s 192550K .......... .......... .......... .......... .......... 73% 45.8M 5s 192600K .......... .......... .......... .......... .......... 73% 12.7M 5s 192650K .......... .......... .......... .......... .......... 73% 50.7M 5s 192700K .......... .......... .......... .......... .......... 73% 2.95M 5s 192750K .......... .......... .......... .......... .......... 73% 41.1M 5s 192800K .......... .......... .......... .......... .......... 73% 112M 5s 192850K .......... .......... .......... .......... .......... 73% 100M 5s 192900K .......... .......... .......... .......... .......... 73% 67.5M 5s 192950K .......... .......... .......... .......... .......... 73% 62.5M 5s 193000K .......... .......... .......... .......... .......... 73% 30.0M 5s 193050K .......... .......... .......... .......... .......... 73% 26.1M 5s 193100K .......... .......... .......... .......... .......... 73% 2.55M 5s 193150K .......... .......... .......... .......... .......... 73% 97.9M 5s 193200K .......... .......... .......... .......... .......... 73% 75.6M 5s 193250K .......... .......... .......... .......... .......... 73% 120M 5s 193300K .......... .......... .......... .......... .......... 73% 66.9M 5s 193350K .......... .......... .......... .......... .......... 73% 144M 5s 193400K .......... .......... .......... .......... .......... 73% 211M 5s 193450K .......... .......... .......... .......... .......... 73% 3.81M 5s 193500K .......... .......... .......... .......... .......... 73% 218M 5s 193550K .......... .......... .......... .......... .......... 73% 231M 5s 193600K .......... .......... .......... .......... .......... 73% 191M 5s 193650K .......... .......... .......... .......... .......... 73% 184M 5s 193700K .......... .......... .......... .......... .......... 73% 39.1M 5s 193750K .......... .......... .......... .......... .......... 73% 249M 5s 193800K .......... .......... .......... .......... .......... 73% 282M 5s 193850K .......... .......... .......... .......... .......... 73% 4.59M 5s 193900K .......... .......... .......... .......... .......... 73% 149M 5s 193950K .......... .......... .......... .......... .......... 73% 95.7M 5s 194000K .......... .......... .......... .......... .......... 74% 151M 5s 194050K .......... .......... .......... .......... .......... 74% 119M 5s 194100K .......... .......... .......... .......... .......... 74% 178M 5s 194150K .......... .......... .......... .......... .......... 74% 201M 5s 194200K .......... .......... .......... .......... .......... 74% 182M 5s 194250K .......... .......... .......... .......... .......... 74% 4.12M 5s 194300K .......... .......... .......... .......... .......... 74% 189M 5s 194350K .......... .......... .......... .......... .......... 74% 124M 5s 194400K .......... .......... .......... .......... .......... 74% 309M 4s 194450K .......... .......... .......... .......... .......... 74% 264M 4s 194500K .......... .......... .......... .......... .......... 74% 296M 4s 194550K .......... .......... .......... .......... .......... 74% 155M 4s 194600K .......... .......... .......... .......... .......... 74% 4.13M 4s 194650K .......... .......... .......... .......... .......... 74% 109M 4s 194700K .......... .......... .......... .......... .......... 74% 134M 4s 194750K .......... .......... .......... .......... .......... 74% 138M 4s 194800K .......... .......... .......... .......... .......... 74% 90.8M 4s 194850K .......... .......... .......... .......... .......... 74% 148M 4s 194900K .......... .......... .......... .......... .......... 74% 92.7M 4s 194950K .......... .......... .......... .......... .......... 74% 117M 4s 195000K .......... .......... .......... .......... .......... 74% 4.26M 4s 195050K .......... .......... .......... .......... .......... 74% 96.7M 4s 195100K .......... .......... .......... .......... .......... 74% 117M 4s 195150K .......... .......... .......... .......... .......... 74% 126M 4s 195200K .......... .......... .......... .......... .......... 74% 144M 4s 195250K .......... .......... .......... .......... .......... 74% 109M 4s 195300K .......... .......... .......... .......... .......... 74% 72.6M 4s 195350K .......... .......... .......... .......... .......... 74% 155M 4s 195400K .......... .......... .......... .......... .......... 74% 5.02M 4s 195450K .......... .......... .......... .......... .......... 74% 69.5M 4s 195500K .......... .......... .......... .......... .......... 74% 104M 4s 195550K .......... .......... .......... .......... .......... 74% 164M 4s 195600K .......... .......... .......... .......... .......... 74% 154M 4s 195650K .......... .......... .......... .......... .......... 74% 48.9M 4s 195700K .......... .......... .......... .......... .......... 74% 95.9M 4s 195750K .......... .......... .......... .......... .......... 74% 5.25M 4s 195800K .......... .......... .......... .......... .......... 74% 132M 4s 195850K .......... .......... .......... .......... .......... 74% 123M 4s 195900K .......... .......... .......... .......... .......... 74% 185M 4s 195950K .......... .......... .......... .......... .......... 74% 186M 4s 196000K .......... .......... .......... .......... .......... 74% 176M 4s 196050K .......... .......... .......... .......... .......... 74% 173M 4s 196100K .......... .......... .......... .......... .......... 74% 189M 4s 196150K .......... .......... .......... .......... .......... 74% 5.78M 4s 196200K .......... .......... .......... .......... .......... 74% 226M 4s 196250K .......... .......... .......... .......... .......... 74% 254M 4s 196300K .......... .......... .......... .......... .......... 74% 342K 4s 196350K .......... .......... .......... .......... .......... 74% 154M 4s 196400K .......... .......... .......... .......... .......... 74% 277M 4s 196450K .......... .......... .......... .......... .......... 74% 270M 4s 196500K .......... .......... .......... .......... .......... 74% 215M 4s 196550K .......... .......... .......... .......... .......... 74% 317M 4s 196600K .......... .......... .......... .......... .......... 74% 243M 4s 196650K .......... .......... .......... .......... .......... 75% 309M 4s 196700K .......... .......... .......... .......... .......... 75% 57.6M 4s 196750K .......... .......... .......... .......... .......... 75% 303M 4s 196800K .......... .......... .......... .......... .......... 75% 321M 4s 196850K .......... .......... .......... .......... .......... 75% 265M 4s 196900K .......... .......... .......... .......... .......... 75% 307M 4s 196950K .......... .......... .......... .......... .......... 75% 107M 4s 197000K .......... .......... .......... .......... .......... 75% 226M 4s 197050K .......... .......... .......... .......... .......... 75% 175M 4s 197100K .......... .......... .......... .......... .......... 75% 256M 4s 197150K .......... .......... .......... .......... .......... 75% 3.95M 4s 197200K .......... .......... .......... .......... .......... 75% 256M 4s 197250K .......... .......... .......... .......... .......... 75% 319M 4s 197300K .......... .......... .......... .......... .......... 75% 169M 4s 197350K .......... .......... .......... .......... .......... 75% 105M 4s 197400K .......... .......... .......... .......... .......... 75% 200M 4s 197450K .......... .......... .......... .......... .......... 75% 212M 4s 197500K .......... .......... .......... .......... .......... 75% 257M 4s 197550K .......... .......... .......... .......... .......... 75% 4.21M 4s 197600K .......... .......... .......... .......... .......... 75% 84.6M 4s 197650K .......... .......... .......... .......... .......... 75% 132M 4s 197700K .......... .......... .......... .......... .......... 75% 132M 4s 197750K .......... .......... .......... .......... .......... 75% 200M 4s 197800K .......... .......... .......... .......... .......... 75% 181M 4s 197850K .......... .......... .......... .......... .......... 75% 66.5M 4s 197900K .......... .......... .......... .......... .......... 75% 94.3M 4s 197950K .......... .......... .......... .......... .......... 75% 4.46M 4s 198000K .......... .......... .......... .......... .......... 75% 114M 4s 198050K .......... .......... .......... .......... .......... 75% 132M 4s 198100K .......... .......... .......... .......... .......... 75% 68.8M 4s 198150K .......... .......... .......... .......... .......... 75% 185M 4s 198200K .......... .......... .......... .......... .......... 75% 79.1M 4s 198250K .......... .......... .......... .......... .......... 75% 206M 4s 198300K .......... .......... .......... .......... .......... 75% 162M 4s 198350K .......... .......... .......... .......... .......... 75% 5.03M 4s 198400K .......... .......... .......... .......... .......... 75% 243M 4s 198450K .......... .......... .......... .......... .......... 75% 252M 4s 198500K .......... .......... .......... .......... .......... 75% 317M 4s 198550K .......... .......... .......... .......... .......... 75% 317M 4s 198600K .......... .......... .......... .......... .......... 75% 91.4M 4s 198650K .......... .......... .......... .......... .......... 75% 146M 4s 198700K .......... .......... .......... .......... .......... 75% 5.56M 4s 198750K .......... .......... .......... .......... .......... 75% 67.2M 4s 198800K .......... .......... .......... .......... .......... 75% 175M 4s 198850K .......... .......... .......... .......... .......... 75% 113M 4s 198900K .......... .......... .......... .......... .......... 75% 107M 4s 198950K .......... .......... .......... .......... .......... 75% 75.9M 4s 199000K .......... .......... .......... .......... .......... 75% 134M 4s 199050K .......... .......... .......... .......... .......... 75% 176M 4s 199100K .......... .......... .......... .......... .......... 75% 5.60M 4s 199150K .......... .......... .......... .......... .......... 75% 170M 4s 199200K .......... .......... .......... .......... .......... 75% 84.6M 4s 199250K .......... .......... .......... .......... .......... 76% 147M 4s 199300K .......... .......... .......... .......... .......... 76% 156M 4s 199350K .......... .......... .......... .......... .......... 76% 214M 4s 199400K .......... .......... .......... .......... .......... 76% 122M 4s 199450K .......... .......... .......... .......... .......... 76% 129M 4s 199500K .......... .......... .......... .......... .......... 76% 5.66M 4s 199550K .......... .......... .......... .......... .......... 76% 291M 4s 199600K .......... .......... .......... .......... .......... 76% 274M 4s 199650K .......... .......... .......... .......... .......... 76% 321M 4s 199700K .......... .......... .......... .......... .......... 76% 125M 4s 199750K .......... .......... .......... .......... .......... 76% 309M 4s 199800K .......... .......... .......... .......... .......... 76% 155M 4s 199850K .......... .......... .......... .......... .......... 76% 82.3M 4s 199900K .......... .......... .......... .......... .......... 76% 3.86M 4s 199950K .......... .......... .......... .......... .......... 76% 160M 4s 200000K .......... .......... .......... .......... .......... 76% 185M 4s 200050K .......... .......... .......... .......... .......... 76% 147M 4s 200100K .......... .......... .......... .......... .......... 76% 167M 4s 200150K .......... .......... .......... .......... .......... 76% 92.5M 4s 200200K .......... .......... .......... .......... .......... 76% 102M 4s 200250K .......... .......... .......... .......... .......... 76% 108M 4s 200300K .......... .......... .......... .......... .......... 76% 4.13M 4s 200350K .......... .......... .......... .......... .......... 76% 70.3M 4s 200400K .......... .......... .......... .......... .......... 76% 790K 4s 200450K .......... .......... .......... .......... .......... 76% 162M 4s 200500K .......... .......... .......... .......... .......... 76% 140M 4s 200550K .......... .......... .......... .......... .......... 76% 94.6M 4s 200600K .......... .......... .......... .......... .......... 76% 78.6M 4s 200650K .......... .......... .......... .......... .......... 76% 60.0M 4s 200700K .......... .......... .......... .......... .......... 76% 3.37M 4s 200750K .......... .......... .......... .......... .......... 76% 141M 4s 200800K .......... .......... .......... .......... .......... 76% 173M 4s 200850K .......... .......... .......... .......... .......... 76% 61.7M 4s 200900K .......... .......... .......... .......... .......... 76% 38.1M 4s 200950K .......... .......... .......... .......... .......... 76% 113M 4s 201000K .......... .......... .......... .......... .......... 76% 203M 4s 201050K .......... .......... .......... .......... .......... 76% 161M 4s 201100K .......... .......... .......... .......... .......... 76% 3.36M 4s 201150K .......... .......... .......... .......... .......... 76% 126M 4s 201200K .......... .......... .......... .......... .......... 76% 135M 4s 201250K .......... .......... .......... .......... .......... 76% 203M 4s 201300K .......... .......... .......... .......... .......... 76% 222M 4s 201350K .......... .......... .......... .......... .......... 76% 234M 4s 201400K .......... .......... .......... .......... .......... 76% 252M 4s 201450K .......... .......... .......... .......... .......... 76% 108M 4s 201500K .......... .......... .......... .......... .......... 76% 3.20M 4s 201550K .......... .......... .......... .......... .......... 76% 188M 4s 201600K .......... .......... .......... .......... .......... 76% 84.3M 4s 201650K .......... .......... .......... .......... .......... 76% 203M 4s 201700K .......... .......... .......... .......... .......... 76% 160M 4s 201750K .......... .......... .......... .......... .......... 76% 133M 4s 201800K .......... .......... .......... .......... .......... 76% 161M 4s 201850K .......... .......... .......... .......... .......... 76% 71.0M 4s 201900K .......... .......... .......... .......... .......... 77% 3.46M 4s 201950K .......... .......... .......... .......... .......... 77% 109M 4s 202000K .......... .......... .......... .......... .......... 77% 267M 4s 202050K .......... .......... .......... .......... .......... 77% 254M 4s 202100K .......... .......... .......... .......... .......... 77% 148M 4s 202150K .......... .......... .......... .......... .......... 77% 256M 4s 202200K .......... .......... .......... .......... .......... 77% 153M 4s 202250K .......... .......... .......... .......... .......... 77% 78.3M 4s 202300K .......... .......... .......... .......... .......... 77% 3.71M 4s 202350K .......... .......... .......... .......... .......... 77% 141M 4s 202400K .......... .......... .......... .......... .......... 77% 91.6M 4s 202450K .......... .......... .......... .......... .......... 77% 99.4M 4s 202500K .......... .......... .......... .......... .......... 77% 184M 4s 202550K .......... .......... .......... .......... .......... 77% 184M 4s 202600K .......... .......... .......... .......... .......... 77% 121M 4s 202650K .......... .......... .......... .......... .......... 77% 182M 4s 202700K .......... .......... .......... .......... .......... 77% 3.62M 4s 202750K .......... .......... .......... .......... .......... 77% 153M 4s 202800K .......... .......... .......... .......... .......... 77% 124M 4s 202850K .......... .......... .......... .......... .......... 77% 99.0M 4s 202900K .......... .......... .......... .......... .......... 77% 117M 4s 202950K .......... .......... .......... .......... .......... 77% 81.2M 4s 203000K .......... .......... .......... .......... .......... 77% 121M 4s 203050K .......... .......... .......... .......... .......... 77% 72.8M 4s 203100K .......... .......... .......... .......... .......... 77% 4.39M 4s 203150K .......... .......... .......... .......... .......... 77% 164M 4s 203200K .......... .......... .......... .......... .......... 77% 97.1M 4s 203250K .......... .......... .......... .......... .......... 77% 93.9M 4s 203300K .......... .......... .......... .......... .......... 77% 142M 4s 203350K .......... .......... .......... .......... .......... 77% 70.1M 4s 203400K .......... .......... .......... .......... .......... 77% 89.8M 4s 203450K .......... .......... .......... .......... .......... 77% 180M 4s 203500K .......... .......... .......... .......... .......... 77% 4.53M 4s 203550K .......... .......... .......... .......... .......... 77% 287M 4s 203600K .......... .......... .......... .......... .......... 77% 84.0M 4s 203650K .......... .......... .......... .......... .......... 77% 97.9M 4s 203700K .......... .......... .......... .......... .......... 77% 127M 4s 203750K .......... .......... .......... .......... .......... 77% 82.6M 4s 203800K .......... .......... .......... .......... .......... 77% 231M 4s 203850K .......... .......... .......... .......... .......... 77% 245M 4s 203900K .......... .......... .......... .......... .......... 77% 3.53M 4s 203950K .......... .......... .......... .......... .......... 77% 195M 4s 204000K .......... .......... .......... .......... .......... 77% 235M 4s 204050K .......... .......... .......... .......... .......... 77% 174M 4s 204100K .......... .......... .......... .......... .......... 77% 199M 4s 204150K .......... .......... .......... .......... .......... 77% 228M 4s 204200K .......... .......... .......... .......... .......... 77% 124M 4s 204250K .......... .......... .......... .......... .......... 77% 281M 4s 204300K .......... .......... .......... .......... .......... 77% 2.72M 4s 204350K .......... .......... .......... .......... .......... 77% 247M 4s 204400K .......... .......... .......... .......... .......... 77% 298M 4s 204450K .......... .......... .......... .......... .......... 77% 213M 4s 204500K .......... .......... .......... .......... .......... 78% 82.2M 4s 204550K .......... .......... .......... .......... .......... 78% 180M 4s 204600K .......... .......... .......... .......... .......... 78% 160M 4s 204650K .......... .......... .......... .......... .......... 78% 68.8M 4s 204700K .......... .......... .......... .......... .......... 78% 3.74M 4s 204750K .......... .......... .......... .......... .......... 78% 56.2M 4s 204800K .......... .......... .......... .......... .......... 78% 74.8M 4s 204850K .......... .......... .......... .......... .......... 78% 213M 4s 204900K .......... .......... .......... .......... .......... 78% 155M 4s 204950K .......... .......... .......... .......... .......... 78% 164M 4s 205000K .......... .......... .......... .......... .......... 78% 215M 4s 205050K .......... .......... .......... .......... .......... 78% 219M 4s 205100K .......... .......... .......... .......... .......... 78% 4.27M 4s 205150K .......... .......... .......... .......... .......... 78% 274M 4s 205200K .......... .......... .......... .......... .......... 78% 273M 4s 205250K .......... .......... .......... .......... .......... 78% 326M 4s 205300K .......... .......... .......... .......... .......... 78% 229M 4s 205350K .......... .......... .......... .......... .......... 78% 274M 4s 205400K .......... .......... .......... .......... .......... 78% 258M 4s 205450K .......... .......... .......... .......... .......... 78% 284M 4s 205500K .......... .......... .......... .......... .......... 78% 2.96M 4s 205550K .......... .......... .......... .......... .......... 78% 103M 4s 205600K .......... .......... .......... .......... .......... 78% 136M 4s 205650K .......... .......... .......... .......... .......... 78% 188M 4s 205700K .......... .......... .......... .......... .......... 78% 179M 4s 205750K .......... .......... .......... .......... .......... 78% 215M 4s 205800K .......... .......... .......... .......... .......... 78% 205M 4s 205850K .......... .......... .......... .......... .......... 78% 178M 4s 205900K .......... .......... .......... .......... .......... 78% 2.97M 4s 205950K .......... .......... .......... .......... .......... 78% 181M 4s 206000K .......... .......... .......... .......... .......... 78% 233M 4s 206050K .......... .......... .......... .......... .......... 78% 274M 4s 206100K .......... .......... .......... .......... .......... 78% 138M 4s 206150K .......... .......... .......... .......... .......... 78% 173M 4s 206200K .......... .......... .......... .......... .......... 78% 230M 4s 206250K .......... .......... .......... .......... .......... 78% 178M 4s 206300K .......... .......... .......... .......... .......... 78% 3.34M 4s 206350K .......... .......... .......... .......... .......... 78% 170M 4s 206400K .......... .......... .......... .......... .......... 78% 219M 4s 206450K .......... .......... .......... .......... .......... 78% 192M 4s 206500K .......... .......... .......... .......... .......... 78% 216M 4s 206550K .......... .......... .......... .......... .......... 78% 115M 4s 206600K .......... .......... .......... .......... .......... 78% 194M 4s 206650K .......... .......... .......... .......... .......... 78% 303M 4s 206700K .......... .......... .......... .......... .......... 78% 3.91M 4s 206750K .......... .......... .......... .......... .......... 78% 221M 4s 206800K .......... .......... .......... .......... .......... 78% 142M 4s 206850K .......... .......... .......... .......... .......... 78% 109M 4s 206900K .......... .......... .......... .......... .......... 78% 124M 4s 206950K .......... .......... .......... .......... .......... 78% 187M 4s 207000K .......... .......... .......... .......... .......... 78% 231M 4s 207050K .......... .......... .......... .......... .......... 78% 184M 4s 207100K .......... .......... .......... .......... .......... 79% 3.53M 4s 207150K .......... .......... .......... .......... .......... 79% 202M 4s 207200K .......... .......... .......... .......... .......... 79% 87.3M 4s 207250K .......... .......... .......... .......... .......... 79% 136M 4s 207300K .......... .......... .......... .......... .......... 79% 209M 4s 207350K .......... .......... .......... .......... .......... 79% 121M 4s 207400K .......... .......... .......... .......... .......... 79% 97.5M 4s 207450K .......... .......... .......... .......... .......... 79% 234M 4s 207500K .......... .......... .......... .......... .......... 79% 326M 4s 207550K .......... .......... .......... .......... .......... 79% 3.88M 4s 207600K .......... .......... .......... .......... .......... 79% 85.4M 4s 207650K .......... .......... .......... .......... .......... 79% 123M 4s 207700K .......... .......... .......... .......... .......... 79% 192M 4s 207750K .......... .......... .......... .......... .......... 79% 196M 4s 207800K .......... .......... .......... .......... .......... 79% 207M 4s 207850K .......... .......... .......... .......... .......... 79% 196M 4s 207900K .......... .......... .......... .......... .......... 79% 163M 4s 207950K .......... .......... .......... .......... .......... 79% 2.83M 4s 208000K .......... .......... .......... .......... .......... 79% 161M 4s 208050K .......... .......... .......... .......... .......... 79% 214M 4s 208100K .......... .......... .......... .......... .......... 79% 124M 4s 208150K .......... .......... .......... .......... .......... 79% 191M 4s 208200K .......... .......... .......... .......... .......... 79% 152M 4s 208250K .......... .......... .......... .......... .......... 79% 236M 4s 208300K .......... .......... .......... .......... .......... 79% 194M 4s 208350K .......... .......... .......... .......... .......... 79% 3.06M 4s 208400K .......... .......... .......... .......... .......... 79% 211M 4s 208450K .......... .......... .......... .......... .......... 79% 143M 4s 208500K .......... .......... .......... .......... .......... 79% 313M 4s 208550K .......... .......... .......... .......... .......... 79% 184M 4s 208600K .......... .......... .......... .......... .......... 79% 138M 4s 208650K .......... .......... .......... .......... .......... 79% 171M 3s 208700K .......... .......... .......... .......... .......... 79% 162M 3s 208750K .......... .......... .......... .......... .......... 79% 3.17M 3s 208800K .......... .......... .......... .......... .......... 79% 89.8M 3s 208850K .......... .......... .......... .......... .......... 79% 162M 3s 208900K .......... .......... .......... .......... .......... 79% 210M 3s 208950K .......... .......... .......... .......... .......... 79% 186M 3s 209000K .......... .......... .......... .......... .......... 79% 203M 3s 209050K .......... .......... .......... .......... .......... 79% 87.5M 3s 209100K .......... .......... .......... .......... .......... 79% 191M 3s 209150K .......... .......... .......... .......... .......... 79% 3.27M 3s 209200K .......... .......... .......... .......... .......... 79% 93.2M 3s 209250K .......... .......... .......... .......... .......... 79% 199M 3s 209300K .......... .......... .......... .......... .......... 79% 122M 3s 209350K .......... .......... .......... .......... .......... 79% 134M 3s 209400K .......... .......... .......... .......... .......... 79% 155M 3s 209450K .......... .......... .......... .......... .......... 79% 75.5M 3s 209500K .......... .......... .......... .......... .......... 79% 124M 3s 209550K .......... .......... .......... .......... .......... 79% 263M 3s 209600K .......... .......... .......... .......... .......... 79% 3.69M 3s 209650K .......... .......... .......... .......... .......... 79% 174M 3s 209700K .......... .......... .......... .......... .......... 79% 106M 3s 209750K .......... .......... .......... .......... .......... 80% 182M 3s 209800K .......... .......... .......... .......... .......... 80% 151M 3s 209850K .......... .......... .......... .......... .......... 80% 108M 3s 209900K .......... .......... .......... .......... .......... 80% 112M 3s 209950K .......... .......... .......... .......... .......... 80% 93.0M 3s 210000K .......... .......... .......... .......... .......... 80% 3.77M 3s 210050K .......... .......... .......... .......... .......... 80% 222M 3s 210100K .......... .......... .......... .......... .......... 80% 191M 3s 210150K .......... .......... .......... .......... .......... 80% 160M 3s 210200K .......... .......... .......... .......... .......... 80% 105M 3s 210250K .......... .......... .......... .......... .......... 80% 66.5M 3s 210300K .......... .......... .......... .......... .......... 80% 76.8M 3s 210350K .......... .......... .......... .......... .......... 80% 116M 3s 210400K .......... .......... .......... .......... .......... 80% 4.07M 3s 210450K .......... .......... .......... .......... .......... 80% 177M 3s 210500K .......... .......... .......... .......... .......... 80% 216M 3s 210550K .......... .......... .......... .......... .......... 80% 218M 3s 210600K .......... .......... .......... .......... .......... 80% 239M 3s 210650K .......... .......... .......... .......... .......... 80% 145K 3s 210700K .......... .......... .......... .......... .......... 80% 118M 3s 210750K .......... .......... .......... .......... .......... 80% 111M 3s 210800K .......... .......... .......... .......... .......... 80% 211M 3s 210850K .......... .......... .......... .......... .......... 80% 121M 3s 210900K .......... .......... .......... .......... .......... 80% 207M 3s 210950K .......... .......... .......... .......... .......... 80% 250M 3s 211000K .......... .......... .......... .......... .......... 80% 201M 3s 211050K .......... .......... .......... .......... .......... 80% 196M 3s 211100K .......... .......... .......... .......... .......... 80% 281M 3s 211150K .......... .......... .......... .......... .......... 80% 337M 3s 211200K .......... .......... .......... .......... .......... 80% 298M 3s 211250K .......... .......... .......... .......... .......... 80% 344M 3s 211300K .......... .......... .......... .......... .......... 80% 346M 3s 211350K .......... .......... .......... .......... .......... 80% 248M 3s 211400K .......... .......... .......... .......... .......... 80% 243M 3s 211450K .......... .......... .......... .......... .......... 80% 274M 3s 211500K .......... .......... .......... .......... .......... 80% 346M 3s 211550K .......... .......... .......... .......... .......... 80% 339M 3s 211600K .......... .......... .......... .......... .......... 80% 291M 3s 211650K .......... .......... .......... .......... .......... 80% 18.8M 3s 211700K .......... .......... .......... .......... .......... 80% 127M 3s 211750K .......... .......... .......... .......... .......... 80% 148M 3s 211800K .......... .......... .......... .......... .......... 80% 196M 3s 211850K .......... .......... .......... .......... .......... 80% 190M 3s 211900K .......... .......... .......... .......... .......... 80% 200M 3s 211950K .......... .......... .......... .......... .......... 80% 159M 3s 212000K .......... .......... .......... .......... .......... 80% 183M 3s 212050K .......... .......... .......... .......... .......... 80% 176M 3s 212100K .......... .......... .......... .......... .......... 80% 151M 3s 212150K .......... .......... .......... .......... .......... 80% 276M 3s 212200K .......... .......... .......... .......... .......... 80% 256M 3s 212250K .......... .......... .......... .......... .......... 80% 326M 3s 212300K .......... .......... .......... .......... .......... 80% 242M 3s 212350K .......... .......... .......... .......... .......... 81% 167M 3s 212400K .......... .......... .......... .......... .......... 81% 214M 3s 212450K .......... .......... .......... .......... .......... 81% 186M 3s 212500K .......... .......... .......... .......... .......... 81% 218M 3s 212550K .......... .......... .......... .......... .......... 81% 219M 3s 212600K .......... .......... .......... .......... .......... 81% 186M 3s 212650K .......... .......... .......... .......... .......... 81% 217M 3s 212700K .......... .......... .......... .......... .......... 81% 1.34M 3s 212750K .......... .......... .......... .......... .......... 81% 132M 3s 212800K .......... .......... .......... .......... .......... 81% 90.9M 3s 212850K .......... .......... .......... .......... .......... 81% 90.4M 3s 212900K .......... .......... .......... .......... .......... 81% 136M 3s 212950K .......... .......... .......... .......... .......... 81% 109M 3s 213000K .......... .......... .......... .......... .......... 81% 84.3M 3s 213050K .......... .......... .......... .......... .......... 81% 33.1M 3s 213100K .......... .......... .......... .......... .......... 81% 155M 3s 213150K .......... .......... .......... .......... .......... 81% 3.33M 3s 213200K .......... .......... .......... .......... .......... 81% 254M 3s 213250K .......... .......... .......... .......... .......... 81% 254M 3s 213300K .......... .......... .......... .......... .......... 81% 237M 3s 213350K .......... .......... .......... .......... .......... 81% 163M 3s 213400K .......... .......... .......... .......... .......... 81% 200M 3s 213450K .......... .......... .......... .......... .......... 81% 214M 3s 213500K .......... .......... .......... .......... .......... 81% 194M 3s 213550K .......... .......... .......... .......... .......... 81% 3.25M 3s 213600K .......... .......... .......... .......... .......... 81% 81.2M 3s 213650K .......... .......... .......... .......... .......... 81% 139M 3s 213700K .......... .......... .......... .......... .......... 81% 183M 3s 213750K .......... .......... .......... .......... .......... 81% 195M 3s 213800K .......... .......... .......... .......... .......... 81% 104M 3s 213850K .......... .......... .......... .......... .......... 81% 93.4M 3s 213900K .......... .......... .......... .......... .......... 81% 133M 3s 213950K .......... .......... .......... .......... .......... 81% 2.79M 3s 214000K .......... .......... .......... .......... .......... 81% 138M 3s 214050K .......... .......... .......... .......... .......... 81% 111M 3s 214100K .......... .......... .......... .......... .......... 81% 118M 3s 214150K .......... .......... .......... .......... .......... 81% 226M 3s 214200K .......... .......... .......... .......... .......... 81% 167M 3s 214250K .......... .......... .......... .......... .......... 81% 228M 3s 214300K .......... .......... .......... .......... .......... 81% 173M 3s 214350K .......... .......... .......... .......... .......... 81% 170M 3s 214400K .......... .......... .......... .......... .......... 81% 3.93M 3s 214450K .......... .......... .......... .......... .......... 81% 182M 3s 214500K .......... .......... .......... .......... .......... 81% 198M 3s 214550K .......... .......... .......... .......... .......... 81% 169M 3s 214600K .......... .......... .......... .......... .......... 81% 200M 3s 214650K .......... .......... .......... .......... .......... 81% 239M 3s 214700K .......... .......... .......... .......... .......... 81% 271M 3s 214750K .......... .......... .......... .......... .......... 81% 131M 3s 214800K .......... .......... .......... .......... .......... 81% 2.34M 3s 214850K .......... .......... .......... .......... .......... 81% 78.8M 3s 214900K .......... .......... .......... .......... .......... 81% 224M 3s 214950K .......... .......... .......... .......... .......... 81% 131M 3s 215000K .......... .......... .......... .......... .......... 82% 201M 3s 215050K .......... .......... .......... .......... .......... 82% 184M 3s 215100K .......... .......... .......... .......... .......... 82% 183M 3s 215150K .......... .......... .......... .......... .......... 82% 140M 3s 215200K .......... .......... .......... .......... .......... 82% 167M 3s 215250K .......... .......... .......... .......... .......... 82% 3.48M 3s 215300K .......... .......... .......... .......... .......... 82% 177M 3s 215350K .......... .......... .......... .......... .......... 82% 179M 3s 215400K .......... .......... .......... .......... .......... 82% 176M 3s 215450K .......... .......... .......... .......... .......... 82% 186M 3s 215500K .......... .......... .......... .......... .......... 82% 213M 3s 215550K .......... .......... .......... .......... .......... 82% 216M 3s 215600K .......... .......... .......... .......... .......... 82% 195M 3s 215650K .......... .......... .......... .......... .......... 82% 3.28M 3s 215700K .......... .......... .......... .......... .......... 82% 189M 3s 215750K .......... .......... .......... .......... .......... 82% 137M 3s 215800K .......... .......... .......... .......... .......... 82% 208M 3s 215850K .......... .......... .......... .......... .......... 82% 191M 3s 215900K .......... .......... .......... .......... .......... 82% 229M 3s 215950K .......... .......... .......... .......... .......... 82% 208M 3s 216000K .......... .......... .......... .......... .......... 82% 234M 3s 216050K .......... .......... .......... .......... .......... 82% 241M 3s 216100K .......... .......... .......... .......... .......... 82% 3.97M 3s 216150K .......... .......... .......... .......... .......... 82% 152M 3s 216200K .......... .......... .......... .......... .......... 82% 128M 3s 216250K .......... .......... .......... .......... .......... 82% 197M 3s 216300K .......... .......... .......... .......... .......... 82% 217M 3s 216350K .......... .......... .......... .......... .......... 82% 157M 3s 216400K .......... .......... .......... .......... .......... 82% 207M 3s 216450K .......... .......... .......... .......... .......... 82% 145M 3s 216500K .......... .......... .......... .......... .......... 82% 2.58M 3s 216550K .......... .......... .......... .......... .......... 82% 171M 3s 216600K .......... .......... .......... .......... .......... 82% 162M 3s 216650K .......... .......... .......... .......... .......... 82% 96.7M 3s 216700K .......... .......... .......... .......... .......... 82% 85.1M 3s 216750K .......... .......... .......... .......... .......... 82% 261M 3s 216800K .......... .......... .......... .......... .......... 82% 80.2M 3s 216850K .......... .......... .......... .......... .......... 82% 119M 3s 216900K .......... .......... .......... .......... .......... 82% 158M 3s 216950K .......... .......... .......... .......... .......... 82% 2.84M 3s 217000K .......... .......... .......... .......... .......... 82% 118M 3s 217050K .......... .......... .......... .......... .......... 82% 201M 3s 217100K .......... .......... .......... .......... .......... 82% 124M 3s 217150K .......... .......... .......... .......... .......... 82% 229M 3s 217200K .......... .......... .......... .......... .......... 82% 158M 3s 217250K .......... .......... .......... .......... .......... 82% 127M 3s 217300K .......... .......... .......... .......... .......... 82% 116M 3s 217350K .......... .......... .......... .......... .......... 82% 3.60M 3s 217400K .......... .......... .......... .......... .......... 82% 247M 3s 217450K .......... .......... .......... .......... .......... 82% 138M 3s 217500K .......... .......... .......... .......... .......... 82% 83.3M 3s 217550K .......... .......... .......... .......... .......... 82% 218M 3s 217600K .......... .......... .......... .......... .......... 83% 122M 3s 217650K .......... .......... .......... .......... .......... 83% 138M 3s 217700K .......... .......... .......... .......... .......... 83% 137M 3s 217750K .......... .......... .......... .......... .......... 83% 198M 3s 217800K .......... .......... .......... .......... .......... 83% 3.05M 3s 217850K .......... .......... .......... .......... .......... 83% 127M 3s 217900K .......... .......... .......... .......... .......... 83% 92.7M 3s 217950K .......... .......... .......... .......... .......... 83% 134M 3s 218000K .......... .......... .......... .......... .......... 83% 131M 3s 218050K .......... .......... .......... .......... .......... 83% 126M 3s 218100K .......... .......... .......... .......... .......... 83% 101M 3s 218150K .......... .......... .......... .......... .......... 83% 122M 3s 218200K .......... .......... .......... .......... .......... 83% 2.83M 3s 218250K .......... .......... .......... .......... .......... 83% 187M 3s 218300K .......... .......... .......... .......... .......... 83% 189M 3s 218350K .......... .......... .......... .......... .......... 83% 157M 3s 218400K .......... .......... .......... .......... .......... 83% 173M 3s 218450K .......... .......... .......... .......... .......... 83% 172M 3s 218500K .......... .......... .......... .......... .......... 83% 159M 3s 218550K .......... .......... .......... .......... .......... 83% 155M 3s 218600K .......... .......... .......... .......... .......... 83% 148M 3s 218650K .......... .......... .......... .......... .......... 83% 3.54M 3s 218700K .......... .......... .......... .......... .......... 83% 150M 3s 218750K .......... .......... .......... .......... .......... 83% 154M 3s 218800K .......... .......... .......... .......... .......... 83% 106M 3s 218850K .......... .......... .......... .......... .......... 83% 95.2M 3s 218900K .......... .......... .......... .......... .......... 83% 123M 3s 218950K .......... .......... .......... .......... .......... 83% 101M 3s 219000K .......... .......... .......... .......... .......... 83% 109M 3s 219050K .......... .......... .......... .......... .......... 83% 3.02M 3s 219100K .......... .......... .......... .......... .......... 83% 178M 3s 219150K .......... .......... .......... .......... .......... 83% 235M 3s 219200K .......... .......... .......... .......... .......... 83% 90.1M 3s 219250K .......... .......... .......... .......... .......... 83% 67.8M 3s 219300K .......... .......... .......... .......... .......... 83% 133M 3s 219350K .......... .......... .......... .......... .......... 83% 184M 3s 219400K .......... .......... .......... .......... .......... 83% 230M 3s 219450K .......... .......... .......... .......... .......... 83% 195M 3s 219500K .......... .......... .......... .......... .......... 83% 2.95M 3s 219550K .......... .......... .......... .......... .......... 83% 213M 3s 219600K .......... .......... .......... .......... .......... 83% 157M 3s 219650K .......... .......... .......... .......... .......... 83% 291M 3s 219700K .......... .......... .......... .......... .......... 83% 124M 3s 219750K .......... .......... .......... .......... .......... 83% 218M 3s 219800K .......... .......... .......... .......... .......... 83% 174M 3s 219850K .......... .......... .......... .......... .......... 83% 130M 3s 219900K .......... .......... .......... .......... .......... 83% 206M 3s 219950K .......... .......... .......... .......... .......... 83% 2.45M 3s 220000K .......... .......... .......... .......... .......... 83% 211M 3s 220050K .......... .......... .......... .......... .......... 83% 167M 3s 220100K .......... .......... .......... .......... .......... 83% 170M 3s 220150K .......... .......... .......... .......... .......... 83% 119M 3s 220200K .......... .......... .......... .......... .......... 83% 188M 3s 220250K .......... .......... .......... .......... .......... 84% 227M 3s 220300K .......... .......... .......... .......... .......... 84% 191M 3s 220350K .......... .......... .......... .......... .......... 84% 3.09M 3s 220400K .......... .......... .......... .......... .......... 84% 233M 3s 220450K .......... .......... .......... .......... .......... 84% 178M 3s 220500K .......... .......... .......... .......... .......... 84% 186M 3s 220550K .......... .......... .......... .......... .......... 84% 138M 3s 220600K .......... .......... .......... .......... .......... 84% 110M 3s 220650K .......... .......... .......... .......... .......... 84% 155M 3s 220700K .......... .......... .......... .......... .......... 84% 130M 3s 220750K .......... .......... .......... .......... .......... 84% 159M 3s 220800K .......... .......... .......... .......... .......... 84% 3.93M 3s 220850K .......... .......... .......... .......... .......... 84% 123M 3s 220900K .......... .......... .......... .......... .......... 84% 96.9M 3s 220950K .......... .......... .......... .......... .......... 84% 108M 3s 221000K .......... .......... .......... .......... .......... 84% 217M 3s 221050K .......... .......... .......... .......... .......... 84% 95.2M 3s 221100K .......... .......... .......... .......... .......... 84% 143M 3s 221150K .......... .......... .......... .......... .......... 84% 208M 3s 221200K .......... .......... .......... .......... .......... 84% 3.04M 3s 221250K .......... .......... .......... .......... .......... 84% 159M 3s 221300K .......... .......... .......... .......... .......... 84% 194M 3s 221350K .......... .......... .......... .......... .......... 84% 174M 3s 221400K .......... .......... .......... .......... .......... 84% 217M 3s 221450K .......... .......... .......... .......... .......... 84% 172M 3s 221500K .......... .......... .......... .......... .......... 84% 212M 3s 221550K .......... .......... .......... .......... .......... 84% 143M 3s 221600K .......... .......... .......... .......... .......... 84% 148M 3s 221650K .......... .......... .......... .......... .......... 84% 3.48M 3s 221700K .......... .......... .......... .......... .......... 84% 186M 3s 221750K .......... .......... .......... .......... .......... 84% 184M 3s 221800K .......... .......... .......... .......... .......... 84% 130M 3s 221850K .......... .......... .......... .......... .......... 84% 164M 3s 221900K .......... .......... .......... .......... .......... 84% 56.7M 3s 221950K .......... .......... .......... .......... .......... 84% 145M 3s 222000K .......... .......... .......... .......... .......... 84% 37.3M 3s 222050K .......... .......... .......... .......... .......... 84% 70.6M 3s 222100K .......... .......... .......... .......... .......... 84% 3.47M 3s 222150K .......... .......... .......... .......... .......... 84% 139M 3s 222200K .......... .......... .......... .......... .......... 84% 83.5M 3s 222250K .......... .......... .......... .......... .......... 84% 152M 3s 222300K .......... .......... .......... .......... .......... 84% 113M 3s 222350K .......... .......... .......... .......... .......... 84% 85.1M 3s 222400K .......... .......... .......... .......... .......... 84% 120M 3s 222450K .......... .......... .......... .......... .......... 84% 56.6M 3s 222500K .......... .......... .......... .......... .......... 84% 1.83M 3s 222550K .......... .......... .......... .......... .......... 84% 123M 3s 222600K .......... .......... .......... .......... .......... 84% 154M 3s 222650K .......... .......... .......... .......... .......... 84% 148M 3s 222700K .......... .......... .......... .......... .......... 84% 205M 3s 222750K .......... .......... .......... .......... .......... 84% 196M 3s 222800K .......... .......... .......... .......... .......... 84% 159M 3s 222850K .......... .......... .......... .......... .......... 85% 210M 3s 222900K .......... .......... .......... .......... .......... 85% 116M 3s 222950K .......... .......... .......... .......... .......... 85% 1.68M 3s 223000K .......... .......... .......... .......... .......... 85% 160M 3s 223050K .......... .......... .......... .......... .......... 85% 171M 3s 223100K .......... .......... .......... .......... .......... 85% 198M 3s 223150K .......... .......... .......... .......... .......... 85% 97.7M 3s 223200K .......... .......... .......... .......... .......... 85% 198M 3s 223250K .......... .......... .......... .......... .......... 85% 228M 3s 223300K .......... .......... .......... .......... .......... 85% 169M 3s 223350K .......... .......... .......... .......... .......... 85% 180M 3s 223400K .......... .......... .......... .......... .......... 85% 3.44M 3s 223450K .......... .......... .......... .......... .......... 85% 162M 3s 223500K .......... .......... .......... .......... .......... 85% 98.8M 3s 223550K .......... .......... .......... .......... .......... 85% 228M 3s 223600K .......... .......... .......... .......... .......... 85% 197M 3s 223650K .......... .......... .......... .......... .......... 85% 214M 3s 223700K .......... .......... .......... .......... .......... 85% 104M 3s 223750K .......... .......... .......... .......... .......... 85% 155M 3s 223800K .......... .......... .......... .......... .......... 85% 184M 3s 223850K .......... .......... .......... .......... .......... 85% 2.99M 2s 223900K .......... .......... .......... .......... .......... 85% 287M 2s 223950K .......... .......... .......... .......... .......... 85% 119M 2s 224000K .......... .......... .......... .......... .......... 85% 98.2M 2s 224050K .......... .......... .......... .......... .......... 85% 185M 2s 224100K .......... .......... .......... .......... .......... 85% 178M 2s 224150K .......... .......... .......... .......... .......... 85% 162M 2s 224200K .......... .......... .......... .......... .......... 85% 186M 2s 224250K .......... .......... .......... .......... .......... 85% 3.86M 2s 224300K .......... .......... .......... .......... .......... 85% 177M 2s 224350K .......... .......... .......... .......... .......... 85% 105M 2s 224400K .......... .......... .......... .......... .......... 85% 158M 2s 224450K .......... .......... .......... .......... .......... 85% 150M 2s 224500K .......... .......... .......... .......... .......... 85% 159M 2s 224550K .......... .......... .......... .......... .......... 85% 164M 2s 224600K .......... .......... .......... .......... .......... 85% 160M 2s 224650K .......... .......... .......... .......... .......... 85% 224M 2s 224700K .......... .......... .......... .......... .......... 85% 2.75M 2s 224750K .......... .......... .......... .......... .......... 85% 208M 2s 224800K .......... .......... .......... .......... .......... 85% 220M 2s 224850K .......... .......... .......... .......... .......... 85% 191M 2s 224900K .......... .......... .......... .......... .......... 85% 165M 2s 224950K .......... .......... .......... .......... .......... 85% 183M 2s 225000K .......... .......... .......... .......... .......... 85% 95.9M 2s 225050K .......... .......... .......... .......... .......... 85% 210M 2s 225100K .......... .......... .......... .......... .......... 85% 142M 2s 225150K .......... .......... .......... .......... .......... 85% 3.19M 2s 225200K .......... .......... .......... .......... .......... 85% 243M 2s 225250K .......... .......... .......... .......... .......... 85% 115M 2s 225300K .......... .......... .......... .......... .......... 85% 45.4M 2s 225350K .......... .......... .......... .......... .......... 85% 101M 2s 225400K .......... .......... .......... .......... .......... 85% 220M 2s 225450K .......... .......... .......... .......... .......... 86% 79.7M 2s 225500K .......... .......... .......... .......... .......... 86% 110M 2s 225550K .......... .......... .......... .......... .......... 86% 178M 2s 225600K .......... .......... .......... .......... .......... 86% 3.08M 2s 225650K .......... .......... .......... .......... .......... 86% 153M 2s 225700K .......... .......... .......... .......... .......... 86% 174M 2s 225750K .......... .......... .......... .......... .......... 86% 165M 2s 225800K .......... .......... .......... .......... .......... 86% 159M 2s 225850K .......... .......... .......... .......... .......... 86% 148M 2s 225900K .......... .......... .......... .......... .......... 86% 168M 2s 225950K .......... .......... .......... .......... .......... 86% 188M 2s 226000K .......... .......... .......... .......... .......... 86% 54.4M 2s 226050K .......... .......... .......... .......... .......... 86% 3.68M 2s 226100K .......... .......... .......... .......... .......... 86% 33.7M 2s 226150K .......... .......... .......... .......... .......... 86% 300M 2s 226200K .......... .......... .......... .......... .......... 86% 179M 2s 226250K .......... .......... .......... .......... .......... 86% 210M 2s 226300K .......... .......... .......... .......... .......... 86% 112M 2s 226350K .......... .......... .......... .......... .......... 86% 115M 2s 226400K .......... .......... .......... .......... .......... 86% 99.6M 2s 226450K .......... .......... .......... .......... .......... 86% 3.48M 2s 226500K .......... .......... .......... .......... .......... 86% 265M 2s 226550K .......... .......... .......... .......... .......... 86% 286M 2s 226600K .......... .......... .......... .......... .......... 86% 239M 2s 226650K .......... .......... .......... .......... .......... 86% 282M 2s 226700K .......... .......... .......... .......... .......... 86% 247M 2s 226750K .......... .......... .......... .......... .......... 86% 291M 2s 226800K .......... .......... .......... .......... .......... 86% 321M 2s 226850K .......... .......... .......... .......... .......... 86% 263M 2s 226900K .......... .......... .......... .......... .......... 86% 3.44M 2s 226950K .......... .......... .......... .......... .......... 86% 200M 2s 227000K .......... .......... .......... .......... .......... 86% 237M 2s 227050K .......... .......... .......... .......... .......... 86% 182M 2s 227100K .......... .......... .......... .......... .......... 86% 132M 2s 227150K .......... .......... .......... .......... .......... 86% 228M 2s 227200K .......... .......... .......... .......... .......... 86% 194M 2s 227250K .......... .......... .......... .......... .......... 86% 231M 2s 227300K .......... .......... .......... .......... .......... 86% 227M 2s 227350K .......... .......... .......... .......... .......... 86% 2.91M 2s 227400K .......... .......... .......... .......... .......... 86% 289M 2s 227450K .......... .......... .......... .......... .......... 86% 109M 2s 227500K .......... .......... .......... .......... .......... 86% 197M 2s 227550K .......... .......... .......... .......... .......... 86% 274M 2s 227600K .......... .......... .......... .......... .......... 86% 236M 2s 227650K .......... .......... .......... .......... .......... 86% 323M 2s 227700K .......... .......... .......... .......... .......... 86% 263M 2s 227750K .......... .......... .......... .......... .......... 86% 270M 2s 227800K .......... .......... .......... .......... .......... 86% 2.58M 2s 227850K .......... .......... .......... .......... .......... 86% 158M 2s 227900K .......... .......... .......... .......... .......... 86% 136M 2s 227950K .......... .......... .......... .......... .......... 86% 168M 2s 228000K .......... .......... .......... .......... .......... 86% 171M 2s 228050K .......... .......... .......... .......... .......... 86% 85.5M 2s 228100K .......... .......... .......... .......... .......... 87% 197M 2s 228150K .......... .......... .......... .......... .......... 87% 186M 2s 228200K .......... .......... .......... .......... .......... 87% 135M 2s 228250K .......... .......... .......... .......... .......... 87% 2.96M 2s 228300K .......... .......... .......... .......... .......... 87% 199M 2s 228350K .......... .......... .......... .......... .......... 87% 133M 2s 228400K .......... .......... .......... .......... .......... 87% 120M 2s 228450K .......... .......... .......... .......... .......... 87% 225M 2s 228500K .......... .......... .......... .......... .......... 87% 187M 2s 228550K .......... .......... .......... .......... .......... 87% 189M 2s 228600K .......... .......... .......... .......... .......... 87% 128M 2s 228650K .......... .......... .......... .......... .......... 87% 173M 2s 228700K .......... .......... .......... .......... .......... 87% 3.45M 2s 228750K .......... .......... .......... .......... .......... 87% 145M 2s 228800K .......... .......... .......... .......... .......... 87% 229M 2s 228850K .......... .......... .......... .......... .......... 87% 171M 2s 228900K .......... .......... .......... .......... .......... 87% 147M 2s 228950K .......... .......... .......... .......... .......... 87% 122M 2s 229000K .......... .......... .......... .......... .......... 87% 107M 2s 229050K .......... .......... .......... .......... .......... 87% 115M 2s 229100K .......... .......... .......... .......... .......... 87% 72.1M 2s 229150K .......... .......... .......... .......... .......... 87% 3.72M 2s 229200K .......... .......... .......... .......... .......... 87% 80.0M 2s 229250K .......... .......... .......... .......... .......... 87% 133M 2s 229300K .......... .......... .......... .......... .......... 87% 226M 2s 229350K .......... .......... .......... .......... .......... 87% 111M 2s 229400K .......... .......... .......... .......... .......... 87% 141M 2s 229450K .......... .......... .......... .......... .......... 87% 169M 2s 229500K .......... .......... .......... .......... .......... 87% 215M 2s 229550K .......... .......... .......... .......... .......... 87% 198M 2s 229600K .......... .......... .......... .......... .......... 87% 3.34M 2s 229650K .......... .......... .......... .......... .......... 87% 175M 2s 229700K .......... .......... .......... .......... .......... 87% 103M 2s 229750K .......... .......... .......... .......... .......... 87% 211M 2s 229800K .......... .......... .......... .......... .......... 87% 124M 2s 229850K .......... .......... .......... .......... .......... 87% 121M 2s 229900K .......... .......... .......... .......... .......... 87% 166M 2s 229950K .......... .......... .......... .......... .......... 87% 83.9M 2s 230000K .......... .......... .......... .......... .......... 87% 2.75M 2s 230050K .......... .......... .......... .......... .......... 87% 98.6M 2s 230100K .......... .......... .......... .......... .......... 87% 88.1M 2s 230150K .......... .......... .......... .......... .......... 87% 89.9M 2s 230200K .......... .......... .......... .......... .......... 87% 138M 2s 230250K .......... .......... .......... .......... .......... 87% 242M 2s 230300K .......... .......... .......... .......... .......... 87% 182M 2s 230350K .......... .......... .......... .......... .......... 87% 189M 2s 230400K .......... .......... .......... .......... .......... 87% 145M 2s 230450K .......... .......... .......... .......... .......... 87% 3.36M 2s 230500K .......... .......... .......... .......... .......... 87% 136M 2s 230550K .......... .......... .......... .......... .......... 87% 173M 2s 230600K .......... .......... .......... .......... .......... 87% 101M 2s 230650K .......... .......... .......... .......... .......... 87% 203M 2s 230700K .......... .......... .......... .......... .......... 88% 132M 2s 230750K .......... .......... .......... .......... .......... 88% 191M 2s 230800K .......... .......... .......... .......... .......... 88% 114M 2s 230850K .......... .......... .......... .......... .......... 88% 153M 2s 230900K .......... .......... .......... .......... .......... 88% 201M 2s 230950K .......... .......... .......... .......... .......... 88% 3.46M 2s 231000K .......... .......... .......... .......... .......... 88% 305M 2s 231050K .......... .......... .......... .......... .......... 88% 300M 2s 231100K .......... .......... .......... .......... .......... 88% 181M 2s 231150K .......... .......... .......... .......... .......... 88% 130M 2s 231200K .......... .......... .......... .......... .......... 88% 128M 2s 231250K .......... .......... .......... .......... .......... 88% 155M 2s 231300K .......... .......... .......... .......... .......... 88% 220M 2s 231350K .......... .......... .......... .......... .......... 88% 3.65M 2s 231400K .......... .......... .......... .......... .......... 88% 89.6M 2s 231450K .......... .......... .......... .......... .......... 88% 128M 2s 231500K .......... .......... .......... .......... .......... 88% 159M 2s 231550K .......... .......... .......... .......... .......... 88% 176M 2s 231600K .......... .......... .......... .......... .......... 88% 138M 2s 231650K .......... .......... .......... .......... .......... 88% 141M 2s 231700K .......... .......... .......... .......... .......... 88% 128M 2s 231750K .......... .......... .......... .......... .......... 88% 146M 2s 231800K .......... .......... .......... .......... .......... 88% 65.2M 2s 231850K .......... .......... .......... .......... .......... 88% 3.28M 2s 231900K .......... .......... .......... .......... .......... 88% 287M 2s 231950K .......... .......... .......... .......... .......... 88% 103M 2s 232000K .......... .......... .......... .......... .......... 88% 109M 2s 232050K .......... .......... .......... .......... .......... 88% 83.8M 2s 232100K .......... .......... .......... .......... .......... 88% 96.7M 2s 232150K .......... .......... .......... .......... .......... 88% 95.0M 2s 232200K .......... .......... .......... .......... .......... 88% 131M 2s 232250K .......... .......... .......... .......... .......... 88% 3.77M 2s 232300K .......... .......... .......... .......... .......... 88% 97.9M 2s 232350K .......... .......... .......... .......... .......... 88% 149M 2s 232400K .......... .......... .......... .......... .......... 88% 182M 2s 232450K .......... .......... .......... .......... .......... 88% 103M 2s 232500K .......... .......... .......... .......... .......... 88% 122M 2s 232550K .......... .......... .......... .......... .......... 88% 160M 2s 232600K .......... .......... .......... .......... .......... 88% 67.4M 2s 232650K .......... .......... .......... .......... .......... 88% 99.0M 2s 232700K .......... .......... .......... .......... .......... 88% 4.17M 2s 232750K .......... .......... .......... .......... .......... 88% 114M 2s 232800K .......... .......... .......... .......... .......... 88% 227M 2s 232850K .......... .......... .......... .......... .......... 88% 85.4M 2s 232900K .......... .......... .......... .......... .......... 88% 277M 2s 232950K .......... .......... .......... .......... .......... 88% 177M 2s 233000K .......... .......... .......... .......... .......... 88% 219M 2s 233050K .......... .......... .......... .......... .......... 88% 219M 2s 233100K .......... .......... .......... .......... .......... 88% 96.7M 2s 233150K .......... .......... .......... .......... .......... 88% 211M 2s 233200K .......... .......... .......... .......... .......... 88% 901K 2s 233250K .......... .......... .......... .......... .......... 88% 182M 2s 233300K .......... .......... .......... .......... .......... 88% 263M 2s 233350K .......... .......... .......... .......... .......... 89% 102M 2s 233400K .......... .......... .......... .......... .......... 89% 181M 2s 233450K .......... .......... .......... .......... .......... 89% 80.2M 2s 233500K .......... .......... .......... .......... .......... 89% 212M 2s 233550K .......... .......... .......... .......... .......... 89% 118M 2s 233600K .......... .......... .......... .......... .......... 89% 72.0M 2s 233650K .......... .......... .......... .......... .......... 89% 3.47M 2s 233700K .......... .......... .......... .......... .......... 89% 195M 2s 233750K .......... .......... .......... .......... .......... 89% 226M 2s 233800K .......... .......... .......... .......... .......... 89% 236M 2s 233850K .......... .......... .......... .......... .......... 89% 210M 2s 233900K .......... .......... .......... .......... .......... 89% 257M 2s 233950K .......... .......... .......... .......... .......... 89% 214M 2s 234000K .......... .......... .......... .......... .......... 89% 211M 2s 234050K .......... .......... .......... .......... .......... 89% 323M 2s 234100K .......... .......... .......... .......... .......... 89% 3.70M 2s 234150K .......... .......... .......... .......... .......... 89% 87.7M 2s 234200K .......... .......... .......... .......... .......... 89% 95.4M 2s 234250K .......... .......... .......... .......... .......... 89% 89.6M 2s 234300K .......... .......... .......... .......... .......... 89% 113M 2s 234350K .......... .......... .......... .......... .......... 89% 164M 2s 234400K .......... .......... .......... .......... .......... 89% 237M 2s 234450K .......... .......... .......... .......... .......... 89% 206M 2s 234500K .......... .......... .......... .......... .......... 89% 229M 2s 234550K .......... .......... .......... .......... .......... 89% 3.44M 2s 234600K .......... .......... .......... .......... .......... 89% 119M 2s 234650K .......... .......... .......... .......... .......... 89% 206M 2s 234700K .......... .......... .......... .......... .......... 89% 198M 2s 234750K .......... .......... .......... .......... .......... 89% 229M 2s 234800K .......... .......... .......... .......... .......... 89% 317M 2s 234850K .......... .......... .......... .......... .......... 89% 281M 2s 234900K .......... .......... .......... .......... .......... 89% 326M 2s 234950K .......... .......... .......... .......... .......... 89% 168M 2s 235000K .......... .......... .......... .......... .......... 89% 3.16M 2s 235050K .......... .......... .......... .......... .......... 89% 214M 2s 235100K .......... .......... .......... .......... .......... 89% 219M 2s 235150K .......... .......... .......... .......... .......... 89% 287M 2s 235200K .......... .......... .......... .......... .......... 89% 47.9M 2s 235250K .......... .......... .......... .......... .......... 89% 125M 2s 235300K .......... .......... .......... .......... .......... 89% 274M 2s 235350K .......... .......... .......... .......... .......... 89% 276M 2s 235400K .......... .......... .......... .......... .......... 89% 68.7M 2s 235450K .......... .......... .......... .......... .......... 89% 3.41M 2s 235500K .......... .......... .......... .......... .......... 89% 133M 2s 235550K .......... .......... .......... .......... .......... 89% 125M 2s 235600K .......... .......... .......... .......... .......... 89% 163M 2s 235650K .......... .......... .......... .......... .......... 89% 137M 2s 235700K .......... .......... .......... .......... .......... 89% 129M 2s 235750K .......... .......... .......... .......... .......... 89% 130M 2s 235800K .......... .......... .......... .......... .......... 89% 243M 2s 235850K .......... .......... .......... .......... .......... 89% 198M 2s 235900K .......... .......... .......... .......... .......... 89% 3.45M 2s 235950K .......... .......... .......... .......... .......... 90% 182M 2s 236000K .......... .......... .......... .......... .......... 90% 130M 2s 236050K .......... .......... .......... .......... .......... 90% 323M 2s 236100K .......... .......... .......... .......... .......... 90% 281M 2s 236150K .......... .......... .......... .......... .......... 90% 284M 2s 236200K .......... .......... .......... .......... .......... 90% 281M 2s 236250K .......... .......... .......... .......... .......... 90% 125M 2s 236300K .......... .......... .......... .......... .......... 90% 53.2M 2s 236350K .......... .......... .......... .......... .......... 90% 3.59M 2s 236400K .......... .......... .......... .......... .......... 90% 85.8M 2s 236450K .......... .......... .......... .......... .......... 90% 261M 2s 236500K .......... .......... .......... .......... .......... 90% 326M 2s 236550K .......... .......... .......... .......... .......... 90% 286M 2s 236600K .......... .......... .......... .......... .......... 90% 88.3M 2s 236650K .......... .......... .......... .......... .......... 90% 179M 2s 236700K .......... .......... .......... .......... .......... 90% 159M 2s 236750K .......... .......... .......... .......... .......... 90% 146M 2s 236800K .......... .......... .......... .......... .......... 90% 282M 2s 236850K .......... .......... .......... .......... .......... 90% 3.77M 2s 236900K .......... .......... .......... .......... .......... 90% 254M 2s 236950K .......... .......... .......... .......... .......... 90% 279M 2s 237000K .......... .......... .......... .......... .......... 90% 334M 2s 237050K .......... .......... .......... .......... .......... 90% 253M 2s 237100K .......... .......... .......... .......... .......... 90% 286M 2s 237150K .......... .......... .......... .......... .......... 90% 330M 2s 237200K .......... .......... .......... .......... .......... 90% 233M 2s 237250K .......... .......... .......... .......... .......... 90% 206M 2s 237300K .......... .......... .......... .......... .......... 90% 3.79M 2s 237350K .......... .......... .......... .......... .......... 90% 149M 2s 237400K .......... .......... .......... .......... .......... 90% 212M 2s 237450K .......... .......... .......... .......... .......... 90% 168M 2s 237500K .......... .......... .......... .......... .......... 90% 296M 2s 237550K .......... .......... .......... .......... .......... 90% 105M 2s 237600K .......... .......... .......... .......... .......... 90% 123M 2s 237650K .......... .......... .......... .......... .......... 90% 183M 2s 237700K .......... .......... .......... .......... .......... 90% 157M 2s 237750K .......... .......... .......... .......... .......... 90% 3.65M 2s 237800K .......... .......... .......... .......... .......... 90% 163M 2s 237850K .......... .......... .......... .......... .......... 90% 151M 2s 237900K .......... .......... .......... .......... .......... 90% 243M 2s 237950K .......... .......... .......... .......... .......... 90% 210M 2s 238000K .......... .......... .......... .......... .......... 90% 189M 2s 238050K .......... .......... .......... .......... .......... 90% 169M 2s 238100K .......... .......... .......... .......... .......... 90% 146M 2s 238150K .......... .......... .......... .......... .......... 90% 247M 2s 238200K .......... .......... .......... .......... .......... 90% 3.56M 2s 238250K .......... .......... .......... .......... .......... 90% 307M 2s 238300K .......... .......... .......... .......... .......... 90% 108M 2s 238350K .......... .......... .......... .......... .......... 90% 166M 2s 238400K .......... .......... .......... .......... .......... 90% 303M 2s 238450K .......... .......... .......... .......... .......... 90% 159M 2s 238500K .......... .......... .......... .......... .......... 90% 164M 2s 238550K .......... .......... .......... .......... .......... 90% 284M 2s 238600K .......... .......... .......... .......... .......... 91% 195M 2s 238650K .......... .......... .......... .......... .......... 91% 3.69M 1s 238700K .......... .......... .......... .......... .......... 91% 174M 1s 238750K .......... .......... .......... .......... .......... 91% 56.4M 1s 238800K .......... .......... .......... .......... .......... 91% 323M 1s 238850K .......... .......... .......... .......... .......... 91% 115M 1s 238900K .......... .......... .......... .......... .......... 91% 171M 1s 238950K .......... .......... .......... .......... .......... 91% 258M 1s 239000K .......... .......... .......... .......... .......... 91% 311M 1s 239050K .......... .......... .......... .......... .......... 91% 120M 1s 239100K .......... .......... .......... .......... .......... 91% 126M 1s 239150K .......... .......... .......... .......... .......... 91% 3.64M 1s 239200K .......... .......... .......... .......... .......... 91% 118M 1s 239250K .......... .......... .......... .......... .......... 91% 208M 1s 239300K .......... .......... .......... .......... .......... 91% 142M 1s 239350K .......... .......... .......... .......... .......... 91% 132M 1s 239400K .......... .......... .......... .......... .......... 91% 305M 1s 239450K .......... .......... .......... .......... .......... 91% 238M 1s 239500K .......... .......... .......... .......... .......... 91% 253M 1s 239550K .......... .......... .......... .......... .......... 91% 140M 1s 239600K .......... .......... .......... .......... .......... 91% 2.75M 1s 239650K .......... .......... .......... .......... .......... 91% 311M 1s 239700K .......... .......... .......... .......... .......... 91% 271M 1s 239750K .......... .......... .......... .......... .......... 91% 276M 1s 239800K .......... .......... .......... .......... .......... 91% 328M 1s 239850K .......... .......... .......... .......... .......... 91% 294M 1s 239900K .......... .......... .......... .......... .......... 91% 281M 1s 239950K .......... .......... .......... .......... .......... 91% 287M 1s 240000K .......... .......... .......... .......... .......... 91% 274M 1s 240050K .......... .......... .......... .......... .......... 91% 2.94M 1s 240100K .......... .......... .......... .......... .......... 91% 170M 1s 240150K .......... .......... .......... .......... .......... 91% 187M 1s 240200K .......... .......... .......... .......... .......... 91% 65.0M 1s 240250K .......... .......... .......... .......... .......... 91% 73.9M 1s 240300K .......... .......... .......... .......... .......... 91% 137M 1s 240350K .......... .......... .......... .......... .......... 91% 88.1M 1s 240400K .......... .......... .......... .......... .......... 91% 87.3M 1s 240450K .......... .......... .......... .......... .......... 91% 129M 1s 240500K .......... .......... .......... .......... .......... 91% 136M 1s 240550K .......... .......... .......... .......... .......... 91% 2.81M 1s 240600K .......... .......... .......... .......... .......... 91% 74.7M 1s 240650K .......... .......... .......... .......... .......... 91% 128M 1s 240700K .......... .......... .......... .......... .......... 91% 93.2M 1s 240750K .......... .......... .......... .......... .......... 91% 81.8M 1s 240800K .......... .......... .......... .......... .......... 91% 195M 1s 240850K .......... .......... .......... .......... .......... 91% 180M 1s 240900K .......... .......... .......... .......... .......... 91% 217M 1s 240950K .......... .......... .......... .......... .......... 91% 48.8M 1s 241000K .......... .......... .......... .......... .......... 91% 2.72M 1s 241050K .......... .......... .......... .......... .......... 91% 155M 1s 241100K .......... .......... .......... .......... .......... 91% 193M 1s 241150K .......... .......... .......... .......... .......... 91% 156M 1s 241200K .......... .......... .......... .......... .......... 92% 175M 1s 241250K .......... .......... .......... .......... .......... 92% 160M 1s 241300K .......... .......... .......... .......... .......... 92% 224M 1s 241350K .......... .......... .......... .......... .......... 92% 411K 1s 241400K .......... .......... .......... .......... .......... 92% 168M 1s 241450K .......... .......... .......... .......... .......... 92% 184M 1s 241500K .......... .......... .......... .......... .......... 92% 212M 1s 241550K .......... .......... .......... .......... .......... 92% 160M 1s 241600K .......... .......... .......... .......... .......... 92% 176M 1s 241650K .......... .......... .......... .......... .......... 92% 185M 1s 241700K .......... .......... .......... .......... .......... 92% 83.0M 1s 241750K .......... .......... .......... .......... .......... 92% 79.1M 1s 241800K .......... .......... .......... .......... .......... 92% 188M 1s 241850K .......... .......... .......... .......... .......... 92% 154M 1s 241900K .......... .......... .......... .......... .......... 92% 227M 1s 241950K .......... .......... .......... .......... .......... 92% 70.1M 1s 242000K .......... .......... .......... .......... .......... 92% 140M 1s 242050K .......... .......... .......... .......... .......... 92% 200M 1s 242100K .......... .......... .......... .......... .......... 92% 115M 1s 242150K .......... .......... .......... .......... .......... 92% 3.10M 1s 242200K .......... .......... .......... .......... .......... 92% 188M 1s 242250K .......... .......... .......... .......... .......... 92% 236M 1s 242300K .......... .......... .......... .......... .......... 92% 143M 1s 242350K .......... .......... .......... .......... .......... 92% 168M 1s 242400K .......... .......... .......... .......... .......... 92% 113M 1s 242450K .......... .......... .......... .......... .......... 92% 158M 1s 242500K .......... .......... .......... .......... .......... 92% 25.0M 1s 242550K .......... .......... .......... .......... .......... 92% 199M 1s 242600K .......... .......... .......... .......... .......... 92% 3.24M 1s 242650K .......... .......... .......... .......... .......... 92% 198M 1s 242700K .......... .......... .......... .......... .......... 92% 174M 1s 242750K .......... .......... .......... .......... .......... 92% 167M 1s 242800K .......... .......... .......... .......... .......... 92% 182M 1s 242850K .......... .......... .......... .......... .......... 92% 164M 1s 242900K .......... .......... .......... .......... .......... 92% 203M 1s 242950K .......... .......... .......... .......... .......... 92% 154M 1s 243000K .......... .......... .......... .......... .......... 92% 214M 1s 243050K .......... .......... .......... .......... .......... 92% 187M 1s 243100K .......... .......... .......... .......... .......... 92% 2.80M 1s 243150K .......... .......... .......... .......... .......... 92% 209M 1s 243200K .......... .......... .......... .......... .......... 92% 187M 1s 243250K .......... .......... .......... .......... .......... 92% 161M 1s 243300K .......... .......... .......... .......... .......... 92% 210M 1s 243350K .......... .......... .......... .......... .......... 92% 185M 1s 243400K .......... .......... .......... .......... .......... 92% 44.5M 1s 243450K .......... .......... .......... .......... .......... 92% 172M 1s 243500K .......... .......... .......... .......... .......... 92% 156M 1s 243550K .......... .......... .......... .......... .......... 92% 3.15M 1s 243600K .......... .......... .......... .......... .......... 92% 148M 1s 243650K .......... .......... .......... .......... .......... 92% 205M 1s 243700K .......... .......... .......... .......... .......... 92% 257M 1s 243750K .......... .......... .......... .......... .......... 92% 313M 1s 243800K .......... .......... .......... .......... .......... 92% 132M 1s 243850K .......... .......... .......... .......... .......... 93% 170M 1s 243900K .......... .......... .......... .......... .......... 93% 301M 1s 243950K .......... .......... .......... .......... .......... 93% 184M 1s 244000K .......... .......... .......... .......... .......... 93% 2.71M 1s 244050K .......... .......... .......... .......... .......... 93% 184M 1s 244100K .......... .......... .......... .......... .......... 93% 150M 1s 244150K .......... .......... .......... .......... .......... 93% 192M 1s 244200K .......... .......... .......... .......... .......... 93% 153M 1s 244250K .......... .......... .......... .......... .......... 93% 163M 1s 244300K .......... .......... .......... .......... .......... 93% 148M 1s 244350K .......... .......... .......... .......... .......... 93% 270M 1s 244400K .......... .......... .......... .......... .......... 93% 184M 1s 244450K .......... .......... .......... .......... .......... 93% 79.5M 1s 244500K .......... .......... .......... .......... .......... 93% 3.38M 1s 244550K .......... .......... .......... .......... .......... 93% 205M 1s 244600K .......... .......... .......... .......... .......... 93% 127M 1s 244650K .......... .......... .......... .......... .......... 93% 214M 1s 244700K .......... .......... .......... .......... .......... 93% 182M 1s 244750K .......... .......... .......... .......... .......... 93% 215M 1s 244800K .......... .......... .......... .......... .......... 93% 207M 1s 244850K .......... .......... .......... .......... .......... 93% 182M 1s 244900K .......... .......... .......... .......... .......... 93% 134M 1s 244950K .......... .......... .......... .......... .......... 93% 3.35M 1s 245000K .......... .......... .......... .......... .......... 93% 281M 1s 245050K .......... .......... .......... .......... .......... 93% 309M 1s 245100K .......... .......... .......... .......... .......... 93% 265M 1s 245150K .......... .......... .......... .......... .......... 93% 317M 1s 245200K .......... .......... .......... .......... .......... 93% 276M 1s 245250K .......... .......... .......... .......... .......... 93% 309M 1s 245300K .......... .......... .......... .......... .......... 93% 326M 1s 245350K .......... .......... .......... .......... .......... 93% 207M 1s 245400K .......... .......... .......... .......... .......... 93% 271M 1s 245450K .......... .......... .......... .......... .......... 93% 3.53M 1s 245500K .......... .......... .......... .......... .......... 93% 218M 1s 245550K .......... .......... .......... .......... .......... 93% 103M 1s 245600K .......... .......... .......... .......... .......... 93% 180M 1s 245650K .......... .......... .......... .......... .......... 93% 220M 1s 245700K .......... .......... .......... .......... .......... 93% 187M 1s 245750K .......... .......... .......... .......... .......... 93% 149M 1s 245800K .......... .......... .......... .......... .......... 93% 247M 1s 245850K .......... .......... .......... .......... .......... 93% 202M 1s 245900K .......... .......... .......... .......... .......... 93% 2.12M 1s 245950K .......... .......... .......... .......... .......... 93% 87.2M 1s 246000K .......... .......... .......... .......... .......... 93% 140M 1s 246050K .......... .......... .......... .......... .......... 93% 156M 1s 246100K .......... .......... .......... .......... .......... 93% 162M 1s 246150K .......... .......... .......... .......... .......... 93% 210M 1s 246200K .......... .......... .......... .......... .......... 93% 123M 1s 246250K .......... .......... .......... .......... .......... 93% 180M 1s 246300K .......... .......... .......... .......... .......... 93% 189M 1s 246350K .......... .......... .......... .......... .......... 93% 2.09M 1s 246400K .......... .......... .......... .......... .......... 93% 180M 1s 246450K .......... .......... .......... .......... .......... 94% 174M 1s 246500K .......... .......... .......... .......... .......... 94% 857K 1s 246550K .......... .......... .......... .......... .......... 94% 211M 1s 246600K .......... .......... .......... .......... .......... 94% 84.5M 1s 246650K .......... .......... .......... .......... .......... 94% 76.3M 1s 246700K .......... .......... .......... .......... .......... 94% 59.2M 1s 246750K .......... .......... .......... .......... .......... 94% 39.4M 1s 246800K .......... .......... .......... .......... .......... 94% 182M 1s 246850K .......... .......... .......... .......... .......... 94% 3.62M 1s 246900K .......... .......... .......... .......... .......... 94% 214M 1s 246950K .......... .......... .......... .......... .......... 94% 132M 1s 247000K .......... .......... .......... .......... .......... 94% 215M 1s 247050K .......... .......... .......... .......... .......... 94% 233M 1s 247100K .......... .......... .......... .......... .......... 94% 196M 1s 247150K .......... .......... .......... .......... .......... 94% 273M 1s 247200K .......... .......... .......... .......... .......... 94% 258M 1s 247250K .......... .......... .......... .......... .......... 94% 313M 1s 247300K .......... .......... .......... .......... .......... 94% 279M 1s 247350K .......... .......... .......... .......... .......... 94% 3.26M 1s 247400K .......... .......... .......... .......... .......... 94% 208M 1s 247450K .......... .......... .......... .......... .......... 94% 54.2M 1s 247500K .......... .......... .......... .......... .......... 94% 97.1M 1s 247550K .......... .......... .......... .......... .......... 94% 96.7M 1s 247600K .......... .......... .......... .......... .......... 94% 72.6M 1s 247650K .......... .......... .......... .......... .......... 94% 91.1M 1s 247700K .......... .......... .......... .......... .......... 94% 86.7M 1s 247750K .......... .......... .......... .......... .......... 94% 57.9M 1s 247800K .......... .......... .......... .......... .......... 94% 3.64M 1s 247850K .......... .......... .......... .......... .......... 94% 140M 1s 247900K .......... .......... .......... .......... .......... 94% 131M 1s 247950K .......... .......... .......... .......... .......... 94% 168M 1s 248000K .......... .......... .......... .......... .......... 94% 64.1M 1s 248050K .......... .......... .......... .......... .......... 94% 81.2M 1s 248100K .......... .......... .......... .......... .......... 94% 148M 1s 248150K .......... .......... .......... .......... .......... 94% 212M 1s 248200K .......... .......... .......... .......... .......... 94% 121M 1s 248250K .......... .......... .......... .......... .......... 94% 155M 1s 248300K .......... .......... .......... .......... .......... 94% 2.63M 1s 248350K .......... .......... .......... .......... .......... 94% 166M 1s 248400K .......... .......... .......... .......... .......... 94% 182M 1s 248450K .......... .......... .......... .......... .......... 94% 163M 1s 248500K .......... .......... .......... .......... .......... 94% 193M 1s 248550K .......... .......... .......... .......... .......... 94% 20.2M 1s 248600K .......... .......... .......... .......... .......... 94% 112M 1s 248650K .......... .......... .......... .......... .......... 94% 176M 1s 248700K .......... .......... .......... .......... .......... 94% 182M 1s 248750K .......... .......... .......... .......... .......... 94% 2.78M 1s 248800K .......... .......... .......... .......... .......... 94% 303M 1s 248850K .......... .......... .......... .......... .......... 94% 145M 1s 248900K .......... .......... .......... .......... .......... 94% 191M 1s 248950K .......... .......... .......... .......... .......... 94% 151M 1s 249000K .......... .......... .......... .......... .......... 94% 203M 1s 249050K .......... .......... .......... .......... .......... 95% 103M 1s 249100K .......... .......... .......... .......... .......... 95% 228M 1s 249150K .......... .......... .......... .......... .......... 95% 185M 1s 249200K .......... .......... .......... .......... .......... 95% 85.7M 1s 249250K .......... .......... .......... .......... .......... 95% 3.16M 1s 249300K .......... .......... .......... .......... .......... 95% 206M 1s 249350K .......... .......... .......... .......... .......... 95% 187M 1s 249400K .......... .......... .......... .......... .......... 95% 171M 1s 249450K .......... .......... .......... .......... .......... 95% 158M 1s 249500K .......... .......... .......... .......... .......... 95% 220M 1s 249550K .......... .......... .......... .......... .......... 95% 150M 1s 249600K .......... .......... .......... .......... .......... 95% 67.1M 1s 249650K .......... .......... .......... .......... .......... 95% 216M 1s 249700K .......... .......... .......... .......... .......... 95% 3.03M 1s 249750K .......... .......... .......... .......... .......... 95% 183M 1s 249800K .......... .......... .......... .......... .......... 95% 161M 1s 249850K .......... .......... .......... .......... .......... 95% 189M 1s 249900K .......... .......... .......... .......... .......... 95% 292M 1s 249950K .......... .......... .......... .......... .......... 95% 199M 1s 250000K .......... .......... .......... .......... .......... 95% 315M 1s 250050K .......... .......... .......... .......... .......... 95% 317M 1s 250100K .......... .......... .......... .......... .......... 95% 154M 1s 250150K .......... .......... .......... .......... .......... 95% 197M 1s 250200K .......... .......... .......... .......... .......... 95% 3.45M 1s 250250K .......... .......... .......... .......... .......... 95% 245M 1s 250300K .......... .......... .......... .......... .......... 95% 292M 1s 250350K .......... .......... .......... .......... .......... 95% 260M 1s 250400K .......... .......... .......... .......... .......... 95% 279M 1s 250450K .......... .......... .......... .......... .......... 95% 273M 1s 250500K .......... .......... .......... .......... .......... 95% 178M 1s 250550K .......... .......... .......... .......... .......... 95% 212M 1s 250600K .......... .......... .......... .......... .......... 95% 132M 1s 250650K .......... .......... .......... .......... .......... 95% 69.6M 1s 250700K .......... .......... .......... .......... .......... 95% 2.48M 1s 250750K .......... .......... .......... .......... .......... 95% 315M 1s 250800K .......... .......... .......... .......... .......... 95% 307M 1s 250850K .......... .......... .......... .......... .......... 95% 210M 1s 250900K .......... .......... .......... .......... .......... 95% 203M 1s 250950K .......... .......... .......... .......... .......... 95% 203M 1s 251000K .......... .......... .......... .......... .......... 95% 330M 1s 251050K .......... .......... .......... .......... .......... 95% 227M 1s 251100K .......... .......... .......... .......... .......... 95% 263M 1s 251150K .......... .......... .......... .......... .......... 95% 3.21M 1s 251200K .......... .......... .......... .......... .......... 95% 206M 1s 251250K .......... .......... .......... .......... .......... 95% 300M 1s 251300K .......... .......... .......... .......... .......... 95% 291M 1s 251350K .......... .......... .......... .......... .......... 95% 261M 1s 251400K .......... .......... .......... .......... .......... 95% 326M 1s 251450K .......... .......... .......... .......... .......... 95% 204M 1s 251500K .......... .......... .......... .......... .......... 95% 315M 1s 251550K .......... .......... .......... .......... .......... 95% 311M 1s 251600K .......... .......... .......... .......... .......... 95% 488K 1s 251650K .......... .......... .......... .......... .......... 95% 3.06M 1s 251700K .......... .......... .......... .......... .......... 96% 125M 1s 251750K .......... .......... .......... .......... .......... 96% 104M 1s 251800K .......... .......... .......... .......... .......... 96% 186M 1s 251850K .......... .......... .......... .......... .......... 96% 195M 1s 251900K .......... .......... .......... .......... .......... 96% 178M 1s 251950K .......... .......... .......... .......... .......... 96% 184M 1s 252000K .......... .......... .......... .......... .......... 96% 199M 1s 252050K .......... .......... .......... .......... .......... 96% 207M 1s 252100K .......... .......... .......... .......... .......... 96% 8.93M 1s 252150K .......... .......... .......... .......... .......... 96% 153M 1s 252200K .......... .......... .......... .......... .......... 96% 174M 1s 252250K .......... .......... .......... .......... .......... 96% 210M 1s 252300K .......... .......... .......... .......... .......... 96% 180M 1s 252350K .......... .......... .......... .......... .......... 96% 6.20M 1s 252400K .......... .......... .......... .......... .......... 96% 219M 1s 252450K .......... .......... .......... .......... .......... 96% 206M 1s 252500K .......... .......... .......... .......... .......... 96% 239M 1s 252550K .......... .......... .......... .......... .......... 96% 237M 1s 252600K .......... .......... .......... .......... .......... 96% 6.84M 1s 252650K .......... .......... .......... .......... .......... 96% 6.11M 1s 252700K .......... .......... .......... .......... .......... 96% 84.8M 1s 252750K .......... .......... .......... .......... .......... 96% 188M 1s 252800K .......... .......... .......... .......... .......... 96% 186M 1s 252850K .......... .......... .......... .......... .......... 96% 80.3M 1s 252900K .......... .......... .......... .......... .......... 96% 113M 1s 252950K .......... .......... .......... .......... .......... 96% 188M 1s 253000K .......... .......... .......... .......... .......... 96% 155M 1s 253050K .......... .......... .......... .......... .......... 96% 228M 1s 253100K .......... .......... .......... .......... .......... 96% 2.78M 1s 253150K .......... .......... .......... .......... .......... 96% 237M 1s 253200K .......... .......... .......... .......... .......... 96% 268M 1s 253250K .......... .......... .......... .......... .......... 96% 92.7M 1s 253300K .......... .......... .......... .......... .......... 96% 135M 1s 253350K .......... .......... .......... .......... .......... 96% 273M 1s 253400K .......... .......... .......... .......... .......... 96% 298M 1s 253450K .......... .......... .......... .......... .......... 96% 110M 1s 253500K .......... .......... .......... .......... .......... 96% 189M 1s 253550K .......... .......... .......... .......... .......... 96% 2.64M 1s 253600K .......... .......... .......... .......... .......... 96% 104M 1s 253650K .......... .......... .......... .......... .......... 96% 3.20M 1s 253700K .......... .......... .......... .......... .......... 96% 145M 1s 253750K .......... .......... .......... .......... .......... 96% 101M 1s 253800K .......... .......... .......... .......... .......... 96% 65.4M 1s 253850K .......... .......... .......... .......... .......... 96% 60.5M 1s 253900K .......... .......... .......... .......... .......... 96% 119M 1s 253950K .......... .......... .......... .......... .......... 96% 174M 1s 254000K .......... .......... .......... .......... .......... 96% 121M 1s 254050K .......... .......... .......... .......... .......... 96% 2.96M 1s 254100K .......... .......... .......... .......... .......... 96% 233M 1s 254150K .......... .......... .......... .......... .......... 96% 198M 1s 254200K .......... .......... .......... .......... .......... 96% 99.0M 1s 254250K .......... .......... .......... .......... .......... 96% 79.8M 1s 254300K .......... .......... .......... .......... .......... 97% 138M 0s 254350K .......... .......... .......... .......... .......... 97% 121M 0s 254400K .......... .......... .......... .......... .......... 97% 108M 0s 254450K .......... .......... .......... .......... .......... 97% 82.8M 0s 254500K .......... .......... .......... .......... .......... 97% 135M 0s 254550K .......... .......... .......... .......... .......... 97% 4.52M 0s 254600K .......... .......... .......... .......... .......... 97% 265M 0s 254650K .......... .......... .......... .......... .......... 97% 195M 0s 254700K .......... .......... .......... .......... .......... 97% 151M 0s 254750K .......... .......... .......... .......... .......... 97% 305M 0s 254800K .......... .......... .......... .......... .......... 97% 300M 0s 254850K .......... .......... .......... .......... .......... 97% 223M 0s 254900K .......... .......... .......... .......... .......... 97% 237M 0s 254950K .......... .......... .......... .......... .......... 97% 115M 0s 255000K .......... .......... .......... .......... .......... 97% 4.81M 0s 255050K .......... .......... .......... .......... .......... 97% 140M 0s 255100K .......... .......... .......... .......... .......... 97% 170M 0s 255150K .......... .......... .......... .......... .......... 97% 105M 0s 255200K .......... .......... .......... .......... .......... 97% 120M 0s 255250K .......... .......... .......... .......... .......... 97% 198M 0s 255300K .......... .......... .......... .......... .......... 97% 177M 0s 255350K .......... .......... .......... .......... .......... 97% 184M 0s 255400K .......... .......... .......... .......... .......... 97% 181M 0s 255450K .......... .......... .......... .......... .......... 97% 110M 0s 255500K .......... .......... .......... .......... .......... 97% 4.99M 0s 255550K .......... .......... .......... .......... .......... 97% 191M 0s 255600K .......... .......... .......... .......... .......... 97% 200M 0s 255650K .......... .......... .......... .......... .......... 97% 210M 0s 255700K .......... .......... .......... .......... .......... 97% 143M 0s 255750K .......... .......... .......... .......... .......... 97% 227M 0s 255800K .......... .......... .......... .......... .......... 97% 230M 0s 255850K .......... .......... .......... .......... .......... 97% 243M 0s 255900K .......... .......... .......... .......... .......... 97% 115M 0s 255950K .......... .......... .......... .......... .......... 97% 141M 0s 256000K .......... .......... .......... .......... .......... 97% 5.29M 0s 256050K .......... .......... .......... .......... .......... 97% 120M 0s 256100K .......... .......... .......... .......... .......... 97% 183M 0s 256150K .......... .......... .......... .......... .......... 97% 142M 0s 256200K .......... .......... .......... .......... .......... 97% 224M 0s 256250K .......... .......... .......... .......... .......... 97% 305M 0s 256300K .......... .......... .......... .......... .......... 97% 146M 0s 256350K .......... .......... .......... .......... .......... 97% 257M 0s 256400K .......... .......... .......... .......... .......... 97% 111M 0s 256450K .......... .......... .......... .......... .......... 97% 75.0M 0s 256500K .......... .......... .......... .......... .......... 97% 4.76M 0s 256550K .......... .......... .......... .......... .......... 97% 307M 0s 256600K .......... .......... .......... .......... .......... 97% 180M 0s 256650K .......... .......... .......... .......... .......... 97% 292M 0s 256700K .......... .......... .......... .......... .......... 97% 1.01M 0s 256750K .......... .......... .......... .......... .......... 97% 193M 0s 256800K .......... .......... .......... .......... .......... 97% 203M 0s 256850K .......... .......... .......... .......... .......... 97% 156M 0s 256900K .......... .......... .......... .......... .......... 97% 67.7M 0s 256950K .......... .......... .......... .......... .......... 98% 128M 0s 257000K .......... .......... .......... .......... .......... 98% 3.94M 0s 257050K .......... .......... .......... .......... .......... 98% 185M 0s 257100K .......... .......... .......... .......... .......... 98% 138M 0s 257150K .......... .......... .......... .......... .......... 98% 102M 0s 257200K .......... .......... .......... .......... .......... 98% 119M 0s 257250K .......... .......... .......... .......... .......... 98% 229M 0s 257300K .......... .......... .......... .......... .......... 98% 289M 0s 257350K .......... .......... .......... .......... .......... 98% 100M 0s 257400K .......... .......... .......... .......... .......... 98% 239M 0s 257450K .......... .......... .......... .......... .......... 98% 3.27M 0s 257500K .......... .......... .......... .......... .......... 98% 204M 0s 257550K .......... .......... .......... .......... .......... 98% 158M 0s 257600K .......... .......... .......... .......... .......... 98% 173M 0s 257650K .......... .......... .......... .......... .......... 98% 311M 0s 257700K .......... .......... .......... .......... .......... 98% 260M 0s 257750K .......... .......... .......... .......... .......... 98% 73.5M 0s 257800K .......... .......... .......... .......... .......... 98% 212M 0s 257850K .......... .......... .......... .......... .......... 98% 181M 0s 257900K .......... .......... .......... .......... .......... 98% 170M 0s 257950K .......... .......... .......... .......... .......... 98% 3.01M 0s 258000K .......... .......... .......... .......... .......... 98% 230M 0s 258050K .......... .......... .......... .......... .......... 98% 171M 0s 258100K .......... .......... .......... .......... .......... 98% 173M 0s 258150K .......... .......... .......... .......... .......... 98% 223M 0s 258200K .......... .......... .......... .......... .......... 98% 238M 0s 258250K .......... .......... .......... .......... .......... 98% 243M 0s 258300K .......... .......... .......... .......... .......... 98% 265M 0s 258350K .......... .......... .......... .......... .......... 98% 215M 0s 258400K .......... .......... .......... .......... .......... 98% 268M 0s 258450K .......... .......... .......... .......... .......... 98% 2.90M 0s 258500K .......... .......... .......... .......... .......... 98% 214M 0s 258550K .......... .......... .......... .......... .......... 98% 152M 0s 258600K .......... .......... .......... .......... .......... 98% 125M 0s 258650K .......... .......... .......... .......... .......... 98% 222M 0s 258700K .......... .......... .......... .......... .......... 98% 182M 0s 258750K .......... .......... .......... .......... .......... 98% 1.53M 0s 258800K .......... .......... .......... .......... .......... 98% 176M 0s 258850K .......... .......... .......... .......... .......... 98% 86.6M 0s 258900K .......... .......... .......... .......... .......... 98% 212M 0s 258950K .......... .......... .......... .......... .......... 98% 2.72M 0s 259000K .......... .......... .......... .......... .......... 98% 212M 0s 259050K .......... .......... .......... .......... .......... 98% 243M 0s 259100K .......... .......... .......... .......... .......... 98% 254M 0s 259150K .......... .......... .......... .......... .......... 98% 315M 0s 259200K .......... .......... .......... .......... .......... 98% 148M 0s 259250K .......... .......... .......... .......... .......... 98% 210M 0s 259300K .......... .......... .......... .......... .......... 98% 197M 0s 259350K .......... .......... .......... .......... .......... 98% 183M 0s 259400K .......... .......... .......... .......... .......... 98% 309M 0s 259450K .......... .......... .......... .......... .......... 98% 3.45M 0s 259500K .......... .......... .......... .......... .......... 98% 227M 0s 259550K .......... .......... .......... .......... .......... 99% 319M 0s 259600K .......... .......... .......... .......... .......... 99% 118M 0s 259650K .......... .......... .......... .......... .......... 99% 230M 0s 259700K .......... .......... .......... .......... .......... 99% 199M 0s 259750K .......... .......... .......... .......... .......... 99% 147M 0s 259800K .......... .......... .......... .......... .......... 99% 53.8M 0s 259850K .......... .......... .......... .......... .......... 99% 181M 0s 259900K .......... .......... .......... .......... .......... 99% 121M 0s 259950K .......... .......... .......... .......... .......... 99% 2.94M 0s 260000K .......... .......... .......... .......... .......... 99% 193M 0s 260050K .......... .......... .......... .......... .......... 99% 186M 0s 260100K .......... .......... .......... .......... .......... 99% 105M 0s 260150K .......... .......... .......... .......... .......... 99% 82.5M 0s 260200K .......... .......... .......... .......... .......... 99% 98.8M 0s 260250K .......... .......... .......... .......... .......... 99% 125M 0s 260300K .......... .......... .......... .......... .......... 99% 178M 0s 260350K .......... .......... .......... .......... .......... 99% 64.3M 0s 260400K .......... .......... .......... .......... .......... 99% 145M 0s 260450K .......... .......... .......... .......... .......... 99% 2.69M 0s 260500K .......... .......... .......... .......... .......... 99% 130M 0s 260550K .......... .......... .......... .......... .......... 99% 155M 0s 260600K .......... .......... .......... .......... .......... 99% 94.4M 0s 260650K .......... .......... .......... .......... .......... 99% 98.0M 0s 260700K .......... .......... .......... .......... .......... 99% 105M 0s 260750K .......... .......... .......... .......... .......... 99% 181M 0s 260800K .......... .......... .......... .......... .......... 99% 142M 0s 260850K .......... .......... .......... .......... .......... 99% 5.85M 0s 260900K .......... .......... .......... .......... .......... 99% 140M 0s 260950K .......... .......... .......... .......... .......... 99% 2.69M 0s 261000K .......... .......... .......... .......... .......... 99% 119M 0s 261050K .......... .......... .......... .......... .......... 99% 105M 0s 261100K .......... .......... .......... .......... .......... 99% 71.6M 0s 261150K .......... .......... .......... .......... .......... 99% 58.5M 0s 261200K .......... .......... .......... .......... .......... 99% 133M 0s 261250K .......... .......... .......... .......... .......... 99% 52.7M 0s 261300K .......... .......... .......... .......... .......... 99% 206M 0s 261350K .......... .......... .......... .......... .......... 99% 228M 0s 261400K .......... .......... .......... .......... .......... 99% 103M 0s 261450K .......... .......... .......... .......... .......... 99% 3.02M 0s 261500K .......... .......... .......... .......... .......... 99% 144M 0s 261550K .......... .......... .......... .......... .......... 99% 182M 0s 261600K .......... .......... .......... .......... .......... 99% 192M 0s 261650K .......... .......... .......... .......... .......... 99% 214M 0s 261700K .......... .......... .......... .......... .......... 99% 69.9M 0s 261750K .......... .......... .......... .......... .......... 99% 157M 0s 261800K .......... .......... .......... .......... .......... 99% 167M 0s 261850K .......... .......... .......... .......... .......... 99% 31.2M 0s 261900K .......... .......... .......... .......... .......... 99% 67.3M 0s 261950K .......... .......... .......... .......... .......... 99% 6.02M 0s 262000K .......... .......... .......... .......... .......... 99% 164M 0s 262050K .......... .......... .......... .......... .......... 99% 110M 0s 262100K .......... .......... .......... .......... .......... 99% 108M 0s 262150K .......... .......... .......... .......... .......... 99% 171M 0s 262200K ........ 100% 85.6M=16s 2024-05-03 00:35:23 (15.6 MB/s) - ‘ESPbeta.tgz’ saved [268501958/268501958] + tar -xf ESPbeta.tgz + rm -rf EngSketchPad/data/Slugs + python --version Python 3.11.5 + [[ '' == *\.\i\f\o\r\t ]] + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/config/ + ./makeEnv ESP runtime AutoConfigurator CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 with contents: bin include lib share Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad EFCOMP = gfortran CARCH = DARWIN64 CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 CASARCH = . CASREV = 7.8 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/7.8/DARWIN64/EngSketchPad/ESPenv.sh ++ export ESP_ARCH=DARWIN64 ++ ESP_ARCH=DARWIN64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad ++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASARCH=. ++ CASARCH=. ++ export CASREV=7.8 ++ CASREV=7.8 ++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/SLUGS/Slugs.html' ++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/ESP/ESP.html' ++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/ESP/ESP.html' ++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/wvClient/wv.html' ++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/wvClient/wv.html' + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src + make (cd EGADS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/DARWIN64 rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/DARWIN64 cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/DARWIN64 touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads_dot.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads_dot.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.inc rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.inc touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/emp.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/emp.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/prm.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/prm.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.inc rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.inc touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsss.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsss.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTris.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTris.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsGeom.cpp -o ./egadsGeom.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsHLevel.cpp -o ./egadsHLevel.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTopo.cpp -o ./egadsTopo.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsCopy.cpp -o ./egadsCopy.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSpline.cpp -o ./egadsSpline.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsIO.cpp -o ./egadsIO.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSplineFit.cpp -o ./egadsSplineFit.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSkinning.cpp -o ./egadsSkinning.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTessSens.cpp -o ./egadsTessSens.o clang++ -g -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsBase.c -o ./egadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o ./egadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTess.c -o ./egadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTris.c -o ./egadsTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o ./egadsQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsFit.c -o ./egadsFit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o ./egadsRobust.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o ./egadsSBO.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmCfit.c -o ./prmCfit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmGrid.c -o ./prmGrid.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmUV.c -o ./prmUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsExport.c -o ./egadsExport.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o ./egadsEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o ./egadsSolids.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -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=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/evaluate.c -o ./evaluate.o clang++ -g -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=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/rational.c -o ./rational.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \ ../util/regQuads.c -o ./regQuads.o clang++ -g -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=7.8 uvmap/main/uvmap.c -Iuvmap \ -o ./uvmap.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 egadsUVmap.c -Iuvmap \ -o ./egadsUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a clang -g -o ./uvmap.exe ./uvmap.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegads.dylib (cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.8 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadstatic.a (cd .; \ ar rs /Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include fgadsBase.c -o ./fgadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsMemory.c -o ./fgadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsAttrs.c -o ./fgadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTess.c -o ./fgadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsHLevel.c -o ./fgadsHLevel.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsGeom.c -o ./fgadsGeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTopo.c -o ./fgadsTopo.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libfgads.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libfgads.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/libfgads.a touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a *** EGADS Build Complete! *** (cd EGADS/lite; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -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=7.8 -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=7.8 -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=7.8 -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=7.8 -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=7.8 -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=7.8 -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=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o ./liteTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o ./liteTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src \ ../src/egadsQuads.c -o ./liteQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o ./liteTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 ../src/egadsRobust.c \ -o ./egadsRobust.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DDARWIN64 -I../include ../util/emp.c \ -o ./emp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o ./evaLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE ../util/rational.c \ -o ./ratLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I../util \ ../util/regQuads.c -o ./liteRegQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o ./liteEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o ./liteUVmap.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslite.dylib (cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslitestatic.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/DARWIN64/EngSketchPad/include fwv.c -o ./fwv.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a (cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/DARWIN64/EngSketchPad/include -I. -o ./servertest.o clang++ -g -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.dylib (cd .; clang++ -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/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 7.8 \ -current_version 1.0.25 ) (cd EGADS/examples; make -f egads2cart.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include egads2cart.c \ -o ./egads2cart.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm (cd EGADS/examples; make -f vCurvature.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vCurvature.c -o ./vCurvature.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vCurvature ./vCurvature.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd EGADS/examples; make -f vGeom.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vGeom.c -o ./vGeom.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd EGADS/examples; make -f vTess.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vTess.c -o ./vTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include ../util/retessFaces.c \ -o ./retessFaces.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd OpenCSM; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udp.c -o ./udp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. tim.c -o ./tim.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libocsm.dylib clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25 clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bezier.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bezier.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/biconvex.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/biconvex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/box.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/box.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bspline.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bspline.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/catmull.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/catmull.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/compare.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/compare.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createBEM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createBEM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createPoly.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createPoly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/csm.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/csm.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/deform.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/deform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/droop.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/droop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/dumpPmtrs.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/editAttr.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/editAttr.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ellipse.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ellipse.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/eqn2body.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fitcurve.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flend.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flend.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/freeform.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/freeform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ganged.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ganged.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/guide.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/guide.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hex.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/import.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/import.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/kulfan.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/kulfan.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/linalg.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/linalg.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/matchBodys.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mechanism.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mechanism.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca6mc.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nacelle.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nacelle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nurbbody.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nuscale.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nuscale.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/offset.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/offset.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parabaloid.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parsec.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parsec.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pod.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pod.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/poly.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/poly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBbox.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBbox.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBrep.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBrep.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printEgo.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printEgo.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/prop.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/prop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/radwaf.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/radwaf.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sample.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sample.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sew.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sew.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/shadow.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/shadow.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slices.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slices.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stag.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stag.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stiffener.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stiffener.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/supell.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/supell.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester1.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester1.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester2.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vsp3.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vsp3.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/waffle.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/waffle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/warp.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/warp.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/warp.so ./udpWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/PDT2.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/PDT2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/naca456.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm -Wl,-w clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ereped.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ereped.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mitten.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mitten.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plotter.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plotter.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plugs.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slugs.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vspSetup.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/common.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/common.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udp.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udp.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/esp.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/esp.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/tim.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/tim.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egg.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egg.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.c (cd Slugs; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. Fitter.c \ -o ./Fitter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. RedBlackTree.c \ -o ./RedBlackTree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. Tessellate.c \ -o ./Tessellate.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \ ./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads \ -lpthread -lz -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads \ -lpthread -lz -lm (cd CAPS; make) /bin/cp Cart3D/OSX64_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libc3dio.a /bin/cp Cart3D/OSX64_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libCart3D.a /bin/cp Executables/DARWIN64/avl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/avl /bin/cp Executables/DARWIN64/pplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/pplot /bin/cp Executables/DARWIN64/pxplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/pxplot /bin/cp Executables/DARWIN64/xfoil /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/xfoil /bin/cp Executables/DARWIN64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/mastros.exe /bin/cp Executables/DARWIN64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/ASTRO.D01 /bin/cp Executables/DARWIN64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/ASTRO.IDX /bin/cp Executables/DARWIN64/mses /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/mses /bin/cp Executables/DARWIN64/mset /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/mset /bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include /bin/cp udunits/DARWIN64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib /bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libudunits2.dylib /bin/cp Libraries/DARWIN64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/aflr2AIM.so /bin/cp Libraries/DARWIN64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/aflr3AIM.so /bin/cp Libraries/DARWIN64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/aflr4AIM.so (cd CAPS/src; make) touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/caps.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/caps.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsErrors.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsErrors.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsTypes.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsTypes.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimUtil.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimUtil.h touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimMesh.h rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimMesh.h clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o ./aimTransferUtil.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../include \ aimMesh.c -o ./aimMesh.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \ ./aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \ -I/usr/include/udunits2 printObject.c -o ./printObject.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcaps.dylib (cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcapsstatic.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/libcapsstatic.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include testingAIM.c \ -o ./testingAIM.o rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include testingWriter.c \ -o ./testingWriter.o rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include phaseUtil.c \ -o ./phaseUtil.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm (cd ../CAPSexamples; make) (make -C cCAPS -f aeroelastic_SU2.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include avlTest.c -o ./avlTest.o clang -g -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include awaveTest.c -o ./awaveTest.o clang -g -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include frictionTest.c -o ./frictionTest.o clang -g -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o clang -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o clang -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o clang -g -o ./aeroelasticTest ./aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmTest.c -o ./hsmTest.o clang -g -o ./hsmTest ./hsmTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o clang -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o clang -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o clang -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include interferenceTest.c \ -o ./interferenceTest.o clang -g -o ./interferenceTest ./interferenceTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include msesTest.c -o ./msesTest.o clang -g -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include mystranTest.c -o ./mystranTest.o clang -g -o ./mystranTest ./mystranTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o clang -g -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd CAPS/aim; make) /Library/Developer/CommandLineTools/usr/bin/make -C utils clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/libutils.a /Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a(attrUtils.o) has no symbols mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \ abaqusAIM.c -o ./abaqusAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -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/7.8/DARWIN64/EngSketchPad/include -I../utils \ abaqusUtils.c -o ./abaqusUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils astrosAIM.c \ -o ./astrosAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils astrosUtils.c \ -o ./astrosUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils astrosCards.c \ -o ./astrosCards.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/avlAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C awave clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils awaveAIM.c \ -o ./awaveAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \ cart3dAIM.c -o ./cart3dAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \ writeTrix.c -o ./writeTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/c3dio \ -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/libCart3D \ surfTrix.c -o ./surfTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -pedantic -I./xddm -I. \ `xml2-config --cflags` ./xddm/xddm.c \ -o ./xddm.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include bodyTess.c -o ./bodyTess.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \ ./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/ \ -lc3dio -lCart3D -ldl -lxml2 -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include cart3dTest.c \ -o ./cart3dTest.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I./xddm \ -I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \ ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lxml2 -lm /Library/Developer/CommandLineTools/usr/bin/make -C cbaero clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o clang -g -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include egads2cgt.c \ -o ./egads2cgt.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include aflr4egads.c \ -o ./aflr4egads.o clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C custom make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C delaundo clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils delaundoAIM.c \ -o ./delaundoAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/delaundoAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C egadsTess clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils egadsTessAIM.c \ -o ./egadsTessAIM.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/egadsTessAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C friction clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils frictionAIM.c \ -o ./frictionAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \ ./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils hsmAIM.c \ -o src/hsmAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils hsmUtils.c \ -o src/hsmUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 \ -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=7.8 \ -o src/genrcmi.o /Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o /Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o /Library/Developer/CommandLineTools/usr/bin/make -C src cross.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o /Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o /Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o /Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a (cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/libhsm.a touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C interference clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include interferenceAIM.c \ -o ./interferenceAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. cloudFns.c \ -o ./cloudFns.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/interferenceAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/interferenceAIM.so \ ./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C masstran clang++ -g -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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils masstranAIM.cpp \ -o ./masstranAIM.o clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C meshWriter /Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include bstlWriter.c \ -o ./bstlWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include bvtkWriter.c \ -o ./bvtkWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C fastWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include fastWriter.c \ -o ./fastWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include libmeshbWriter.c \ -o ./libmeshbWriter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C stlWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include stlWriter.c \ -o ./stlWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include su2Writer.c \ -o ./su2Writer.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include tecplotWriter.c \ -o ./tecplotWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include ugridWriter.c \ -o ./ugridWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vtkWriter.c \ -o ./vtkWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C mses clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils mystranAIM.c \ -o ./mystranAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils mystranUtils.c \ -o ./mystranUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils nastranAIM.c \ -o ./nastranAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils pointwiseAIM.c \ -o ./pointwiseAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils hashElement.c \ -o ./hashElement.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pointwiseAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -lpthread /Library/Developer/CommandLineTools/usr/bin/make -C refine clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 \ -I../meshWriter/libmeshbWriter/libMeshb/sources \ ../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/refineAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils skeletonAIM.c \ -o ./skeletonAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2Utils.c \ -o ./su2Utils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2_801_Harrier.c \ -o ./su2_801_Harrier.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils tacsAIM.c \ -o ./tacsAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils tetgenAIM.cpp \ -o ./tetgenAIM.o clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \ ./tetgen_Interface.o ./tetgen.o \ ./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tsfoil clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \ tsfoilAIM.c -o ./tsfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \ xfoilAIM.c -o ./xfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C zaero clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl (cd OpenCSM; make -f serveESP.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/capsMode.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/capsMode.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flowchart.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flowchart.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/viewer.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/viewer.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib/pyscript.so rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pyscript.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./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/7.8/DARWIN64/EngSketchPad/data + CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data + cd /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/Verification.sh + bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/Verification.sh + expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set) ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set) ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set) ==> serveESP completed successfully with no verification data real 0m1.114s user 0m0.035s sys 0m0.015s + set +x ============================================= ESP verification case 01 passed (as expected) ============================================= + expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/demo2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/demo2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.239s user 0m0.267s sys 0m0.031s + set +x ============================================= ESP verification case 02 passed (as expected) ============================================= + expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m2.386s user 0m3.445s sys 0m0.641s + set +x ============================================= ESP verification case 03 passed (as expected) ============================================= + expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.517s user 0m0.589s sys 0m0.054s + set +x ============================================= ESP verification case 04 passed (as expected) ============================================= + expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.472s user 0m0.676s sys 0m0.043s + set +x ============================================= ESP verification case 05 passed (as expected) ============================================= + expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m1.466s user 0m0.705s sys 0m0.039s + set +x ============================================= ESP verification case 06 passed (as expected) ============================================= + expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m5.934s user 0m5.363s sys 0m0.439s + set +x ============================================= ESP verification case 07 passed (as expected) ============================================= + expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/CAPS/myPlane + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/CAPS/myPlane WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped ==> serveESP completed successfully with 12 warnings and no verification data real 0m24.035s user 0m39.296s sys 0m1.935s + set +x ============================================= ESP verification case 08 passed (as expected) ============================================= + expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/bottle + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/bottle WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.435s user 0m0.564s sys 0m0.033s + set +x ============================================= ESP verification case 09 passed (as expected) ============================================= + expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/wingMultiModel + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/wingMultiModel WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped ==> serveESP completed successfully with 4 warnings and no verification data real 0m30.045s user 1m9.898s sys 0m14.331s + set +x ============================================= ESP verification case 10 passed (as expected) ============================================= + expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/bullet + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/bullet WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped WARNING:: 8 _hist and/or __trace__ attributes removed WARNING:: 8 _hist and/or __trace__ attributes removed ==> serveESP completed successfully with 1 warnings and no verification data real 0m0.306s user 0m0.229s sys 0m0.033s + set +x ============================================= ESP verification case 11 passed (as expected) ============================================= + expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/connect5 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/connect5 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.423s user 0m0.675s sys 0m0.024s + set +x ============================================= ESP verification case 12 passed (as expected) ============================================= + expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/group2 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/group2 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.130s user 0m0.167s sys 0m0.017s + set +x ============================================= ESP verification case 13 passed (as expected) ============================================= + expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/csm3 + ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/csm3 WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped nnode=8 nedge=12 nface=6 nnode=8 nedge=12 nface=6 nnode=16 nedge=24 nface=10 nnode=8 nedge=12 nface=6 ==> serveESP completed successfully with no verification data real 0m0.370s user 0m0.419s sys 0m0.026s + set +x ============================================= ESP verification case 14 passed (as expected) ============================================= + cd /Users/jenkins/workspace/ESP_Beta/7.8/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 2.049s OK + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/testOCSM + source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/test_pyOCSM.sh ++ set -x ++ python -u test_pyOCSM.py -skipHelp real 0m6.497s user 0m9.019s sys 0m0.297s ++ set +x ================================================= test_pyOCSM.py passed (as expected) ================================================= + cd /Users/jenkins/workspace/ESP_Beta/7.8/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 216.844s OK WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/ + make test python --version Python 3.11.5 python -u -m unittest discover --verbose test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.024 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.068 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.010 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 Number of quad = 0 Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.025 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4122 6020 AFLR2 GG : Nodes, Faces = 5812 9400 AFLR2 GG : Nodes, Faces = 7299 12374 AFLR2 GG : Nodes, Faces = 8574 14924 AFLR2 GG : Nodes, Faces = 9729 17234 AFLR2 GG : Nodes, Faces = 10787 19350 AFLR2 GG : Nodes, Faces = 11767 21310 AFLR2 GG : Nodes, Faces = 12683 23142 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 14278 26332 AFLR2 GG : Nodes, Faces = 14999 27774 AFLR2 GG : Nodes, Faces = 15682 29140 AFLR2 GG : Nodes, Faces = 16312 30400 AFLR2 GG : Nodes, Faces = 16899 31574 AFLR2 GG : Nodes, Faces = 17451 32678 AFLR2 GG : Nodes, Faces = 17959 33694 AFLR2 GG : Nodes, Faces = 18443 34662 AFLR2 GG : Nodes, Faces = 18877 35530 AFLR2 GG : Nodes, Faces = 19283 36342 AFLR2 GG : Nodes, Faces = 19650 37076 AFLR2 GG : Nodes, Faces = 19994 37764 AFLR2 GG : Nodes, Faces = 20325 38426 AFLR2 GG : Nodes, Faces = 20638 39052 AFLR2 GG : Nodes, Faces = 20940 39656 AFLR2 GG : Nodes, Faces = 21240 40256 AFLR2 GG : Nodes, Faces = 21523 40822 AFLR2 GG : Nodes, Faces = 21792 41360 AFLR2 GG : Nodes, Faces = 22053 41882 AFLR2 GG : Nodes, Faces = 22305 42386 AFLR2 GG : Nodes, Faces = 22521 42818 AFLR2 GG : Nodes, Faces = 22696 43168 AFLR2 GG : Nodes, Faces = 22829 43434 AFLR2 GG : Nodes, Faces = 22953 43682 AFLR2 GG : Nodes, Faces = 23050 43876 AFLR2 GG : Nodes, Faces = 23110 43996 AFLR2 GG : Nodes, Faces = 23139 44054 AFLR2 GG : Nodes, Faces = 23157 44090 AFLR2 GG : Nodes, Faces = 23175 44126 AFLR2 GG : Nodes, Faces = 23183 44142 AFLR2 GG : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.064 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.006 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23187 Number of elements = 46374 Number of tris = 44150 Number of quad = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.036 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.085 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.007 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2224 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2224 2224 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 446 894 AFLR2 IG : Nodes, Faces = 892 1786 AFLR2 IG : Nodes, Faces = 918 1838 AFLR2 IG : Nodes, Faces = 1033 2068 AFLR2 IG : Nodes, Faces = 1133 2268 AFLR2 IG : Nodes, Faces = 1233 2468 AFLR2 IG : Nodes, Faces = 1333 2668 AFLR2 IG : Nodes, Faces = 1338 2678 AFLR2 IG : Nodes, Faces = 1433 2868 AFLR2 IG : Nodes, Faces = 1533 3068 AFLR2 IG : Nodes, Faces = 1633 3268 AFLR2 IG : Nodes, Faces = 1733 3468 AFLR2 IG : Nodes, Faces = 1784 3570 AFLR2 IG : Nodes, Faces = 1833 3668 AFLR2 IG : Nodes, Faces = 1858 3718 AFLR2 IG : Nodes, Faces = 2224 4450 AFLR2 IG : Nodes, Faces = 2228 4450 AFLR2 IG : Nodes, Faces = 2224 2224 AFLR2 : CPU Time = 0.027 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2224 2224 AFLR2 GG : Nodes, Faces = 4122 6020 AFLR2 GG : Nodes, Faces = 5812 9400 AFLR2 GG : Nodes, Faces = 7299 12374 AFLR2 GG : Nodes, Faces = 8574 14924 AFLR2 GG : Nodes, Faces = 9729 17234 AFLR2 GG : Nodes, Faces = 10787 19350 AFLR2 GG : Nodes, Faces = 11767 21310 AFLR2 GG : Nodes, Faces = 12683 23142 AFLR2 GG : Nodes, Faces = 13516 24808 AFLR2 GG : Nodes, Faces = 14278 26332 AFLR2 GG : Nodes, Faces = 14999 27774 AFLR2 GG : Nodes, Faces = 15682 29140 AFLR2 GG : Nodes, Faces = 16312 30400 AFLR2 GG : Nodes, Faces = 16899 31574 AFLR2 GG : Nodes, Faces = 17451 32678 AFLR2 GG : Nodes, Faces = 17959 33694 AFLR2 GG : Nodes, Faces = 18443 34662 AFLR2 GG : Nodes, Faces = 18877 35530 AFLR2 GG : Nodes, Faces = 19283 36342 AFLR2 GG : Nodes, Faces = 19650 37076 AFLR2 GG : Nodes, Faces = 19994 37764 AFLR2 GG : Nodes, Faces = 20325 38426 AFLR2 GG : Nodes, Faces = 20638 39052 AFLR2 GG : Nodes, Faces = 20940 39656 AFLR2 GG : Nodes, Faces = 21240 40256 AFLR2 GG : Nodes, Faces = 21523 40822 AFLR2 GG : Nodes, Faces = 21792 41360 AFLR2 GG : Nodes, Faces = 22053 41882 AFLR2 GG : Nodes, Faces = 22305 42386 AFLR2 GG : Nodes, Faces = 22521 42818 AFLR2 GG : Nodes, Faces = 22696 43168 AFLR2 GG : Nodes, Faces = 22829 43434 AFLR2 GG : Nodes, Faces = 22953 43682 AFLR2 GG : Nodes, Faces = 23050 43876 AFLR2 GG : Nodes, Faces = 23110 43996 AFLR2 GG : Nodes, Faces = 23139 44054 AFLR2 GG : Nodes, Faces = 23157 44090 AFLR2 GG : Nodes, Faces = 23175 44126 AFLR2 GG : Nodes, Faces = 23183 44142 AFLR2 GG : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.066 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.005 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 23187 Number of elements = 46374 Number of tris = 44150 Number of quad = 0 CAPS Info: Hit last success -- going live! Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 ok test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 2244 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 2244 2244 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 450 902 AFLR2 IG : Nodes, Faces = 900 1802 AFLR2 IG : Nodes, Faces = 1145 2292 AFLR2 IG : Nodes, Faces = 1260 2522 AFLR2 IG : Nodes, Faces = 1350 2702 AFLR2 IG : Nodes, Faces = 1360 2722 AFLR2 IG : Nodes, Faces = 1460 2922 AFLR2 IG : Nodes, Faces = 1560 3122 AFLR2 IG : Nodes, Faces = 1660 3322 AFLR2 IG : Nodes, Faces = 1760 3522 AFLR2 IG : Nodes, Faces = 1800 3602 AFLR2 IG : Nodes, Faces = 1860 3722 AFLR2 IG : Nodes, Faces = 1960 3922 AFLR2 IG : Nodes, Faces = 2060 4122 AFLR2 IG : Nodes, Faces = 2085 4172 AFLR2 IG : Nodes, Faces = 2244 4490 AFLR2 IG : Nodes, Faces = 2248 4490 AFLR2 IG : Nodes, Faces = 2244 2244 AFLR2 : CPU Time = 0.023 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 2244 2244 AFLR2 GG : Nodes, Faces = 4283 6322 AFLR2 GG : Nodes, Faces = 6128 10012 AFLR2 GG : Nodes, Faces = 7863 13482 AFLR2 GG : Nodes, Faces = 9464 16684 AFLR2 GG : Nodes, Faces = 10948 19652 AFLR2 GG : Nodes, Faces = 12322 22400 AFLR2 GG : Nodes, Faces = 13619 24994 AFLR2 GG : Nodes, Faces = 14829 27414 AFLR2 GG : Nodes, Faces = 15981 29718 AFLR2 GG : Nodes, Faces = 17082 31920 AFLR2 GG : Nodes, Faces = 18110 33976 AFLR2 GG : Nodes, Faces = 19081 35918 AFLR2 GG : Nodes, Faces = 20014 37784 AFLR2 GG : Nodes, Faces = 20924 39604 AFLR2 GG : Nodes, Faces = 21782 41320 AFLR2 GG : Nodes, Faces = 22595 42946 AFLR2 GG : Nodes, Faces = 23377 44510 AFLR2 GG : Nodes, Faces = 24129 46014 AFLR2 GG : Nodes, Faces = 24840 47436 AFLR2 GG : Nodes, Faces = 25522 48800 AFLR2 GG : Nodes, Faces = 26170 50096 AFLR2 GG : Nodes, Faces = 26793 51342 AFLR2 GG : Nodes, Faces = 27346 52448 AFLR2 GG : Nodes, Faces = 27846 53448 AFLR2 GG : Nodes, Faces = 28280 54316 AFLR2 GG : Nodes, Faces = 28652 55060 AFLR2 GG : Nodes, Faces = 28920 55596 AFLR2 GG : Nodes, Faces = 29143 56042 AFLR2 GG : Nodes, Faces = 29358 56472 AFLR2 GG : Nodes, Faces = 29550 56856 AFLR2 GG : Nodes, Faces = 29693 57142 AFLR2 GG : Nodes, Faces = 29805 57366 AFLR2 GG : Nodes, Faces = 29875 57506 AFLR2 GG : Nodes, Faces = 29895 57546 AFLR2 GG : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.093 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.009 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 29897 Number of elements = 59794 Number of tris = 57550 Number of quad = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 48 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 10 22 AFLR2 IG : Nodes, Faces = 20 42 AFLR2 IG : Nodes, Faces = 30 62 AFLR2 IG : Nodes, Faces = 40 82 AFLR2 IG : Nodes, Faces = 45 92 AFLR2 IG : Nodes, Faces = 46 94 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 98 AFLR2 IG : Nodes, Faces = 48 48 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 48 48 AFLR2 GG : Nodes, Faces = 88 128 AFLR2 GG : Nodes, Faces = 109 170 AFLR2 GG : Nodes, Faces = 124 200 AFLR2 GG : Nodes, Faces = 136 224 AFLR2 GG : Nodes, Faces = 148 248 AFLR2 GG : Nodes, Faces = 161 274 AFLR2 GG : Nodes, Faces = 171 294 AFLR2 GG : Nodes, Faces = 181 314 AFLR2 GG : Nodes, Faces = 187 326 AFLR2 GG : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 190 332 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 190 Number of elements = 380 Number of tris = 332 Number of quad = 0 ok test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 344 344 AFLR2 GG : Nodes, Faces = 679 1014 AFLR2 GG : Nodes, Faces = 1006 1668 AFLR2 GG : Nodes, Faces = 1321 2298 AFLR2 GG : Nodes, Faces = 1604 2864 AFLR2 GG : Nodes, Faces = 1886 3428 AFLR2 GG : Nodes, Faces = 2155 3966 AFLR2 GG : Nodes, Faces = 2409 4474 AFLR2 GG : Nodes, Faces = 2649 4954 AFLR2 GG : Nodes, Faces = 2867 5390 AFLR2 GG : Nodes, Faces = 3063 5782 AFLR2 GG : Nodes, Faces = 3243 6142 AFLR2 GG : Nodes, Faces = 3400 6456 AFLR2 GG : Nodes, Faces = 3540 6736 AFLR2 GG : Nodes, Faces = 3665 6986 AFLR2 GG : Nodes, Faces = 3786 7228 AFLR2 GG : Nodes, Faces = 3900 7456 AFLR2 GG : Nodes, Faces = 4010 7676 AFLR2 GG : Nodes, Faces = 4114 7884 AFLR2 GG : Nodes, Faces = 4209 8074 AFLR2 GG : Nodes, Faces = 4292 8240 AFLR2 GG : Nodes, Faces = 4368 8392 AFLR2 GG : Nodes, Faces = 4439 8534 AFLR2 GG : Nodes, Faces = 4503 8662 AFLR2 GG : Nodes, Faces = 4560 8776 AFLR2 GG : Nodes, Faces = 4611 8878 AFLR2 GG : Nodes, Faces = 4650 8956 AFLR2 GG : Nodes, Faces = 4677 9010 AFLR2 GG : Nodes, Faces = 4695 9046 AFLR2 GG : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.011 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.002 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4705 Number of elements = 9410 Number of tris = 9066 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing FAST file .... Finished writing FAST file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.010 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.009 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 339 680 AFLR2 IG : Nodes, Faces = 340 682 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 682 1020 AFLR2 GGp: Nodes, Faces = 1010 1676 AFLR2 GGp: Nodes, Faces = 1316 2288 AFLR2 GGp: Nodes, Faces = 1592 2840 AFLR2 GGp: Nodes, Faces = 1855 3366 AFLR2 GGp: Nodes, Faces = 2106 3868 AFLR2 GGp: Nodes, Faces = 2341 4338 AFLR2 GGp: Nodes, Faces = 2551 4758 AFLR2 GGp: Nodes, Faces = 2741 5138 AFLR2 GGp: Nodes, Faces = 2917 5490 AFLR2 GGp: Nodes, Faces = 3082 5820 AFLR2 GGp: Nodes, Faces = 3240 6136 AFLR2 GGp: Nodes, Faces = 3379 6414 AFLR2 GGp: Nodes, Faces = 3513 6682 AFLR2 GGp: Nodes, Faces = 3642 6940 AFLR2 GGp: Nodes, Faces = 3748 7152 AFLR2 GGp: Nodes, Faces = 3846 7348 AFLR2 GGp: Nodes, Faces = 3931 7518 AFLR2 GGp: Nodes, Faces = 3999 7654 AFLR2 GGp: Nodes, Faces = 4044 7744 AFLR2 GGp: Nodes, Faces = 4058 7772 AFLR2 : CPU Time = 0.015 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4058 7772 AFLR2 QI : Nodes, Faces = 4057 364 AFLR2 QI : Nodes, Faces = 4057 3703 AFLR2 QI : Nodes, Faces = 4057 7770 AFLR2 QI : Nodes, Faces = 4056 344 AFLR2 QI : Nodes, Faces = 4056 3712 AFLR2 QI : Nodes, Faces = 4056 7768 AFLR2 QI : Nodes, Faces = 4055 348 AFLR2 QI : Nodes, Faces = 4055 3709 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 392 AFLR2 QI : Nodes, Faces = 4055 3687 AFLR2 QI : Nodes, Faces = 4055 7766 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 QI : Nodes, Faces = 4055 386 AFLR2 QI : Nodes, Faces = 4055 3690 AFLR2 : CPU Time = 0.008 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Tecplot file .... Finished writing Tecplot file ok test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 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 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 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 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 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 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 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 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 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 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 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 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 10474 Number of elements = 58678 Number of triangles = 6352 Number of quadrilatarals = 0 Number of tetrahedrals = 52326 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 88507 Number of elements = 497504 Number of triangles = 51750 Number of quadrilatarals = 0 Number of tetrahedrals = 445754 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16456 Number of elements = 93635 Number of triangles = 7926 Number of quadrilatarals = 0 Number of tetrahedrals = 85709 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2589 Number of elements = 13809 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11051 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3654 Number of elements = 19800 Number of triangles = 3394 Number of quadrilatarals = 0 Number of tetrahedrals = 16406 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5456 Number of elements = 30308 Number of triangles = 3656 Number of quadrilatarals = 0 Number of tetrahedrals = 26652 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4694 Number of elements = 25935 Number of triangles = 3326 Number of quadrilatarals = 0 Number of tetrahedrals = 22609 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5554 Number of elements = 30862 Number of triangles = 3756 Number of quadrilatarals = 0 Number of tetrahedrals = 27106 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2260 Number of elements = 12133 Number of triangles = 2222 Number of quadrilatarals = 0 Number of tetrahedrals = 9911 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2392 Number of elements = 12577 Number of triangles = 2666 Number of quadrilatarals = 0 Number of tetrahedrals = 9911 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3341 Number of elements = 18069 Number of triangles = 3110 Number of quadrilatarals = 0 Number of tetrahedrals = 14959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 3606 Number of elements = 18961 Number of triangles = 4002 Number of quadrilatarals = 0 Number of tetrahedrals = 14959 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4414 Number of elements = 23974 Number of triangles = 3998 Number of quadrilatarals = 0 Number of tetrahedrals = 19976 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 4) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4811 Number of elements = 25310 Number of triangles = 5334 Number of quadrilatarals = 0 Number of tetrahedrals = 19976 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 4): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 4): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 4): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 4) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 4): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5490 Number of elements = 29891 Number of triangles = 4886 Number of quadrilatarals = 0 Number of tetrahedrals = 25005 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6019 Number of elements = 31671 Number of triangles = 6666 Number of quadrilatarals = 0 Number of tetrahedrals = 25005 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6542 Number of elements = 35667 Number of triangles = 5774 Number of quadrilatarals = 0 Number of tetrahedrals = 29893 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 6) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7203 Number of elements = 37891 Number of triangles = 7998 Number of quadrilatarals = 0 Number of tetrahedrals = 29893 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 6): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 6): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 6): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 6): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 6): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 6) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 6): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 7601 Number of elements = 41489 Number of triangles = 6662 Number of quadrilatarals = 0 Number of tetrahedrals = 34827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 7) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8394 Number of elements = 44157 Number of triangles = 9330 Number of quadrilatarals = 0 Number of tetrahedrals = 34827 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 7): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 7): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 7): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 7): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 7): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 7): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 7): Number of nodes = 1191 Number of elements = 6266 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4934 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 19800 Number of elements = 109798 Number of triangles = 15540 Number of quadrilatarals = 0 Number of tetrahedrals = 94258 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 6 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 7 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 8 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 9 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 10 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 11 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 12 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 13 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 14 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 15 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 16 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 17 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 18 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 19 (of 19) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 22741 Number of elements = 119570 Number of triangles = 25312 Number of quadrilatarals = 0 Number of tetrahedrals = 94258 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 19): Number of nodes = 1208 Number of elements = 6360 Number of triangles = 1334 Number of quadrilatarals = 0 Number of tetrahedrals = 5026 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 19): Number of nodes = 1184 Number of elements = 6217 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4885 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 19): Number of nodes = 1214 Number of elements = 6384 Number of triangles = 1336 Number of quadrilatarals = 0 Number of tetrahedrals = 5048 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 19): Number of nodes = 1205 Number of elements = 6349 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5017 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 19): Number of nodes = 1208 Number of elements = 6361 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5029 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 6 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 6 (of 19): Number of nodes = 1184 Number of elements = 6220 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4888 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 7 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 7 (of 19): Number of nodes = 1191 Number of elements = 6266 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4934 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 8 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 8 (of 19): Number of nodes = 1193 Number of elements = 6272 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4940 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 9 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 9 (of 19): Number of nodes = 1176 Number of elements = 6165 Number of triangles = 1330 Number of quadrilatarals = 0 Number of tetrahedrals = 4835 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 10 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 10 (of 19): Number of nodes = 1203 Number of elements = 6314 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4982 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 11 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 11 (of 19): Number of nodes = 1192 Number of elements = 6269 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4937 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 12 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 12 (of 19): Number of nodes = 1192 Number of elements = 6269 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4937 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 13 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 13 (of 19): Number of nodes = 1198 Number of elements = 6296 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4964 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 14 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 14 (of 19): Number of nodes = 1223 Number of elements = 6443 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 5111 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 15 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 15 (of 19): Number of nodes = 1184 Number of elements = 6224 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4892 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 16 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 16 (of 19): Number of nodes = 1195 Number of elements = 6287 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4955 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 17 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 17 (of 19): Number of nodes = 1197 Number of elements = 6311 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4979 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 18 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 18 (of 19): Number of nodes = 1203 Number of elements = 6310 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4978 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 19 (of 19) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 19 (of 19): Number of nodes = 1191 Number of elements = 6253 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4921 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8857 Number of elements = 49191 Number of triangles = 6284 Number of quadrilatarals = 0 Number of tetrahedrals = 42907 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 8989 Number of elements = 49635 Number of triangles = 6728 Number of quadrilatarals = 0 Number of tetrahedrals = 42907 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 7796 Number of elements = 43368 Number of triangles = 5396 Number of quadrilatarals = 0 Number of tetrahedrals = 37972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 1193 Number of elements = 6267 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4935 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9944 Number of elements = 55193 Number of triangles = 7174 Number of quadrilatarals = 0 Number of tetrahedrals = 48019 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10218 Number of elements = 56081 Number of triangles = 8062 Number of quadrilatarals = 0 Number of tetrahedrals = 48019 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7818 Number of elements = 43469 Number of triangles = 5398 Number of quadrilatarals = 0 Number of tetrahedrals = 38071 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1202 Number of elements = 6320 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4988 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 1198 Number of elements = 6292 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4960 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9609 Number of elements = 53228 Number of triangles = 6994 Number of quadrilatarals = 0 Number of tetrahedrals = 46234 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9829 Number of elements = 53956 Number of triangles = 7722 Number of quadrilatarals = 0 Number of tetrahedrals = 46234 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7789 Number of elements = 43295 Number of triangles = 5394 Number of quadrilatarals = 0 Number of tetrahedrals = 37901 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1186 Number of elements = 6230 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4898 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 854 Number of elements = 4431 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3435 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9348 Number of elements = 51734 Number of triangles = 6812 Number of quadrilatarals = 0 Number of tetrahedrals = 44922 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9531 Number of elements = 52330 Number of triangles = 7408 Number of quadrilatarals = 0 Number of tetrahedrals = 44922 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7804 Number of elements = 43358 Number of triangles = 5386 Number of quadrilatarals = 0 Number of tetrahedrals = 37972 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 1200 Number of elements = 6311 Number of triangles = 1332 Number of quadrilatarals = 0 Number of tetrahedrals = 4979 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2661 Number of triangles = 690 Number of quadrilatarals = 0 Number of tetrahedrals = 1971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9183 Number of elements = 50871 Number of triangles = 6632 Number of quadrilatarals = 0 Number of tetrahedrals = 44239 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 9322 Number of elements = 51307 Number of triangles = 7068 Number of quadrilatarals = 0 Number of tetrahedrals = 44239 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7927 Number of elements = 44116 Number of triangles = 5382 Number of quadrilatarals = 0 Number of tetrahedrals = 38734 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 868 Number of elements = 4530 Number of triangles = 996 Number of quadrilatarals = 0 Number of tetrahedrals = 3534 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 527 Number of elements = 2661 Number of triangles = 690 Number of quadrilatarals = 0 Number of tetrahedrals = 1971 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10181 Number of elements = 56797 Number of triangles = 6782 Number of quadrilatarals = 0 Number of tetrahedrals = 50015 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 10671 Number of elements = 58561 Number of triangles = 8546 Number of quadrilatarals = 0 Number of tetrahedrals = 50015 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 7741 Number of elements = 43010 Number of triangles = 5362 Number of quadrilatarals = 0 Number of tetrahedrals = 37648 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 2692 Number of elements = 14435 Number of triangles = 2800 Number of quadrilatarals = 0 Number of tetrahedrals = 11635 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 238 Number of elements = 1116 Number of triangles = 384 Number of quadrilatarals = 0 Number of tetrahedrals = 732 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1500 Number of elements = 7757 Number of triangles = 1986 Number of quadrilatarals = 0 Number of tetrahedrals = 5771 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 3) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1564 Number of elements = 7881 Number of triangles = 2110 Number of quadrilatarals = 0 Number of tetrahedrals = 5771 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 3): Number of nodes = 1160 Number of elements = 6087 Number of triangles = 1308 Number of quadrilatarals = 0 Number of tetrahedrals = 4779 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 3): Number of nodes = 360 Number of elements = 1635 Number of triangles = 718 Number of quadrilatarals = 0 Number of tetrahedrals = 917 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 3): Number of nodes = 44 Number of elements = 159 Number of triangles = 84 Number of quadrilatarals = 0 Number of tetrahedrals = 75 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5075 Number of elements = 27761 Number of triangles = 4072 Number of quadrilatarals = 0 Number of tetrahedrals = 23689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 5221 Number of elements = 28313 Number of triangles = 4624 Number of quadrilatarals = 0 Number of tetrahedrals = 23689 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 4882 Number of elements = 26790 Number of triangles = 4040 Number of quadrilatarals = 0 Number of tetrahedrals = 22750 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 339 Number of elements = 1523 Number of triangles = 584 Number of quadrilatarals = 0 Number of tetrahedrals = 939 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 32776 Number of elements = 189806 Number of triangles = 8496 Number of quadrilatarals = 0 Number of tetrahedrals = 181310 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 3 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 4 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 5 (of 5) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 36115 Number of elements = 203130 Number of triangles = 21820 Number of quadrilatarals = 0 Number of tetrahedrals = 181310 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 5): Number of nodes = 28584 Number of elements = 162362 Number of triangles = 15158 Number of quadrilatarals = 0 Number of tetrahedrals = 147204 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 5): Number of nodes = 1425 Number of elements = 7592 Number of triangles = 1456 Number of quadrilatarals = 0 Number of tetrahedrals = 6136 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 3 (of 5): Number of nodes = 4138 Number of elements = 22901 Number of triangles = 2938 Number of quadrilatarals = 0 Number of tetrahedrals = 19963 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 4 (of 5): Number of nodes = 711 Number of elements = 3685 Number of triangles = 844 Number of quadrilatarals = 0 Number of tetrahedrals = 2841 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 5 (of 5): Number of nodes = 1257 Number of elements = 6590 Number of triangles = 1424 Number of quadrilatarals = 0 Number of tetrahedrals = 5166 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 16639 Number of elements = 94369 Number of triangles = 8800 Number of quadrilatarals = 0 Number of tetrahedrals = 85569 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Getting volume mesh for body 2 (of 2) EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 18563 Number of elements = 101745 Number of triangles = 16176 Number of quadrilatarals = 0 Number of tetrahedrals = 85569 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 1 (of 2): Number of nodes = 12009 Number of elements = 67436 Number of triangles = 7140 Number of quadrilatarals = 0 Number of tetrahedrals = 60296 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 6554 Number of elements = 34309 Number of triangles = 9036 Number of quadrilatarals = 0 Number of tetrahedrals = 25273 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2865 Number of elements = 12676 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7224 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2477 Number of elements = 10753 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6201 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 4989 Number of elements = 27641 Number of triangles = 3462 Number of quadrilatarals = 0 Number of tetrahedrals = 24179 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 6401 Number of elements = 35742 Number of triangles = 4048 Number of quadrilatarals = 0 Number of tetrahedrals = 31694 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 59702 Number of elements = 348382 Number of triangles = 12928 Number of quadrilatarals = 0 Number of tetrahedrals = 335454 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 58332 Number of elements = 339688 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 327260 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Getting mesh sizing parameters Mesh sizing name - Wake Done getting mesh sizing parameters Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 59702 Number of elements = 347882 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 335454 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required ok test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - trailingEdge Done getting mesh sizing parameters ok test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 44 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 3 Surface 2: Number of points found for aero-spline = 6 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 8 automatic connections were made for capsConnect Rib_Root (node id 1) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! ok test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL ok test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing mass properties file: caps.mass Parsing MassProp ok test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing ok test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. ok test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - VTail1 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - VTail2 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Writing surface - VTail1 (ID = 0) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - VTail2 (ID = 1) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Writing surface - Wing (ID = 2) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 ok test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control RightAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control LeftAileron not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Elevator not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Warning: Control Rudder not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice control surface data VLM control surface name - Elevator VLM control surface name - LeftAileron VLM control surface name - RightAileron VLM control surface name - Rudder Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Control surface 1 of 1 Section 2 of 4 (ID = 2) Control surface 1 of 1 Section 3 of 4 (ID = 1) Control surface 1 of 1 Section 4 of 4 (ID = 0) Control surface 1 of 1 Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Control surface 1 of 1 Section 2 of 3 (ID = 1) Control surface 1 of 1 Section 3 of 3 (ID = 0) Control surface 1 of 1 Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 ok test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable' test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable' test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable' test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable' test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable' test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Wing1, index = 1 Name = trailingEdge, index = 2 Writing FAST file .... Finished writing FAST file Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero Writing CBAero tagged regions - TaggedRegions Writing CBAero setup file - cbaero_CAPS.stp ok test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters ok test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 119815E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 119815E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7000097A8000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7000097A8000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 7000097A8000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7000097A8000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 119815E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 119815E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 7000097A8000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7000097A8000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 119815E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 119815E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_box (test_egadsTess.TestEGADS.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_egadsTess.TestEGADS.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 119815E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 119815E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 119815E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 119815E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) ok test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = nodeBody, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_setInput (test_egadsTess.TestEGADS.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.31633 Creating surface mesh ... Surface mesh seconds: 0.059252 Recovering boundaries... Boundary recovery seconds: 0.166465 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.087443 Recovering Delaunayness... Delaunay recovery seconds: 0.103857 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: 4.30188 Smoothing vertices... Mesh smoothing seconds: 4.03921 Improving mesh... Mesh improvement seconds: 0.088464 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.034445 Total running seconds: 9.19838 Statistics: Input points: 14233 Input facets: 28454 Input segments: 42681 Input holes: 2 Input regions: 0 Mesh points: 33078 Mesh tetrahedra: 159812 Mesh faces: 333851 Mesh faces on exterior boundary: 28454 Mesh faces on input facets: 28454 Mesh edges on input segments: 42681 Steiner points inside domain: 18845 Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 5 Design Variable name - Mach Warning: No initial value set for Mach Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. ok test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 6 Design Variable name - Alpha Design Variable name - Beta Warning: No initial value set for Beta Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Overwrite_NML is set to 'True' - a new namelist will be created Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Reading rubber.data Getting CFD design variables....... Number of design variables - 1 Design Variable name - Alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Creating FUN3D directory tree DesignVariable = Alpha Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Overwrite_NML is set to 'True' - a new namelist will be created Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Reading rubber.data ok test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 6 Design Variable name - Alpha Design Variable name - Beta Warning: No initial value set for Beta Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Getting CFD functional....... Number of design variables - 2 Objective name - Composite Objective name - Lift^2 Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing rubber.data Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Projecting tessellation 1 (of 3) on to new body Projecting tessellation 2 (of 3) on to new body Projecting tessellation 3 (of 3) on to new body Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data Projecting tessellation 1 (of 3) on to new body Projecting tessellation 2 (of 3) on to new body Projecting tessellation 3 (of 3) on to new body Python library was linked, but will not be used! Creating FUN3D directory tree DesignVariable = Alpha DesignVariable = Beta DesignVariable = area DesignVariable = aspect DesignVariable = taper DesignVariable = twist Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1 Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1 Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1 Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Reading rubber.data ok test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7820 Number of elements = 15636 Number of triangle elements = 15636 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 524 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14233 Total number of elements = 28454 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.310115 Creating surface mesh ... Surface mesh seconds: 0.062177 Recovering boundaries... Boundary recovery seconds: 0.180809 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.098428 Recovering Delaunayness... Delaunay recovery seconds: 0.112951 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: 4.35204 Smoothing vertices... Mesh smoothing seconds: 3.9482 Improving mesh... Mesh improvement seconds: 0.082207 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.032255 Total running seconds: 9.18034 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/7.8/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/7.8/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/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. ok test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions Boundary condition name - Wing1 ok test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X ok test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 5079, elements - 10146 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 5079, elements - 10146 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables Python library was linked, but will not be used! Creating FUN3D directory tree Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 4 Design Variable name - area Design Variable name - aspect Design Variable name - taper Design Variable name - twist Done getting CFD design variables CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! ok test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Writing moving_body.input ok test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14233, elements - 28454 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. ok test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. ok test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Projecting tessellation 1 (of 1) on to new body Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1692 Number of elements = 3380 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 3380 Elemental Quad4 = 0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - box2 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2402 Number of elements = 2400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Design_Variable_Relation name - thick_box2 Number of design variable relations - 4 Done getting FEA design variables ok test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 Combined Elemental Quad4 = 0 Updating mesh element types based on properties input EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4009 Number of elements = 8014 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 8014 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6178 Combined Number of elements = 12347 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12346 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input CAPS Info: Hit last success -- going live! Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 4332 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 4332 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 4000 Number of elements = 7996 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 7996 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 2 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 6169 Combined Number of elements = 12329 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 12328 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input ok test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 3 Done getting FEA design variables ok test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - point Done getting FEA properties Updating mesh element types based on properties input Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 7 Design_Variable name - H Design_Variable name - L Design_Variable name - W Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> L Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> W Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> H Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input ===> x0 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = point, index = 2 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 441 Number of elements = 400 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 400 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 442 Combined Number of elements = 401 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 400 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> x1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m0 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ===> m1 Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables Updating mesh element types based on properties input Getting FEA design variables....... Number of design variables - 4 Design_Variable name - m0 Design_Variable name - m1 Design_Variable name - x0 Design_Variable name - x1 Design_Variable_Relation name - mass_point Design_Variable_Relation name - rho_madeupium Name madeupium not found in attribute map!!!! Design_Variable_Relation name - rho_unobtainium Name unobtainium not found in attribute map!!!! Design_Variable_Relation name - thick_box1 Number of design variable relations - 4 Done getting FEA design variables ok test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... Getting CFD design variables....... Number of design variables - 4 Design Variable name - alowervar Design Variable name - auppervar Design Variable name - classvar Design Variable name - ztailvar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - avar Done getting CFD design variables CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 CAPS Info: Sensitivity FD step 1.000000e-05 ok test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... Getting CFD design variables....... Number of design variables - 2 Design Variable name - camber Design Variable name - thick Done getting CFD design variables ok test_journal (test_mses.TestMSES_NACA.test_journal) ... Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables CAPS Info: Hit last success -- going live! Getting CFD design variables....... Number of design variables - 1 Design Variable name - thick Done getting CFD design variables ok test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable' test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable' test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable' test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable' test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable' test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable' test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable' test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable' test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable' test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable' EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 54 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 54 54 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 12 26 AFLR2 IG : Nodes, Faces = 24 50 AFLR2 IG : Nodes, Faces = 36 74 AFLR2 IG : Nodes, Faces = 48 98 AFLR2 IG : Nodes, Faces = 52 106 AFLR2 IG : Nodes, Faces = 53 108 AFLR2 IG : Nodes, Faces = 54 110 AFLR2 IG : Nodes, Faces = 58 110 AFLR2 IG : Nodes, Faces = 54 54 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GG : Nodes, Faces = 54 54 AFLR2 GG : Nodes, Faces = 100 146 AFLR2 GG : Nodes, Faces = 122 190 AFLR2 GG : Nodes, Faces = 138 222 AFLR2 GG : Nodes, Faces = 153 252 AFLR2 GG : Nodes, Faces = 168 282 AFLR2 GG : Nodes, Faces = 180 306 AFLR2 GG : Nodes, Faces = 192 330 AFLR2 GG : Nodes, Faces = 201 348 AFLR2 GG : Nodes, Faces = 210 366 AFLR2 GG : Nodes, Faces = 216 378 AFLR2 GG : Nodes, Faces = 221 388 AFLR2 GG : Nodes, Faces = 224 394 AFLR2 GG : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.002 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 225 396 AFLR2 : CPU Time = 0.000 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 225 Number of elements = 450 Number of tris = 396 Number of quad = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file ok test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1602 Number of elements = 8758 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7518 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 2600 Number of elements = 13864 Number of triangles = 2758 Number of quadrilatarals = 0 Number of tetrahedrals = 11106 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = boxhole, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1071 Number of elements = 5705 Number of triangles = 998 Number of quadrilatarals = 0 Number of tetrahedrals = 4707 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 15544 Number of elements = 89331 Number of triangles = 4632 Number of quadrilatarals = 0 Number of tetrahedrals = 84699 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = farfield, index = 1 Name = box, index = 2 Name = sphere, index = 3 Name = boxhole, index = 4 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 1602 Number of elements = 8758 Number of triangles = 1240 Number of quadrilatarals = 0 Number of tetrahedrals = 7518 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_refine.TestREFINE.test_inputs) ... ok test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 438 Number of elements = 2179 Number of triangles = 644 Number of quadrilatarals = 0 Number of tetrahedrals = 1535 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = box, index = 2 ok test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = farfield, index = 1 Name = sphere, index = 2 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 936 Number of elements = 4999 Number of triangles = 758 Number of quadrilatarals = 0 Number of tetrahedrals = 4241 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 ok test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 3 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 8 Faces EGADS : Body 0 has 15 Edges EGADS : Body 0 has 8 Loops EGADS : Body 0 has 9 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 8 Faces EGADS : Body 1 has 15 Edges EGADS : Body 1 has 8 Loops EGADS : Body 1 has 9 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 2 Faces EGADS : Body 2 has 6 Edges EGADS : Body 2 has 2 Loops EGADS : Body 2 has 2 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 1 1 2 3 4 5 EGADS : 2 Yes 0 0 1 1 1 1 3 4 6 EGADS : 3 Yes 0 0 1 1 1 1 2 4 7 EGADS : 4 Yes 0 0 1 1 1 1 2 3 EGADS : 5 Yes 0 0 1 1 1 1 6 7 8 EGADS : 6 Yes 0 0 1 1 1 2 5 7 8 EGADS : 7 Yes 0 0 1 1 1 3 5 6 8 EGADS : 8 Yes 0 0 1 1 1 5 6 7 EGADS : 9 Yes 1 0 1 0 10 10 11 12 13 EGADS : 10 Yes 1 0 1 0 10 9 11 12 14 EGADS : 11 Yes 1 0 1 0 10 9 10 12 15 EGADS : 12 Yes 1 0 1 0 10 9 10 11 EGADS : 13 Yes 1 0 1 0 10 9 14 15 16 EGADS : 14 Yes 1 0 1 0 10 10 13 15 16 EGADS : 15 Yes 1 0 1 0 10 11 13 14 16 EGADS : 16 Yes 1 0 1 0 10 13 14 15 EGADS : 17 Yes 2 0 1 NA NA 18 EGADS : 18 Yes 2 0 1 NA NA 17 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 4 -3 -2 EGADS : 2 3 7 -6 -5 EGADS : 3 6 9 -1 -8 EGADS : 4 -4 -9 -7 EGADS : 5 -10 2 11 -12 EGADS : 6 -11 5 13 -14 EGADS : 7 -13 8 10 -15 EGADS : 8 12 14 15 EGADS : 9 16 19 -18 -17 EGADS : 10 18 22 -21 -20 EGADS : 11 21 24 -16 -23 EGADS : 12 -19 -24 -22 EGADS : 13 -25 17 26 -27 EGADS : 14 -26 20 28 -29 EGADS : 15 -28 23 25 -30 EGADS : 16 27 29 30 EGADS : 17 -31 -32 33 34 EGADS : 18 -35 -34 36 32 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 4 -3 -2 EGADS : 2 Yes 3 7 -6 -5 EGADS : 3 Yes 6 9 -1 -8 EGADS : 4 Yes -4 -9 -7 EGADS : 5 Yes -10 2 11 -12 EGADS : 6 Yes -11 5 13 -14 EGADS : 7 Yes -13 8 10 -15 EGADS : 8 Yes 12 14 15 EGADS : 9 Yes 16 19 -18 -17 EGADS : 10 Yes 18 22 -21 -20 EGADS : 11 Yes 21 24 -16 -23 EGADS : 12 Yes -19 -24 -22 EGADS : 13 Yes -25 17 26 -27 EGADS : 14 Yes -26 20 28 -29 EGADS : 15 Yes -28 23 25 -30 EGADS : 16 Yes 27 29 30 EGADS : 17 Yes -31 -32 33 34 EGADS : 18 Yes -35 -34 36 32 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 2 1 1 3 EGADS : 2 0 Yes 1 3 1 1 5 EGADS : 3 0 Yes 3 4 1 1 2 EGADS : 4 0 Yes 2 4 1 1 4 EGADS : 5 0 Yes 3 5 1 2 6 EGADS : 6 0 Yes 5 6 1 2 3 EGADS : 7 0 Yes 4 6 1 2 4 EGADS : 8 0 Yes 5 1 1 3 7 EGADS : 9 0 Yes 6 2 1 3 4 EGADS : 10 0 Yes 1 7 1 5 7 EGADS : 11 0 Yes 3 8 1 5 6 EGADS : 12 0 Yes 7 8 1 5 8 EGADS : 13 0 Yes 5 9 1 6 7 EGADS : 14 0 Yes 8 9 1 6 8 EGADS : 15 0 Yes 9 7 1 7 8 EGADS : 16 1 Yes 10 11 1 9 11 EGADS : 17 1 Yes 10 12 1 9 13 EGADS : 18 1 Yes 12 13 1 9 10 EGADS : 19 1 Yes 11 13 1 9 12 EGADS : 20 1 Yes 12 14 1 10 14 EGADS : 21 1 Yes 14 15 1 10 11 EGADS : 22 1 Yes 13 15 1 10 12 EGADS : 23 1 Yes 14 10 1 11 15 EGADS : 24 1 Yes 15 11 1 11 12 EGADS : 25 1 Yes 10 16 1 13 15 EGADS : 26 1 Yes 12 17 1 13 14 EGADS : 27 1 Yes 16 17 1 13 16 EGADS : 28 1 Yes 14 18 1 14 15 EGADS : 29 1 Yes 17 18 1 14 16 EGADS : 30 1 Yes 18 16 1 15 16 EGADS : 31 2 DEGEN 19 19 - 17 EGADS : 32 2 Yes 20 19 NA 17 18 EGADS : 33 2 DEGEN 20 20 - 17 EGADS : 34 2 Yes 20 19 NA 17 18 EGADS : 35 2 DEGEN 19 19 - 18 EGADS : 36 2 DEGEN 20 20 - 18 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 3.77246052 0 0.00459131419 EGADS : 2 Yes 5.90487498 7.07106781 0 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 4.0824829 7.07106781 0.123425948 EGADS : 5 Yes 3.77001182 0 0 EGADS : 6 Yes 5.90282524 7.07106781 0 EGADS : 7 Yes 5.90487498 0 0 EGADS : 8 Yes 4.0824829 0 0.123425948 EGADS : 9 Yes 5.90282524 0 0 EGADS : 10 Yes 11.5089842 0 0.00183652568 EGADS : 11 Yes 12.36195 2.82842712 0 EGADS : 12 Yes 10 0 0 EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791 EGADS : 14 Yes 11.5080047 0 0 EGADS : 15 Yes 12.3611301 2.82842712 0 EGADS : 16 Yes 12.36195 0 0 EGADS : 17 Yes 11.6329932 0 0.0493703791 EGADS : 18 Yes 12.3611301 0 0 EGADS : 19 Yes 0 0 80 EGADS : 20 Yes 0 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 160 AFLR4 : Min Bounding Box Length = 160 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 0.890888 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 15.6122 AFLR4 : Abs Min Surf Spacing = 0.00222722 AFLR4 : Min Surf Spacing = 0.00445444 AFLR4 : Max Surf Spacing = 0.0890888 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD AFLR4 : 2 CAD geometry 0 STD AFLR4 : 3 CAD geometry 0 STD AFLR4 : 4 CAD geometry 0 STD AFLR4 : 5 CAD geometry 0 STD AFLR4 : 6 CAD geometry 0 STD AFLR4 : 7 CAD geometry 0 STD AFLR4 : 8 CAD geometry 0 STD AFLR4 : 9 CAD geometry 0 STD AFLR4 : 10 CAD geometry 0 STD AFLR4 : 11 CAD geometry 0 STD AFLR4 : 12 CAD geometry 0 STD AFLR4 : 13 CAD geometry 0 STD AFLR4 : 14 CAD geometry 0 STD AFLR4 : 15 CAD geometry 0 STD AFLR4 : 16 CAD geometry 0 STD AFLR4 : 17 CAD geometry 0 FARFIELD AFLR4 : 18 CAD geometry 0 FARFIELD AFLR4 : Case has 2 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8 AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR43 : INPUT SURFACE MESH FROM TESS AFLR43 : Quad Surface Faces= 0 AFLR43 : Tria Surface Faces= 12428 AFLR43 : Nodes = 6220 UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR UG PARAM : mrecm = 3 UG PARAM : mrecqm = 3 UG PARAM : mpfrmt = 0 AFLR3 : --------------------------------------- AFLR3 : AFLR3 LIBRARY AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR3 : TETRAHEDRAL GRID GENERATOR AFLR3 : Version Number 16.32.50 AFLR3 : Version Date 10/31/23 @ 06:31PM AFLR3 : Compile OS Darwin 22.6.0 x86_64 AFLR3 : Compile Date 11/01/23 @ 12:19PM AFLR3 : Copyright 1994-2021, D.L. Marcum AFLR3 : --------------------------------------- AFLR3 IC : INPUT SURFACE GRID CHECK AFLR3 IC : Nodes, Elements = 6220 0 UG3 : Boundary Conditions UG3 : B-Face ID Boundary Condition UG3 : 1 Solid UG3 : 2 Solid UG3 : 3 Solid UG3 : 4 Solid UG3 : 5 Solid UG3 : 6 Solid UG3 : 7 Solid UG3 : 8 Solid UG3 : 9 Solid UG3 : 10 Solid UG3 : 11 Solid UG3 : 12 Solid UG3 : 13 Solid UG3 : 14 Solid UG3 : 15 Solid UG3 : 16 Solid UG3 : 17 FarField UG3 : 18 FarField AFLR3 : CPU Time = 0.022 seconds AFLR3 IG : INITIAL VOLUME GRID GENERATION AFLR3 IG : Nodes, Elements = 6220 0 AFLR3 IG : Nodes, Elements = 8 10 AFLR3 IG : Nodes, Elements = 1246 7333 AFLR3 IG : Nodes, Elements = 2492 16261 AFLR3 IG : Nodes, Elements = 3738 25021 AFLR3 IG : Nodes, Elements = 4984 34304 AFLR3 IG : Nodes, Elements = 6227 43518 AFLR3 IG : Nodes, Elements = 6227 43440 AFLR3 IG : Nodes, Elements = 6227 43474 AFLR3 IG : Nodes, Elements = 6227 43437 AFLR3 IG : Nodes, Elements = 6220 26107 AFLR3 IG : Nodes, Elements = 6220 26133 AFLR3 IG : Nodes, Elements = 6220 21538 AFLR3 IG : Nodes, Elements = 6220 19141 AFLR3 : CPU Time = 0.204 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 6220 19141 AFLR3 GG : Nodes, Elements = 9092 27970 AFLR3 GG : Nodes, Elements = 9092 39349 AFLR3 GG : Nodes, Elements = 9092 36380 AFLR3 GG : Nodes, Elements = 9092 34923 AFLR3 GG : Nodes, Elements = 11659 42981 AFLR3 GG : Nodes, Elements = 11659 53807 AFLR3 GG : Nodes, Elements = 11659 50702 AFLR3 GG : Nodes, Elements = 11659 49815 AFLR3 GG : Nodes, Elements = 14477 58553 AFLR3 GG : Nodes, Elements = 14477 70855 AFLR3 GG : Nodes, Elements = 14477 67465 AFLR3 GG : Nodes, Elements = 14477 66533 AFLR3 GG : Nodes, Elements = 17443 75634 AFLR3 GG : Nodes, Elements = 17443 88707 AFLR3 GG : Nodes, Elements = 17443 85026 AFLR3 GG : Nodes, Elements = 17443 84166 AFLR3 GG : Nodes, Elements = 20625 93912 AFLR3 GG : Nodes, Elements = 20625 107483 AFLR3 GG : Nodes, Elements = 20625 103837 AFLR3 GG : Nodes, Elements = 20625 103014 AFLR3 GG : Nodes, Elements = 23983 113245 AFLR3 GG : Nodes, Elements = 23983 127691 AFLR3 GG : Nodes, Elements = 23983 123762 AFLR3 GG : Nodes, Elements = 23983 122939 AFLR3 GG : Nodes, Elements = 27471 133562 AFLR3 GG : Nodes, Elements = 27471 148246 AFLR3 GG : Nodes, Elements = 27471 144367 AFLR3 GG : Nodes, Elements = 27471 143483 AFLR3 GG : Nodes, Elements = 31049 154330 AFLR3 GG : Nodes, Elements = 31049 169629 AFLR3 GG : Nodes, Elements = 31049 165573 AFLR3 GG : Nodes, Elements = 31049 164719 AFLR3 GG : Nodes, Elements = 34642 175591 AFLR3 GG : Nodes, Elements = 34642 190772 AFLR3 GG : Nodes, Elements = 34642 186857 AFLR3 GG : Nodes, Elements = 34642 186049 AFLR3 GG : Nodes, Elements = 38204 196811 AFLR3 GG : Nodes, Elements = 38204 211769 AFLR3 GG : Nodes, Elements = 38204 208011 AFLR3 GG : Nodes, Elements = 38204 207203 AFLR3 GG : Nodes, Elements = 41735 217867 AFLR3 GG : Nodes, Elements = 41735 232734 AFLR3 GG : Nodes, Elements = 41735 228893 AFLR3 GG : Nodes, Elements = 41735 228199 AFLR3 GG : Nodes, Elements = 45118 238407 AFLR3 GG : Nodes, Elements = 45118 252771 AFLR3 GG : Nodes, Elements = 45118 249083 AFLR3 GG : Nodes, Elements = 45118 248399 AFLR3 GG : Nodes, Elements = 48432 258383 AFLR3 GG : Nodes, Elements = 48432 272398 AFLR3 GG : Nodes, Elements = 48432 268767 AFLR3 GG : Nodes, Elements = 48432 268040 AFLR3 GG : Nodes, Elements = 51632 277673 AFLR3 GG : Nodes, Elements = 51632 291124 AFLR3 GG : Nodes, Elements = 51632 287737 AFLR3 GG : Nodes, Elements = 51632 287138 AFLR3 GG : Nodes, Elements = 54742 296489 AFLR3 GG : Nodes, Elements = 54742 309545 AFLR3 GG : Nodes, Elements = 54742 306294 AFLR3 GG : Nodes, Elements = 54742 305700 AFLR3 GG : Nodes, Elements = 57753 314750 AFLR3 GG : Nodes, Elements = 57753 327393 AFLR3 GG : Nodes, Elements = 57753 324205 AFLR3 GG : Nodes, Elements = 57753 323671 AFLR3 GG : Nodes, Elements = 60589 332185 AFLR3 GG : Nodes, Elements = 60589 344195 AFLR3 GG : Nodes, Elements = 60589 341132 AFLR3 GG : Nodes, Elements = 60589 340678 AFLR3 GG : Nodes, Elements = 63303 348823 AFLR3 GG : Nodes, Elements = 63303 360078 AFLR3 GG : Nodes, Elements = 63303 357259 AFLR3 GG : Nodes, Elements = 63303 356861 AFLR3 GG : Nodes, Elements = 65821 364418 AFLR3 GG : Nodes, Elements = 65821 375019 AFLR3 GG : Nodes, Elements = 65821 372315 AFLR3 GG : Nodes, Elements = 65821 371973 AFLR3 GG : Nodes, Elements = 68056 378682 AFLR3 GG : Nodes, Elements = 68056 387933 AFLR3 GG : Nodes, Elements = 68056 385584 AFLR3 GG : Nodes, Elements = 68056 385301 AFLR3 GG : Nodes, Elements = 69951 390988 AFLR3 GG : Nodes, Elements = 69951 398948 AFLR3 GG : Nodes, Elements = 69951 396934 AFLR3 GG : Nodes, Elements = 69951 396704 AFLR3 GG : Nodes, Elements = 71446 401190 AFLR3 GG : Nodes, Elements = 71446 407532 AFLR3 GG : Nodes, Elements = 71446 405836 AFLR3 GG : Nodes, Elements = 71446 405665 AFLR3 GG : Nodes, Elements = 72588 409091 AFLR3 GG : Nodes, Elements = 72588 414051 AFLR3 GG : Nodes, Elements = 72588 412698 AFLR3 GG : Nodes, Elements = 72588 412555 AFLR3 GG : Nodes, Elements = 73412 415028 AFLR3 GG : Nodes, Elements = 73412 418465 AFLR3 GG : Nodes, Elements = 73412 417560 AFLR3 GG : Nodes, Elements = 73412 417491 AFLR3 GG : Nodes, Elements = 73970 419165 AFLR3 GG : Nodes, Elements = 73970 421515 AFLR3 GG : Nodes, Elements = 73970 420850 AFLR3 GG : Nodes, Elements = 73970 420801 AFLR3 GG : Nodes, Elements = 74329 421878 AFLR3 GG : Nodes, Elements = 74329 423409 AFLR3 GG : Nodes, Elements = 74329 422967 AFLR3 GG : Nodes, Elements = 74329 422934 AFLR3 GG : Nodes, Elements = 74527 423528 AFLR3 GG : Nodes, Elements = 74527 424406 AFLR3 GG : Nodes, Elements = 74527 424145 AFLR3 GG : Nodes, Elements = 74527 424123 AFLR3 GG : Nodes, Elements = 74619 424399 AFLR3 GG : Nodes, Elements = 74619 424805 AFLR3 GG : Nodes, Elements = 74619 424686 AFLR3 GG : Nodes, Elements = 74619 424681 AFLR3 GG : Nodes, Elements = 74657 424795 AFLR3 GG : Nodes, Elements = 74657 424951 AFLR3 GG : Nodes, Elements = 74657 424897 AFLR3 GG : Nodes, Elements = 74672 424942 AFLR3 GG : Nodes, Elements = 74672 425006 AFLR3 GG : Nodes, Elements = 74672 424985 AFLR3 GG : Nodes, Elements = 74672 424986 AFLR3 GG : Nodes, Elements = 74673 424989 AFLR3 GG : Nodes, Elements = 74673 424992 AFLR3 GG : Nodes, Elements = 74673 424991 AFLR3 GG : Nodes, Elements = 74696 425060 AFLR3 GG : Nodes, Elements = 74696 425133 AFLR3 GG : Nodes, Elements = 74696 425114 AFLR3 GG : Nodes, Elements = 74696 425117 AFLR3 GG : Nodes, Elements = 74700 425129 AFLR3 GG : Nodes, Elements = 74700 425145 AFLR3 GG : Nodes, Elements = 74700 425140 AFLR3 GG : Nodes, Elements = 74702 425146 AFLR3 GG : Nodes, Elements = 74702 425155 AFLR3 GG : Nodes, Elements = 74702 425152 AFLR3 GG : Nodes, Elements = 74702 425150 AFLR3 : CPU Time = 7.217 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 74702 425150 AFLR3 QI : Nodes, Elements = 73200 416638 AFLR3 QI : Nodes, Elements = 72976 415359 AFLR3 QI : Nodes, Elements = 72961 415273 AFLR3 QI : Nodes, Elements = 72960 415266 AFLR3 QI : Nodes, Elements = 72960 419161 AFLR3 QI : Nodes, Elements = 72960 415035 AFLR3 QI : Nodes, Elements = 72960 414621 AFLR3 QI : Nodes, Elements = 72960 415001 AFLR3 QI : Nodes, Elements = 72960 414373 AFLR3 QI : Nodes, Elements = 72960 414178 AFLR3 QI : Nodes, Elements = 72960 414472 AFLR3 QI : Nodes, Elements = 72960 414145 AFLR3 QI : Nodes, Elements = 72960 414045 AFLR3 QI : Nodes, Elements = 72960 414288 AFLR3 QI : Nodes, Elements = 72960 414039 AFLR3 QI : Nodes, Elements = 72960 413980 AFLR3 QI : Nodes, Elements = 72960 414224 AFLR3 QI : Nodes, Elements = 72960 413989 AFLR3 QI : Nodes, Elements = 72960 413938 AFLR3 QI : Nodes, Elements = 72966 413964 AFLR3 QI : Nodes, Elements = 72966 414196 AFLR3 QI : Nodes, Elements = 72966 413985 AFLR3 QI : Nodes, Elements = 72966 413966 AFLR3 QI : Nodes, Elements = 72966 414195 AFLR3 QI : Nodes, Elements = 72966 413976 AFLR3 QI : Nodes, Elements = 72966 413935 AFLR3 : CPU Time = 2.368 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 72966 413935 AFLR3 QRG: Nodes, Elements = 72978 413998 AFLR3 QRG: Nodes, Elements = 72988 414052 AFLR3 QRG: Nodes, Elements = 72990 414061 AFLR3 QRG: Nodes, Elements = 72991 414065 AFLR3 QRG: Nodes, Elements = 72990 414059 AFLR3 QRG: Nodes, Elements = 72998 414101 AFLR3 QRG: Nodes, Elements = 72998 414099 AFLR3 QRG: Nodes, Elements = 73000 414112 AFLR3 QRG: Nodes, Elements = 73007 414152 AFLR3 : CPU Time = 0.077 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 414152 UG3 : Min, Max Ang = 1.137 170.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 61 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 414152 UG3 : Min Vol = 6.36e-10 UG3 : Average Vol = 5.12 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : No. Tet Elems = 414152 UG3 : Min, Max Q = 0.0734 1 UG3 : Average Q = 0.894 UG3 : No. Q< 0.1 = 29 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 10.507 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 414152 UG3 : Min, Max Ang = 1.137 170.9 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 61 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 414152 UG3 : Min Vol = 6.36e-10 UG3 : Average Vol = 5.12 UG3 : Total-Tet-Vol = 2.12e+06 UG3 : No. Vol<TOL = 0 UG3 : Q VOL-LENGTH-RATIO CHECK 2/3 2 UG3 : Q = c * Vol / sum( L ) UG3 : 0 <= Q <= 1 UG3 : Note that L includes scaling for BL-aspect=ratio UG3 : No. Tet Elems = 414152 UG3 : Min, Max Q = 0.223 1 UG3 : Average Q = 0.859 UG3 : No. Q< 0.1 = 0 UG3 : No. Q< 0.01 = 0 UG3 : CPU Time = 0.000 seconds EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : CREATE EGADS TESS FROM AFLR3 DATA EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14 EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7 EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29 EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15 EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16 EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32 EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34 EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17 EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18 EGADS : EGADS TESS CREATED EGADS : CHECK TESS FACE NODE MAP EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7 EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15 EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16 EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17 EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18 Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Cardinal" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Raven" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Falcon" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions Boundary condition name - Wing1 ok test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X ok test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2 1 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2 2 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" CAPS Info: Hit last success -- going live! Running SU2 1 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" CAPS Info: Hit last success -- going live! Running SU2 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions ok test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 73007 Number of elements = 426580 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 414152 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " ok test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" ok test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Face 1 TFI quading disabled with attribute .qParams Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Projecting tessellation 1 (of 1) on to new body Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - plateWidth Number of design variable relations - 0 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 1 Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards ok test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61976) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 119815E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7000097A8000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7000097A8000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! 119815E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 294 Number of elements = 584 Number of triangle elements = 584 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 Body 4 (of 7) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 7) Number of nodes = 152 Number of elements = 300 Number of triangle elements = 300 Number of quadrilateral elements = 0 Body 6 (of 7) Number of nodes = 624 Number of elements = 1248 Number of triangle elements = 1248 Number of quadrilateral elements = 0 Body 7 (of 7) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4192 Total number of elements = 8364 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 294, elements - 584 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 488, elements - 972 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 294, elements - 584 Body 3 number of surface: nodes - 488, elements - 972 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 488, elements - 972 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Number of surface: nodes - 4192, elements - 8364 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 374 Number of elements = 744 Number of triangle elements = 744 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 472 Total number of elements = 936 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 374, elements - 744 Body 2 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 386 Number of elements = 768 Number of triangle elements = 768 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 582 Total number of elements = 1152 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 386, elements - 768 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 98, elements - 192 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 351 Number of elements = 698 Number of triangle elements = 698 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 491 Total number of elements = 970 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 351, elements - 698 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 376 Number of elements = 748 Number of triangle elements = 748 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1020 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 376, elements - 748 Body 2 number of surface: nodes - 98, elements - 192 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 42 Number of elements = 80 Number of triangle elements = 80 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 454 Total number of elements = 896 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 42, elements - 80 Body 3 number of surface: nodes - 42, elements - 80 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 370 Number of elements = 736 Number of triangle elements = 736 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 126 Number of elements = 252 Number of triangle elements = 252 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 20 Number of elements = 36 Number of triangle elements = 36 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 516 Total number of elements = 1024 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 370, elements - 736 Body 2 number of surface: nodes - 126, elements - 252 Body 3 number of surface: nodes - 20, elements - 36 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 109 Number of elements = 214 Number of triangle elements = 214 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 48 Number of elements = 96 Number of triangle elements = 96 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 12 Number of elements = 20 Number of triangle elements = 20 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 169 Total number of elements = 330 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 109, elements - 214 Body 2 number of surface: nodes - 48, elements - 96 Body 3 number of surface: nodes - 12, elements - 20 Getting volume mesh for body 1 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 3) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 536 Number of elements = 1072 Number of triangle elements = 1072 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 544 Number of elements = 1084 Number of triangle elements = 1084 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1080 Total number of elements = 2156 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 536, elements - 1072 Body 2 number of surface: nodes - 544, elements - 1084 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 5) Getting surface mesh for body 2 (of 5) Getting surface mesh for body 3 (of 5) Getting surface mesh for body 4 (of 5) Getting surface mesh for body 5 (of 5) Body 1 (of 5) Number of nodes = 1351 Number of elements = 2682 Number of triangle elements = 2682 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 288 Number of elements = 572 Number of triangle elements = 572 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 174 Number of elements = 344 Number of triangle elements = 344 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 26 Number of elements = 48 Number of triangle elements = 48 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 482 Number of elements = 960 Number of triangle elements = 960 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 2321 Total number of elements = 4606 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 174, elements - 344 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1351, elements - 2682 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 174, elements - 344 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 444 Number of elements = 884 Number of triangle elements = 884 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 522 Number of elements = 1044 Number of triangle elements = 1044 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 966 Total number of elements = 1928 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 444, elements - 884 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 444, elements - 884 Body 2 number of surface: nodes - 522, elements - 1044 Getting volume mesh for body 1 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 ok test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7173, elements - 14338 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ok test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9601 Number of elements = 19194 Number of triangle elements = 19194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9601 Total number of elements = 19194 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9601, elements - 19194 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing Binary VTK file .... Finished writing Binary VTK file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing FAST file .... Finished writing FAST file Writing SU2 file .... Finished writing SU2 file Writing Binary STL file .... Finished writing Binary STL file Writing ASCII STL file .... Finished writing ASCII STL file Writing Tecplot file .... Finished writing Tecplot file ok test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ok test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok test_Output (test_zaero.TestZAERO.test_Output) ... ok test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1220 Number of elements = 2680 Number of triangle elements = 2680 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1221 Total number of elements = 2680 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1220 Number of elements = 2680 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 2680 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 1221 Combined Number of elements = 2681 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 2680 Combined Elemental Quad4 = 0 Getting FEA materials....... Number of materials - 1 Material name - madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 6 Property name - Rib_Root Property name - Rib_Root_Point Property name - Ribs Property name - Skin Property name - Spar1 Property name - Spar2 Done getting FEA properties Updating mesh element types based on properties input 'Smart_Restart' is ON Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting vortex lattice control surface data VLM control surface name - CntrlLE VLM control surface name - CntrlTE Done getting vortex lattice control surface data Getting FEA vortex lattice mesh Getting ZAERO UAIC Configurations....... Number of UAIC Configurations - 2 UAIC Configuration: climb, id = 1 - Mach Number : 0.200000 - Reduced Freq: [0.020000, ... , 0.250000] UAIC Configuration: cruise, id = 2 - Mach Number : 0.700000 - Reduced Freq: [0.040000, ... , 0.350000] Getting ZAERO Analysis Subcases....... Number of Analysis Subcases - 2 Analysis Subcase: FlutterCruise, id = 1 - Discipline : flutter - UAIC : cruise Analysis Subcase: Trim, id = 2 - Discipline : Trim - UAIC : climb Getting ZAERO Trim Variables....... Number of Trim Variables - 2 Trim Variable: ANGLEA - Label : ALPHA - Value : free Trim Variable: URDD3 - Label : NZ - Value : 1.0 Updating StaticAeroelastic subcase: Trim - vectorToCG -> [0.345898, 1.652951, -0.041403] - weight -> 476456.149985 - weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523] ok ---------------------------------------------------------------------- Ran 143 tests in 1066.695s OK (skipped=15) + cd /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/ESP_venv/bin/python ================================================= Running.... MINIMAL PyTests ================================================= + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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 0m3.051s user 0m1.386s sys 0m0.960s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'xfoil_PyTest.py test;' xfoil_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u xfoil_PyTest.py -outLevel=0 -noPlotData 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 0m6.481s user 0m5.464s sys 0m0.460s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= ================================================= + echo 'mses_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Cl = 0.37837932402995744 Cd = 0.0077758580442312715 Cm = 0.005262576090327783 real 0m5.712s user 0m4.548s sys 0m0.583s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected) ================================================= ================================================= + echo 'friction_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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 0m2.096s user 0m1.110s sys 0m0.410s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tsfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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 0m1.476s user 0m0.943s sys 0m0.281s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected) ================================================= ================================================= + echo 'delaundo_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt delaundo_PyTest.py test; + python -u delaundo_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Name = AirfoilTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 6 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Name = AirfoilTE, index = 6 Getting mesh sizing parameters Mesh sizing name - Airfoil Mesh sizing name - AirfoilTE Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting edge discretization for body 1 Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping! Swapping z and y coordinates! Writing delaundo control file - delaundo.ctr Writing out *.pts file Reading delaundo mesh file - delaundo_CAPS.mesh Swapping y and z coordinates! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file real 0m2.244s user 0m1.229s sys 0m0.485s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected) ================================================= ================================================= + echo 'egadsTess_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_PyTest.py test; + python -u egadsTess_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Rib_Root_Point, index = 6 Name = Wing, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = LeadingEdge, index = 1 Name = TrailingEdge, index = 2 Getting mesh sizing parameters Mesh sizing name - LeadingEdge Done getting mesh sizing parameters Getting surface mesh for body 1 (of 4) Getting surface mesh for body 2 (of 4) Getting surface mesh for body 3 (of 4) Getting surface mesh for body 4 (of 4) Body 1 (of 4) Number of nodes = 3793 Number of elements = 4001 Number of triangle elements = 0 Number of quadrilateral elements = 4001 Body 2 (of 4) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 3 (of 4) Number of nodes = 76 Number of elements = 55 Number of triangle elements = 0 Number of quadrilateral elements = 55 Body 4 (of 4) Number of nodes = 100 Number of elements = 73 Number of triangle elements = 0 Number of quadrilateral elements = 73 ---------------------------- Total number of nodes = 3970 Total number of elements = 4129 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file real 0m15.692s user 0m20.266s sys 0m2.342s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr2_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr2_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u aflr2_PyTest.py -outLevel=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 mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.002 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 = 0.027 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 = 0.015 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file real 0m2.142s user 0m1.396s sys 0m0.505s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_and_aflr3_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_and_aflr3_PyTest.py test; + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u aflr4_and_aflr3_PyTest.py -outLevel=0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing ugrid file .... Finished writing ugrid file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Getting mesh sizing parameters Mesh sizing name - Wing1 Mesh sizing name - Wing2 Done getting mesh sizing parameters Getting volume mesh AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 x86_64 AFLR4 : Compile Date 04/23/24 @ 11:49AM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh: Number of nodes = 150173 Number of elements = 449915 Number of triangles = 14380 Number of quadrilatarals = 0 Number of tetrahedrals = 214483 Number of pyramids = 425 Number of prisms = 220627 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m25.727s user 0m21.302s sys 0m1.438s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tetgen_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tetgen_PyTest.py test; + python -u tetgen_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 2236 Number of elements = 4468 Number of triangle elements = 4468 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 636 Number of elements = 1268 Number of triangle elements = 1268 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 267 Number of elements = 530 Number of triangle elements = 530 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3139 Total number of elements = 6266 Writing Tecplot file .... Finished writing Tecplot file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 3139, elements - 6266 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.036516 Creating surface mesh ... Surface mesh seconds: 0.00926 Recovering boundaries... Boundary recovery seconds: 0.07797 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.010358 Suppressing Steiner points ... Steiner suppression seconds: 4.1e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.011653 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: 1.12135 Smoothing vertices... Mesh smoothing seconds: 1.14263 Improving mesh... Mesh improvement seconds: 0.020917 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.006212 Total running seconds: 2.43729 Statistics: Input points: 3139 Input facets: 6266 Input segments: 9399 Input holes: 2 Input regions: 0 Mesh points: 7895 Mesh tetrahedra: 38676 Mesh faces: 80485 Mesh faces on exterior boundary: 6266 Mesh faces on input facets: 6266 Mesh edges on input segments: 9399 Steiner points inside domain: 4756 Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file real 0m13.696s user 0m11.325s sys 0m0.815s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_AFLR2_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Saving geometry Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 x86_64 AFLR2 : Compile Date 04/23/24 @ 11:49AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 545 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 545 545 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 110 222 AFLR2 IG : Nodes, Faces = 220 442 AFLR2 IG : Nodes, Faces = 330 662 AFLR2 IG : Nodes, Faces = 440 882 AFLR2 IG : Nodes, Faces = 517 1036 AFLR2 IG : Nodes, Faces = 545 1092 AFLR2 IG : Nodes, Faces = 549 1092 AFLR2 IG : Nodes, Faces = 545 545 AFLR2 : CPU Time = 0.002 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 = 0.048 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 = 0.019 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 11153 Number of elements = 11885 Number of tris = 917 Number of quad = 10423 EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)! EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)! EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Writing SU2 file .... SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Airfoil Boundary condition name - InFlow Boundary condition name - OutFlow Boundary condition name - TunnelWall Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Running SU2...... ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.0 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2023, SU2 Contributors | | | | SU2 is free software; you can redistribute it and/or | | modify it under the terms of the GNU Lesser General Public | | License as published by the Free Software Foundation; either | | version 2.1 of the License, or (at your option) any later version. | | | | SU2 is distributed in the hope that it will be useful, | | but WITHOUT ANY WARRANTY; without even the implied warranty of | | MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU | | Lesser General Public License for more details. | | | | You should have received a copy of the GNU Lesser General Public | | License along with SU2. If not, see <http://www.gnu.org/licenses/>. | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible Euler equations. Mach number: 0.4. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. No restart solution, use the values at infinity (freestream). Dimensional simulation. The reference area is 1 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 1 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: BC_5. Surface(s) plotted in the output file: BC_5, BC_2. Input mesh file name: ../aflr2/aflr2_CAPS.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ Roe (with entropy fix = 0.001) solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Gradient for upwind reconstruction: inverse-distance weighted Least-Squares. Gradient for viscous and source terms: inverse-distance weighted Least-Squares. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 1e-06. Max number of linear iterations: 10. V Multigrid Cycle, with 2 multigrid levels. Damping factor for the residual restriction: 0.75. Damping factor for the correction prolongation: 0.75. No CFL adaptation. +-------------------------------------------+ | MG Level| Presmooth|PostSmooth|CorrectSmo| +-------------------------------------------+ | 0| 1| 0| 0| | 1| 2| 0| 0| | 2| 3| 0| 0| +-------------------------------------------+ Courant-Friedrichs-Lewy number: 10 ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-14. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 250| | SURFACE_CSV| 250| | TECPLOT| 250| | SURFACE_TECPLOT| 250| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat. Surface file name: surface_flow_pyCAPS_su2_aflr2. Volume file name: flow_pyCAPS_su2_aflr2. Restart file name: restart_flow_pyCAPS_su2_aflr2.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Euler wall| BC_5| | | BC_2| +-----------------------------------------------------------------------+ | Inlet boundary| BC_4| +-----------------------------------------------------------------------+ | Outlet boundary| BC_3| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 11153 grid points. 11340 volume elements. 4 surface markers. 98 boundary elements in index 0 (Marker = BC_2). 24 boundary elements in index 1 (Marker = BC_3). 24 boundary elements in index 2 (Marker = BC_4). 399 boundary elements in index 3 (Marker = BC_5). 917 triangles. 10423 quadrilaterals. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 917 TRIANGLE volume elements. There has been a re-orientation of 10423 QUADRILATERAL volume elements. There has been a re-orientation of 73 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 999.878. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 49.3184| 90| | CV Face Area Aspect Ratio| 1.00035| 33.4982| | CV Sub-Volume Ratio| 1.00001| 7.89914| +--------------------------------------------------------------+ Setting the multigrid structure. +-------------------------------------------+ | MG Level| CVs|Aggl. Rate| CFL| +-------------------------------------------+ | 0| 11153| 1/1.00| 10| | 1| 2702| 1/4.13| 7.38309| | 2| 549| 1/4.92| 4.99198| +-------------------------------------------+ Finding max control volume width. Wetted area = 2.06265 m. Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m. Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m. Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker BC_5 is NOT a single straight. Boundary marker BC_2 is NOT a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Inviscid flow: Computing density based on free-stream temperature and pressure using the ideal gas law. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | -| -| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 1| N.m/kg.K| 287.058| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 101325| 1| Pa| 101325| | Density| 1.22498| 1| kg/m^3| 1.22498| | Temperature| 288.15| 1| K| 288.15| | Total Energy| 216054| 1| m^2/s^2| 216054| | Velocity-X| 136.119| 1| m/s| 136.119| | Velocity-Y| 0| 1| m/s| 0| | Velocity Magnitude| 136.119| 1| m/s| 136.119| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 0.4| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Euler). MG level: 0. Initialize Jacobian structure (Euler). MG level: 1. Initialize Jacobian structure (Euler). MG level: 2. ------------------- Numerics Preprocessing ( Zone 0 ) ------------------- ----------------- Integration Preprocessing ( Zone 0 ) ------------------ ------------------- Iteration Preprocessing ( Zone 0 ) ------------------ Euler/Navier-Stokes/RANS fluid iteration. ------------------------------ Begin Solver ----------------------------- Simulation Run using the Single-zone Driver WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better, see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations +----------------------------------------------------------------------------------------------------------------------------------------------+ | Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff| +----------------------------------------------------------------------------------------------------------------------------------------------+ | 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.2004e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.1373e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0647e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.0408e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1536e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.1795e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.1748e-01| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.2346e-01| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.2598e-01| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.2968e-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 0m13.454s user 0m3.524s sys 0m1.092s + 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/7.8/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/7.8/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 0m3.319s user 0m1.205s sys 0m0.581s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'astros_Flutter_15degree.py test;' astros_Flutter_15degree.py test; + python -u astros_Flutter_15degree.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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 0m3.706s user 0m1.582s sys 0m1.005s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected) ================================================= ================================================= + echo 'masstran_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results mass properties..... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1159 Number of elements = 798 Number of triangle elements = 0 Number of quadrilateral elements = 798 ---------------------------- Total number of nodes = 1159 Total number of elements = 798 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = Rib_Constraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1159 Number of elements = 798 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 798 Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - Ribs_and_Spars No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Area 3.428666259747 Mass 5383.006027803 Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11] CG [1.222256036874, 0.1634981473778, -4.234574416087e-11] Ixx 22133.97306033 Iyy 23448.30046709 Izz 1389.213122582 Ixy 164.2055275657 Ixz -7.454849830627e-06 Iyz 1.707682983295e-06 I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06] II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]] real 0m13.830s user 0m14.032s sys 0m4.326s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected) ================================================= ================================================= + echo 'hsm_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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 0m10.935s user 0m1.541s sys 0m0.267s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + echo '../corsairlite/qp.py test;' + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt ../corsairlite/qp.py test; + python -u ../corsairlite/qp.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_Beta/7.8/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 0m40.535s user 0m2.615s sys 0m0.438s + 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/7.8/DARWIN64 + mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/test/plugs + cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/test/plugs + find /Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/DARWIN64/JenkinsESP/data/plugs/plugsFailure.txt + cp /Users/jenkins/workspace/ESP_Beta/7.8/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 51928 -rw-r--r-- 1 jenkins staff 1.2M May 3 00:41 ASTRO.D01 -rw-r--r-- 1 jenkins staff 277K May 3 00:41 ASTRO.IDX -rwxr-xr-x 1 jenkins staff 131K May 3 00:41 ESPxddm -rwxr-xr-x 1 jenkins staff 229K May 3 00:41 Slugs -rwxr-xr-x 1 jenkins staff 102K May 3 00:41 TestFit -rwxr-xr-x 1 jenkins staff 1.8M May 3 00:41 avl -rwxr-xr-x 1 jenkins staff 50K May 3 00:41 cart3dTest -rwxr-xr-x 1 jenkins staff 50K May 3 00:39 egads2cart -rwxr-xr-x 1 jenkins staff 86K May 3 00:41 egads2cgt -rwxr-xr-x 1 jenkins staff 383K May 3 00:41 friction -rwxr-xr-x 1 jenkins staff 8.9M May 3 00:41 mastros.exe -rwxr-xr-x 1 jenkins staff 2.2M May 3 00:41 mses -rwxr-xr-x 1 jenkins staff 2.5M May 3 00:41 mset -rwxr-xr-x 1 jenkins staff 51K May 3 00:41 phaseUtil -rw-r--r-- 1 jenkins staff 1.6K May 3 00:43 pod.egads -rw-r--r-- 1 jenkins staff 0B May 3 00:43 port7681.jrnl -rwxr-xr-x 1 jenkins staff 1.2M May 3 00:41 pplot -rwxr-xr-x 1 jenkins staff 1.2M May 3 00:41 pxplot -rwxr-xr-x 1 jenkins staff 84K May 3 00:40 sensCSM -rwxr-xr-x 1 jenkins staff 224K May 3 00:40 serveCSM -rwxr-xr-x 1 jenkins staff 192K May 3 00:40 serveESP -rwxr-xr-x 1 jenkins staff 68K May 3 00:39 vCurvature -rwxr-xr-x 1 jenkins staff 51K May 3 00:39 vGeom -rwxr-xr-x 1 jenkins staff 52K May 3 00:39 vTess -rwxr-xr-x 1 jenkins staff 2.3M May 3 00:39 vTesstatic -rw-r--r-- 1 jenkins staff 195K May 3 00:43 wingMultiModel.bdf -rwxr-xr-x 1 jenkins staff 1.8M May 3 00:41 xfoil ( 1 / 4 ) data/Plugs/plugs0a.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0 Starting pass 3 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m22.177s user 0m13.330s sys 0m1.184s ++ set +x data/Plugs/plugs0a passed (as expected) -------------------------------------------------------------------------------------------------- ( 2 / 4 ) data/Plugs/plugs0b.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0 Starting pass 5 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m17.269s user 0m19.022s sys 0m0.626s ++ set +x data/Plugs/plugs0b passed (as expected) -------------------------------------------------------------------------------------------------- ( 3 / 4 ) data/Plugs/plugs0c.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0 Starting pass 5 (of 25) of phase2 Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0 Starting pass 6 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m43.276s user 0m53.833s sys 0m0.896s ++ set +x data/Plugs/plugs0c passed (as expected) -------------------------------------------------------------------------------------------------- ( 4 / 4 ) data/Plugs/plugs0d.csm; ++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped =================================== PLUGS with 4562 points in the cloud =================================== PLUGS phase1: match bounding boxes PLUGS phase2: match cloud points Starting pass 1 (of 25) of phase2 Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554 Starting pass 2 (of 25) of phase2 Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0 Starting pass 3 (of 25) of phase2 Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0 Starting pass 4 (of 25) of phase2 Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0 Starting pass 5 (of 25) of phase2 Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0 Starting pass 6 (of 25) of phase2 Phase2 passes converged because points are classified same as previous pass ==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl" ==> Closing input journal file ==> serveCSM completed successfully with no verification data real 0m31.729s user 0m45.905s sys 0m0.699s ++ 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/7.8/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/7.8/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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/7.8/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=7.8,ESP_ARCH=DARWIN64,buildnode=macys_VM #713'. [Checks API] No suitable checks publisher found. [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] done Finished: SUCCESS