![[Jenkins]](/csi/static/a404d988/images/svgs/logo.svg){kind=logo}
The Jenkins Controller is preparing for shutdown. No new builds can be started.
Started by upstream project "ESP_Beta" build number 711 originally caused by: Started by remote host 18.18.33.14 Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on reynolds-ubuntu18 in workspace /home/jenkins/workspace/ESP_Beta/7.8/LINUX64 [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] Done Checking out a fresh workspace because there's no workspace at /home/jenkins/workspace/ESP_Beta/7.8/LINUX64 Cleaning local Directory . Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-04-28T10:16:15.782 -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 2481 Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP doesn't exist Cleaning local Directory JenkinsESP Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-04-28T10:16:15.782 -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 858 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 [reynolds-ubuntu18] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]] Run condition [Execution node ] enabling perform for step [Execute shell] [LINUX64] $ /bin/bash -ex /tmp/jenkins7161882761836569473.sh + bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh + source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Env.sh ++ export OCCTREF=7.6 ++ OCCTREF=7.6 ++ AFLR_VERSION=11.5.14 ++ SU2_VERSION=8.0.0 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.34.0 ++ export PYTHON_VERSION=3.11.9 ++ PYTHON_VERSION=3.11.9 ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ [[ reynolds-ubuntu18 == \r\e\y\n\o\l\d\s ]] ++ [[ LINUX64 == *\.\i\f\o\r\t ]] ++ '[' -f /opt/intel/oneapi/setvars.sh ']' ++ '[' -f /home/jenkins/.bashrc ']' ++ source /home/jenkins/.bashrc +++ case $- in +++ return ++ export CAPS_OUTLEVEL=0 ++ CAPS_OUTLEVEL=0 ++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64 ++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64 ++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64 ++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64 ++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia ++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.6 != '' ]] ++ [[ '' != '' ]] ++ [[ reynolds-ubuntu18 == *\r\e\y\n\o\l\d\s* ]] ++ [[ '' != '' ]] ++ [[ -d /home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ]] ++ export PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ++ PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ++ export PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ++ export EMPnumProc=4 ++ EMPnumProc=4 ++ export OMP_NUM_THREADS=4 ++ OMP_NUM_THREADS=4 ++ '[' '!' -z '' ']' +++ ls -d /home/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASARCH=. ++ CASARCH=. ++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ++ export ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs ++ ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs ++ export AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14 ++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14 ++ export AFLR_ARCH=Linux-x86-64 ++ AFLR_ARCH=Linux-x86-64 ++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ++ CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ++ export CART3D_ARCH=X86_64_ICC ++ CART3D_ARCH=X86_64_ICC ++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries ++ MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries ++ export PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/aim/pointwise/glyph ++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/aim/pointwise/glyph ++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin ++ [[ reynolds-ubuntu18 == \r\e\y\n\o\l\d\s ]] ++ export SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0 ++ SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0 ++ export SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0 ++ export PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ']' ++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ [[ reynolds-ubuntu18 == \m\a\c\y\s* ]] ++ [[ reynolds-ubuntu18 == \v\i\g\g\e\n ]] +++ python-config --includes ++ export 'PYTHONINC=. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' ++ PYTHONINC='. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11' +++ python-config --help ++ [[ Usage: /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/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/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm ' ++ PYTHONLIB=' -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl -lutil -lm ' ++ [[ reynolds-ubuntu18 == \m\a\c\y\s ]] ++ [[ reynolds-ubuntu18 == \v\i\g\g\e\n ]] ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.9 ++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data ++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data + virtualenv /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv created virtual environment CPython3.11.9.final.0-64 in 265ms creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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=/home/jenkins/.local/share/virtualenv) added seed packages: pip==24.0, setuptools==69.2.0, wheel==0.43.0 activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator + . /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate ++ '[' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv ++ '[' linux-gnu = cygwin ']' ++ '[' linux-gnu = msys ']' ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH ++ '[' x '!=' x ']' +++ basename /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv ++ VIRTUAL_ENV_PROMPT=ESP_venv ++ export VIRTUAL_ENV_PROMPT ++ '[' -z _ ']' ++ _OLD_VIRTUAL_PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ++ unset PYTHONHOME ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ PS1='(ESP_venv) ' ++ export PS1 ++ alias pydoc ++ true ++ hash -r + pip_install pip + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy Collecting numpy Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB) Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB) Installing collected packages: numpy Successfully installed numpy-1.26.4 + pip_install openmdao + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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-manylinux_2_17_x86_64.manylinux2014_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-manylinux_2_17_x86_64.manylinux2014_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-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (38.6 MB) Using cached certifi-2024.2.2-py3-none-any.whl (163 kB) Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (140 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 + [[ reynolds-ubuntu18 == *\v\i\g\g\e\n* ]] + pip_install cvxopt + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (1.3 kB) Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (13.6 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 + pip_install dill + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.8.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (5.8 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_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-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_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-manylinux_2_17_x86_64.manylinux2014_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-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (11.6 MB) Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (306 kB) Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB) Using cached fonttools-4.51.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.9 MB) Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (1.4 MB) Using cached pillow-10.3.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.4 MB) Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB) Using cached six-1.16.0-py2.py3-none-any.whl (11 kB) Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.8.4 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0 + pip_install scipy + /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.0) Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4) + unset PYTHONINC + unset PYTHONLIB + unset UDUNITS2_XML_PATH + unset ESP_BLOC + unset ESP_ROOT + unset ESP_ARCH + unset AWAVE + unset AFLR + unset AFLR_ARCH + wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz --2024-04-28 10:17:00-- https://acdl.mit.edu/ESP/archive/ESPbeta.tgz Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14 Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected. HTTP request sent, awaiting response... 200 OK Length: 268483520 (256M) [application/x-gzip] Saving to: ‘ESPbeta.tgz’ 0K .......... .......... .......... .......... .......... 0% 14.8M 17s 50K .......... .......... .......... .......... .......... 0% 13.3M 18s 100K .......... .......... .......... .......... .......... 0% 14.9M 18s 150K .......... .......... .......... .......... .......... 0% 15.8M 17s 200K .......... .......... .......... .......... .......... 0% 11.5M 18s 250K .......... .......... .......... .......... .......... 0% 11.7M 19s 300K .......... .......... .......... .......... .......... 0% 11.4M 19s 350K .......... .......... .......... .......... .......... 0% 12.3M 20s 400K .......... .......... .......... .......... .......... 0% 17.9M 19s 450K .......... .......... .......... .......... .......... 0% 10.8M 20s 500K .......... .......... .......... .......... .......... 0% 18.9M 19s 550K .......... .......... .......... .......... .......... 0% 12.5M 19s 600K .......... .......... .......... .......... .......... 0% 14.8M 19s 650K .......... .......... .......... .......... .......... 0% 16.2M 19s 700K .......... .......... .......... .......... .......... 0% 15.1M 19s 750K .......... .......... .......... .......... .......... 0% 14.2M 19s 800K .......... .......... .......... .......... .......... 0% 16.0M 18s 850K .......... .......... .......... .......... .......... 0% 13.4M 18s 900K .......... .......... .......... .......... .......... 0% 7.80M 19s 950K .......... .......... .......... .......... .......... 0% 14.1M 19s 1000K .......... .......... .......... .......... .......... 0% 11.8M 19s 1050K .......... .......... .......... .......... .......... 0% 14.0M 19s 1100K .......... .......... .......... .......... .......... 0% 9.07M 20s 1150K .......... .......... .......... .......... .......... 0% 12.3M 20s 1200K .......... .......... .......... .......... .......... 0% 28.4M 19s 1250K .......... .......... .......... .......... .......... 0% 12.7M 19s 1300K .......... .......... .......... .......... .......... 0% 21.7M 19s 1350K .......... .......... .......... .......... .......... 0% 11.9M 19s 1400K .......... .......... .......... .......... .......... 0% 23.1M 19s 1450K .......... .......... .......... .......... .......... 0% 22.6M 18s 1500K .......... .......... .......... .......... .......... 0% 21.4M 18s 1550K .......... .......... .......... .......... .......... 0% 22.8M 18s 1600K .......... .......... .......... .......... .......... 0% 21.6M 18s 1650K .......... .......... .......... .......... .......... 0% 23.4M 18s 1700K .......... .......... .......... .......... .......... 0% 12.2M 18s 1750K .......... .......... .......... .......... .......... 0% 64.9M 17s 1800K .......... .......... .......... .......... .......... 0% 28.7M 17s 1850K .......... .......... .......... .......... .......... 0% 21.8M 17s 1900K .......... .......... .......... .......... .......... 0% 26.1M 17s 1950K .......... .......... .......... .......... .......... 0% 22.4M 17s 2000K .......... .......... .......... .......... .......... 0% 24.5M 16s 2050K .......... .......... .......... .......... .......... 0% 27.2M 16s 2100K .......... .......... .......... .......... .......... 0% 19.4M 16s 2150K .......... .......... .......... .......... .......... 0% 23.8M 16s 2200K .......... .......... .......... .......... .......... 0% 24.0M 16s 2250K .......... .......... .......... .......... .......... 0% 22.1M 16s 2300K .......... .......... .......... .......... .......... 0% 15.5M 16s 2350K .......... .......... .......... .......... .......... 0% 17.2M 16s 2400K .......... .......... .......... .......... .......... 0% 15.2M 16s 2450K .......... .......... .......... .......... .......... 0% 16.0M 16s 2500K .......... .......... .......... .......... .......... 0% 9.30M 16s 2550K .......... .......... .......... .......... .......... 0% 12.6M 16s 2600K .......... .......... .......... .......... .......... 1% 55.4M 16s 2650K .......... .......... .......... .......... .......... 1% 11.3M 16s 2700K .......... .......... .......... .......... .......... 1% 7.17M 16s 2750K .......... .......... .......... .......... .......... 1% 70.1M 16s 2800K .......... .......... .......... .......... .......... 1% 16.6M 16s 2850K .......... .......... .......... .......... .......... 1% 24.2M 16s 2900K .......... .......... .......... .......... .......... 1% 37.5M 16s 2950K .......... .......... .......... .......... .......... 1% 10.1M 16s 3000K .......... .......... .......... .......... .......... 1% 17.6M 16s 3050K .......... .......... .......... .......... .......... 1% 17.7M 16s 3100K .......... .......... .......... .......... .......... 1% 14.7M 16s 3150K .......... .......... .......... .......... .......... 1% 14.0M 16s 3200K .......... .......... .......... .......... .......... 1% 8.91M 16s 3250K .......... .......... .......... .......... .......... 1% 17.2M 16s 3300K .......... .......... .......... .......... .......... 1% 19.5M 16s 3350K .......... .......... .......... .......... .......... 1% 21.5M 16s 3400K .......... .......... .......... .......... .......... 1% 20.0M 16s 3450K .......... .......... .......... .......... .......... 1% 26.5M 16s 3500K .......... .......... .......... .......... .......... 1% 21.4M 16s 3550K .......... .......... .......... .......... .......... 1% 20.3M 16s 3600K .......... .......... .......... .......... .......... 1% 19.2M 16s 3650K .......... .......... .......... .......... .......... 1% 30.5M 16s 3700K .......... .......... .......... .......... .......... 1% 19.4M 16s 3750K .......... .......... .......... .......... .......... 1% 26.9M 16s 3800K .......... .......... .......... .......... .......... 1% 18.9M 16s 3850K .......... .......... .......... .......... .......... 1% 18.4M 15s 3900K .......... .......... .......... .......... .......... 1% 26.9M 15s 3950K .......... .......... .......... .......... .......... 1% 35.4M 15s 4000K .......... .......... .......... .......... .......... 1% 30.1M 15s 4050K .......... .......... .......... .......... .......... 1% 23.4M 15s 4100K .......... .......... .......... .......... .......... 1% 21.1M 15s 4150K .......... .......... .......... .......... .......... 1% 18.7M 15s 4200K .......... .......... .......... .......... .......... 1% 20.5M 15s 4250K .......... .......... .......... .......... .......... 1% 18.9M 15s 4300K .......... .......... .......... .......... .......... 1% 14.6M 15s 4350K .......... .......... .......... .......... .......... 1% 23.0M 15s 4400K .......... .......... .......... .......... .......... 1% 27.1M 15s 4450K .......... .......... .......... .......... .......... 1% 14.6M 15s 4500K .......... .......... .......... .......... .......... 1% 31.4M 15s 4550K .......... .......... .......... .......... .......... 1% 20.4M 15s 4600K .......... .......... .......... .......... .......... 1% 17.5M 15s 4650K .......... .......... .......... .......... .......... 1% 17.4M 15s 4700K .......... .......... .......... .......... .......... 1% 16.6M 15s 4750K .......... .......... .......... .......... .......... 1% 12.5M 15s 4800K .......... .......... .......... .......... .......... 1% 18.0M 15s 4850K .......... .......... .......... .......... .......... 1% 14.4M 15s 4900K .......... .......... .......... .......... .......... 1% 23.4M 15s 4950K .......... .......... .......... .......... .......... 1% 17.8M 15s 5000K .......... .......... .......... .......... .......... 1% 25.7M 15s 5050K .......... .......... .......... .......... .......... 1% 19.5M 15s 5100K .......... .......... .......... .......... .......... 1% 19.0M 15s 5150K .......... .......... .......... .......... .......... 1% 24.3M 15s 5200K .......... .......... .......... .......... .......... 2% 15.3M 15s 5250K .......... .......... .......... .......... .......... 2% 25.8M 15s 5300K .......... .......... .......... .......... .......... 2% 23.6M 15s 5350K .......... .......... .......... .......... .......... 2% 19.4M 15s 5400K .......... .......... .......... .......... .......... 2% 21.4M 15s 5450K .......... .......... .......... .......... .......... 2% 16.3M 15s 5500K .......... .......... .......... .......... .......... 2% 19.5M 15s 5550K .......... .......... .......... .......... .......... 2% 26.4M 15s 5600K .......... .......... .......... .......... .......... 2% 20.2M 14s 5650K .......... .......... .......... .......... .......... 2% 16.0M 15s 5700K .......... .......... .......... .......... .......... 2% 13.5M 15s 5750K .......... .......... .......... .......... .......... 2% 11.4M 15s 5800K .......... .......... .......... .......... .......... 2% 12.8M 15s 5850K .......... .......... .......... .......... .......... 2% 11.0M 15s 5900K .......... .......... .......... .......... .......... 2% 13.8M 15s 5950K .......... .......... .......... .......... .......... 2% 11.6M 15s 6000K .......... .......... .......... .......... .......... 2% 9.88M 15s 6050K .......... .......... .......... .......... .......... 2% 11.4M 15s 6100K .......... .......... .......... .......... .......... 2% 10.7M 15s 6150K .......... .......... .......... .......... .......... 2% 11.0M 15s 6200K .......... .......... .......... .......... .......... 2% 8.81M 15s 6250K .......... .......... .......... .......... .......... 2% 17.7M 15s 6300K .......... .......... .......... .......... .......... 2% 9.75M 15s 6350K .......... .......... .......... .......... .......... 2% 11.3M 15s 6400K .......... .......... .......... .......... .......... 2% 18.0M 15s 6450K .......... .......... .......... .......... .......... 2% 12.3M 15s 6500K .......... .......... .......... .......... .......... 2% 14.7M 15s 6550K .......... .......... .......... .......... .......... 2% 20.9M 15s 6600K .......... .......... .......... .......... .......... 2% 19.6M 15s 6650K .......... .......... .......... .......... .......... 2% 22.0M 15s 6700K .......... .......... .......... .......... .......... 2% 13.6M 15s 6750K .......... .......... .......... .......... .......... 2% 16.8M 15s 6800K .......... .......... .......... .......... .......... 2% 39.8M 15s 6850K .......... .......... .......... .......... .......... 2% 22.3M 15s 6900K .......... .......... .......... .......... .......... 2% 19.4M 15s 6950K .......... .......... .......... .......... .......... 2% 17.0M 15s 7000K .......... .......... .......... .......... .......... 2% 17.3M 15s 7050K .......... .......... .......... .......... .......... 2% 18.3M 15s 7100K .......... .......... .......... .......... .......... 2% 13.6M 15s 7150K .......... .......... .......... .......... .......... 2% 12.1M 15s 7200K .......... .......... .......... .......... .......... 2% 8.21M 15s 7250K .......... .......... .......... .......... .......... 2% 7.33M 15s 7300K .......... .......... .......... .......... .......... 2% 9.04M 15s 7350K .......... .......... .......... .......... .......... 2% 9.82M 16s 7400K .......... .......... .......... .......... .......... 2% 12.8M 16s 7450K .......... .......... .......... .......... .......... 2% 10.3M 16s 7500K .......... .......... .......... .......... .......... 2% 10.8M 16s 7550K .......... .......... .......... .......... .......... 2% 13.5M 16s 7600K .......... .......... .......... .......... .......... 2% 25.8M 16s 7650K .......... .......... .......... .......... .......... 2% 26.4M 16s 7700K .......... .......... .......... .......... .......... 2% 41.1M 16s 7750K .......... .......... .......... .......... .......... 2% 41.6M 15s 7800K .......... .......... .......... .......... .......... 2% 51.9M 15s 7850K .......... .......... .......... .......... .......... 3% 20.5M 15s 7900K .......... .......... .......... .......... .......... 3% 61.7M 15s 7950K .......... .......... .......... .......... .......... 3% 22.8M 15s 8000K .......... .......... .......... .......... .......... 3% 20.7M 15s 8050K .......... .......... .......... .......... .......... 3% 22.8M 15s 8100K .......... .......... .......... .......... .......... 3% 23.6M 15s 8150K .......... .......... .......... .......... .......... 3% 18.0M 15s 8200K .......... .......... .......... .......... .......... 3% 24.4M 15s 8250K .......... .......... .......... .......... .......... 3% 13.0M 15s 8300K .......... .......... .......... .......... .......... 3% 52.1M 15s 8350K .......... .......... .......... .......... .......... 3% 13.4M 15s 8400K .......... .......... .......... .......... .......... 3% 17.2M 15s 8450K .......... .......... .......... .......... .......... 3% 13.8M 15s 8500K .......... .......... .......... .......... .......... 3% 14.0M 15s 8550K .......... .......... .......... .......... .......... 3% 14.6M 15s 8600K .......... .......... .......... .......... .......... 3% 9.20M 15s 8650K .......... .......... .......... .......... .......... 3% 10.5M 15s 8700K .......... .......... .......... .......... .......... 3% 12.4M 15s 8750K .......... .......... .......... .......... .......... 3% 15.3M 15s 8800K .......... .......... .......... .......... .......... 3% 14.8M 15s 8850K .......... .......... .......... .......... .......... 3% 12.9M 15s 8900K .......... .......... .......... .......... .......... 3% 14.2M 15s 8950K .......... .......... .......... .......... .......... 3% 14.4M 15s 9000K .......... .......... .......... .......... .......... 3% 18.7M 15s 9050K .......... .......... .......... .......... .......... 3% 19.5M 15s 9100K .......... .......... .......... .......... .......... 3% 11.8M 15s 9150K .......... .......... .......... .......... .......... 3% 14.5M 15s 9200K .......... .......... .......... .......... .......... 3% 13.3M 15s 9250K .......... .......... .......... .......... .......... 3% 18.3M 15s 9300K .......... .......... .......... .......... .......... 3% 21.4M 15s 9350K .......... .......... .......... .......... .......... 3% 12.8M 15s 9400K .......... .......... .......... .......... .......... 3% 14.8M 15s 9450K .......... .......... .......... .......... .......... 3% 9.50M 15s 9500K .......... .......... .......... .......... .......... 3% 33.7M 15s 9550K .......... .......... .......... .......... .......... 3% 18.6M 15s 9600K .......... .......... .......... .......... .......... 3% 12.3M 15s 9650K .......... .......... .......... .......... .......... 3% 19.8M 15s 9700K .......... .......... .......... .......... .......... 3% 15.9M 15s 9750K .......... .......... .......... .......... .......... 3% 17.5M 15s 9800K .......... .......... .......... .......... .......... 3% 10.2M 15s 9850K .......... .......... .......... .......... .......... 3% 18.2M 15s 9900K .......... .......... .......... .......... .......... 3% 13.5M 15s 9950K .......... .......... .......... .......... .......... 3% 11.0M 15s 10000K .......... .......... .......... .......... .......... 3% 16.9M 15s 10050K .......... .......... .......... .......... .......... 3% 16.5M 15s 10100K .......... .......... .......... .......... .......... 3% 16.4M 15s 10150K .......... .......... .......... .......... .......... 3% 19.0M 15s 10200K .......... .......... .......... .......... .......... 3% 17.6M 15s 10250K .......... .......... .......... .......... .......... 3% 18.2M 15s 10300K .......... .......... .......... .......... .......... 3% 18.3M 15s 10350K .......... .......... .......... .......... .......... 3% 12.7M 15s 10400K .......... .......... .......... .......... .......... 3% 16.3M 15s 10450K .......... .......... .......... .......... .......... 4% 11.2M 15s 10500K .......... .......... .......... .......... .......... 4% 16.0M 15s 10550K .......... .......... .......... .......... .......... 4% 16.2M 15s 10600K .......... .......... .......... .......... .......... 4% 14.2M 15s 10650K .......... .......... .......... .......... .......... 4% 18.5M 15s 10700K .......... .......... .......... .......... .......... 4% 10.0M 15s 10750K .......... .......... .......... .......... .......... 4% 10.2M 15s 10800K .......... .......... .......... .......... .......... 4% 9.23M 15s 10850K .......... .......... .......... .......... .......... 4% 6.68M 16s 10900K .......... .......... .......... .......... .......... 4% 11.1M 16s 10950K .......... .......... .......... .......... .......... 4% 12.7M 16s 11000K .......... .......... .......... .......... .......... 4% 12.3M 16s 11050K .......... .......... .......... .......... .......... 4% 20.4M 16s 11100K .......... .......... .......... .......... .......... 4% 12.7M 16s 11150K .......... .......... .......... .......... .......... 4% 12.8M 16s 11200K .......... .......... .......... .......... .......... 4% 10.4M 16s 11250K .......... .......... .......... .......... .......... 4% 13.9M 16s 11300K .......... .......... .......... .......... .......... 4% 15.2M 16s 11350K .......... .......... .......... .......... .......... 4% 12.7M 16s 11400K .......... .......... .......... .......... .......... 4% 13.3M 16s 11450K .......... .......... .......... .......... .......... 4% 8.95M 16s 11500K .......... .......... .......... .......... .......... 4% 11.3M 16s 11550K .......... .......... .......... .......... .......... 4% 8.24M 16s 11600K .......... .......... .......... .......... .......... 4% 8.78M 16s 11650K .......... .......... .......... .......... .......... 4% 12.3M 16s 11700K .......... .......... .......... .......... .......... 4% 10.3M 16s 11750K .......... .......... .......... .......... .......... 4% 7.83M 16s 11800K .......... .......... .......... .......... .......... 4% 10.1M 16s 11850K .......... .......... .......... .......... .......... 4% 7.28M 16s 11900K .......... .......... .......... .......... .......... 4% 8.37M 16s 11950K .......... .......... .......... .......... .......... 4% 8.68M 16s 12000K .......... .......... .......... .......... .......... 4% 8.59M 16s 12050K .......... .......... .......... .......... .......... 4% 7.06M 16s 12100K .......... .......... .......... .......... .......... 4% 9.33M 16s 12150K .......... .......... .......... .......... .......... 4% 8.85M 16s 12200K .......... .......... .......... .......... .......... 4% 7.04M 16s 12250K .......... .......... .......... .......... .......... 4% 10.2M 16s 12300K .......... .......... .......... .......... .......... 4% 9.62M 16s 12350K .......... .......... .......... .......... .......... 4% 8.70M 17s 12400K .......... .......... .......... .......... .......... 4% 6.32M 17s 12450K .......... .......... .......... .......... .......... 4% 5.59M 17s 12500K .......... .......... .......... .......... .......... 4% 8.95M 17s 12550K .......... .......... .......... .......... .......... 4% 11.6M 17s 12600K .......... .......... .......... .......... .......... 4% 6.56M 17s 12650K .......... .......... .......... .......... .......... 4% 5.46M 17s 12700K .......... .......... .......... .......... .......... 4% 6.32M 17s 12750K .......... .......... .......... .......... .......... 4% 12.8M 17s 12800K .......... .......... .......... .......... .......... 4% 13.6M 17s 12850K .......... .......... .......... .......... .......... 4% 22.6M 17s 12900K .......... .......... .......... .......... .......... 4% 34.4M 17s 12950K .......... .......... .......... .......... .......... 4% 21.6M 17s 13000K .......... .......... .......... .......... .......... 4% 31.9M 17s 13050K .......... .......... .......... .......... .......... 4% 17.1M 17s 13100K .......... .......... .......... .......... .......... 5% 16.2M 17s 13150K .......... .......... .......... .......... .......... 5% 12.9M 17s 13200K .......... .......... .......... .......... .......... 5% 43.8M 17s 13250K .......... .......... .......... .......... .......... 5% 20.5M 17s 13300K .......... .......... .......... .......... .......... 5% 13.7M 17s 13350K .......... .......... .......... .......... .......... 5% 14.4M 17s 13400K .......... .......... .......... .......... .......... 5% 13.5M 17s 13450K .......... .......... .......... .......... .......... 5% 17.1M 17s 13500K .......... .......... .......... .......... .......... 5% 19.7M 17s 13550K .......... .......... .......... .......... .......... 5% 16.7M 17s 13600K .......... .......... .......... .......... .......... 5% 18.6M 17s 13650K .......... .......... .......... .......... .......... 5% 24.0M 17s 13700K .......... .......... .......... .......... .......... 5% 3.86M 17s 13750K .......... .......... .......... .......... .......... 5% 8.53M 17s 13800K .......... .......... .......... .......... .......... 5% 21.7M 17s 13850K .......... .......... .......... .......... .......... 5% 128M 17s 13900K .......... .......... .......... .......... .......... 5% 175M 17s 13950K .......... .......... .......... .......... .......... 5% 169M 17s 14000K .......... .......... .......... .......... .......... 5% 80.2M 17s 14050K .......... .......... .......... .......... .......... 5% 11.7M 17s 14100K .......... .......... .......... .......... .......... 5% 7.91M 17s 14150K .......... .......... .......... .......... .......... 5% 17.1M 17s 14200K .......... .......... .......... .......... .......... 5% 9.21M 17s 14250K .......... .......... .......... .......... .......... 5% 12.4M 17s 14300K .......... .......... .......... .......... .......... 5% 15.0M 17s 14350K .......... .......... .......... .......... .......... 5% 12.8M 17s 14400K .......... .......... .......... .......... .......... 5% 14.6M 17s 14450K .......... .......... .......... .......... .......... 5% 11.2M 17s 14500K .......... .......... .......... .......... .......... 5% 13.9M 17s 14550K .......... .......... .......... .......... .......... 5% 13.0M 17s 14600K .......... .......... .......... .......... .......... 5% 10.9M 17s 14650K .......... .......... .......... .......... .......... 5% 17.6M 17s 14700K .......... .......... .......... .......... .......... 5% 14.8M 17s 14750K .......... .......... .......... .......... .......... 5% 20.4M 17s 14800K .......... .......... .......... .......... .......... 5% 19.7M 17s 14850K .......... .......... .......... .......... .......... 5% 16.1M 17s 14900K .......... .......... .......... .......... .......... 5% 22.1M 17s 14950K .......... .......... .......... .......... .......... 5% 20.2M 17s 15000K .......... .......... .......... .......... .......... 5% 18.8M 17s 15050K .......... .......... .......... .......... .......... 5% 18.4M 17s 15100K .......... .......... .......... .......... .......... 5% 10.5M 17s 15150K .......... .......... .......... .......... .......... 5% 14.6M 17s 15200K .......... .......... .......... .......... .......... 5% 9.76M 17s 15250K .......... .......... .......... .......... .......... 5% 12.2M 17s 15300K .......... .......... .......... .......... .......... 5% 12.5M 17s 15350K .......... .......... .......... .......... .......... 5% 11.5M 17s 15400K .......... .......... .......... .......... .......... 5% 13.6M 17s 15450K .......... .......... .......... .......... .......... 5% 8.84M 17s 15500K .......... .......... .......... .......... .......... 5% 8.98M 17s 15550K .......... .......... .......... .......... .......... 5% 232K 20s 15600K .......... .......... .......... .......... .......... 5% 10.7M 20s 15650K .......... .......... .......... .......... .......... 5% 12.9M 20s 15700K .......... .......... .......... .......... .......... 6% 18.0M 20s 15750K .......... .......... .......... .......... .......... 6% 17.3M 20s 15800K .......... .......... .......... .......... .......... 6% 12.7M 20s 15850K .......... .......... .......... .......... .......... 6% 11.1M 20s 15900K .......... .......... .......... .......... .......... 6% 13.1M 20s 15950K .......... .......... .......... .......... .......... 6% 12.4M 20s 16000K .......... .......... .......... .......... .......... 6% 15.0M 20s 16050K .......... .......... .......... .......... .......... 6% 15.4M 20s 16100K .......... .......... .......... .......... .......... 6% 11.6M 20s 16150K .......... .......... .......... .......... .......... 6% 12.5M 20s 16200K .......... .......... .......... .......... .......... 6% 13.4M 20s 16250K .......... .......... .......... .......... .......... 6% 18.3M 20s 16300K .......... .......... .......... .......... .......... 6% 17.6M 20s 16350K .......... .......... .......... .......... .......... 6% 15.0M 20s 16400K .......... .......... .......... .......... .......... 6% 14.7M 20s 16450K .......... .......... .......... .......... .......... 6% 18.8M 20s 16500K .......... .......... .......... .......... .......... 6% 20.4M 20s 16550K .......... .......... .......... .......... .......... 6% 14.9M 20s 16600K .......... .......... .......... .......... .......... 6% 8.37M 20s 16650K .......... .......... .......... .......... .......... 6% 7.40M 20s 16700K .......... .......... .......... .......... .......... 6% 7.42M 20s 16750K .......... .......... .......... .......... .......... 6% 12.3M 20s 16800K .......... .......... .......... .......... .......... 6% 15.9M 20s 16850K .......... .......... .......... .......... .......... 6% 10.2M 20s 16900K .......... .......... .......... .......... .......... 6% 23.1M 20s 16950K .......... .......... .......... .......... .......... 6% 19.8M 20s 17000K .......... .......... .......... .......... .......... 6% 15.5M 20s 17050K .......... .......... .......... .......... .......... 6% 18.2M 20s 17100K .......... .......... .......... .......... .......... 6% 19.0M 20s 17150K .......... .......... .......... .......... .......... 6% 15.6M 20s 17200K .......... .......... .......... .......... .......... 6% 13.1M 20s 17250K .......... .......... .......... .......... .......... 6% 15.1M 20s 17300K .......... .......... .......... .......... .......... 6% 10.8M 20s 17350K .......... .......... .......... .......... .......... 6% 10.9M 20s 17400K .......... .......... .......... .......... .......... 6% 9.14M 20s 17450K .......... .......... .......... .......... .......... 6% 16.0M 20s 17500K .......... .......... .......... .......... .......... 6% 16.3M 20s 17550K .......... .......... .......... .......... .......... 6% 16.3M 20s 17600K .......... .......... .......... .......... .......... 6% 17.5M 20s 17650K .......... .......... .......... .......... .......... 6% 22.6M 20s 17700K .......... .......... .......... .......... .......... 6% 5.49M 20s 17750K .......... .......... .......... .......... .......... 6% 6.65M 20s 17800K .......... .......... .......... .......... .......... 6% 8.80M 20s 17850K .......... .......... .......... .......... .......... 6% 6.59M 20s 17900K .......... .......... .......... .......... .......... 6% 9.81M 20s 17950K .......... .......... .......... .......... .......... 6% 14.1M 20s 18000K .......... .......... .......... .......... .......... 6% 11.3M 20s 18050K .......... .......... .......... .......... .......... 6% 12.9M 20s 18100K .......... .......... .......... .......... .......... 6% 10.7M 20s 18150K .......... .......... .......... .......... .......... 6% 15.2M 20s 18200K .......... .......... .......... .......... .......... 6% 14.2M 20s 18250K .......... .......... .......... .......... .......... 6% 13.5M 20s 18300K .......... .......... .......... .......... .......... 6% 13.8M 20s 18350K .......... .......... .......... .......... .......... 7% 11.5M 20s 18400K .......... .......... .......... .......... .......... 7% 12.0M 20s 18450K .......... .......... .......... .......... .......... 7% 11.8M 20s 18500K .......... .......... .......... .......... .......... 7% 10.1M 20s 18550K .......... .......... .......... .......... .......... 7% 11.8M 20s 18600K .......... .......... .......... .......... .......... 7% 11.5M 20s 18650K .......... .......... .......... .......... .......... 7% 13.0M 20s 18700K .......... .......... .......... .......... .......... 7% 7.88M 20s 18750K .......... .......... .......... .......... .......... 7% 13.2M 20s 18800K .......... .......... .......... .......... .......... 7% 13.5M 20s 18850K .......... .......... .......... .......... .......... 7% 9.51M 20s 18900K .......... .......... .......... .......... .......... 7% 14.6M 20s 18950K .......... .......... .......... .......... .......... 7% 14.2M 20s 19000K .......... .......... .......... .......... .......... 7% 18.2M 20s 19050K .......... .......... .......... .......... .......... 7% 16.3M 20s 19100K .......... .......... .......... .......... .......... 7% 16.4M 20s 19150K .......... .......... .......... .......... .......... 7% 22.0M 20s 19200K .......... .......... .......... .......... .......... 7% 24.5M 20s 19250K .......... .......... .......... .......... .......... 7% 21.1M 20s 19300K .......... .......... .......... .......... .......... 7% 20.1M 20s 19350K .......... .......... .......... .......... .......... 7% 19.5M 20s 19400K .......... .......... .......... .......... .......... 7% 14.1M 20s 19450K .......... .......... .......... .......... .......... 7% 11.9M 20s 19500K .......... .......... .......... .......... .......... 7% 17.2M 20s 19550K .......... .......... .......... .......... .......... 7% 13.8M 20s 19600K .......... .......... .......... .......... .......... 7% 14.4M 19s 19650K .......... .......... .......... .......... .......... 7% 21.4M 19s 19700K .......... .......... .......... .......... .......... 7% 20.7M 19s 19750K .......... .......... .......... .......... .......... 7% 19.8M 19s 19800K .......... .......... .......... .......... .......... 7% 20.2M 19s 19850K .......... .......... .......... .......... .......... 7% 15.7M 19s 19900K .......... .......... .......... .......... .......... 7% 14.4M 19s 19950K .......... .......... .......... .......... .......... 7% 8.97M 19s 20000K .......... .......... .......... .......... .......... 7% 13.2M 19s 20050K .......... .......... .......... .......... .......... 7% 10.9M 19s 20100K .......... .......... .......... .......... .......... 7% 12.9M 19s 20150K .......... .......... .......... .......... .......... 7% 14.7M 19s 20200K .......... .......... .......... .......... .......... 7% 10.5M 19s 20250K .......... .......... .......... .......... .......... 7% 9.54M 19s 20300K .......... .......... .......... .......... .......... 7% 12.9M 19s 20350K .......... .......... .......... .......... .......... 7% 10.6M 19s 20400K .......... .......... .......... .......... .......... 7% 14.1M 19s 20450K .......... .......... .......... .......... .......... 7% 14.6M 19s 20500K .......... .......... .......... .......... .......... 7% 16.0M 19s 20550K .......... .......... .......... .......... .......... 7% 24.3M 19s 20600K .......... .......... .......... .......... .......... 7% 11.6M 19s 20650K .......... .......... .......... .......... .......... 7% 10.1M 19s 20700K .......... .......... .......... .......... .......... 7% 10.7M 19s 20750K .......... .......... .......... .......... .......... 7% 7.19M 19s 20800K .......... .......... .......... .......... .......... 7% 8.72M 19s 20850K .......... .......... .......... .......... .......... 7% 6.25M 19s 20900K .......... .......... .......... .......... .......... 7% 7.57M 19s 20950K .......... .......... .......... .......... .......... 8% 7.83M 19s 21000K .......... .......... .......... .......... .......... 8% 8.62M 19s 21050K .......... .......... .......... .......... .......... 8% 8.98M 19s 21100K .......... .......... .......... .......... .......... 8% 10.5M 19s 21150K .......... .......... .......... .......... .......... 8% 8.53M 19s 21200K .......... .......... .......... .......... .......... 8% 5.58M 20s 21250K .......... .......... .......... .......... .......... 8% 17.2M 20s 21300K .......... .......... .......... .......... .......... 8% 23.3M 19s 21350K .......... .......... .......... .......... .......... 8% 14.9M 19s 21400K .......... .......... .......... .......... .......... 8% 21.8M 19s 21450K .......... .......... .......... .......... .......... 8% 12.4M 19s 21500K .......... .......... .......... .......... .......... 8% 15.7M 19s 21550K .......... .......... .......... .......... .......... 8% 15.8M 19s 21600K .......... .......... .......... .......... .......... 8% 18.9M 19s 21650K .......... .......... .......... .......... .......... 8% 26.2M 19s 21700K .......... .......... .......... .......... .......... 8% 21.8M 19s 21750K .......... .......... .......... .......... .......... 8% 26.4M 19s 21800K .......... .......... .......... .......... .......... 8% 25.9M 19s 21850K .......... .......... .......... .......... .......... 8% 15.1M 19s 21900K .......... .......... .......... .......... .......... 8% 21.7M 19s 21950K .......... .......... .......... .......... .......... 8% 15.5M 19s 22000K .......... .......... .......... .......... .......... 8% 15.9M 19s 22050K .......... .......... .......... .......... .......... 8% 16.4M 19s 22100K .......... .......... .......... .......... .......... 8% 17.6M 19s 22150K .......... .......... .......... .......... .......... 8% 16.1M 19s 22200K .......... .......... .......... .......... .......... 8% 14.4M 19s 22250K .......... .......... .......... .......... .......... 8% 16.1M 19s 22300K .......... .......... .......... .......... .......... 8% 14.3M 19s 22350K .......... .......... .......... .......... .......... 8% 10.7M 19s 22400K .......... .......... .......... .......... .......... 8% 11.6M 19s 22450K .......... .......... .......... .......... .......... 8% 12.9M 19s 22500K .......... .......... .......... .......... .......... 8% 17.8M 19s 22550K .......... .......... .......... .......... .......... 8% 15.4M 19s 22600K .......... .......... .......... .......... .......... 8% 12.2M 19s 22650K .......... .......... .......... .......... .......... 8% 9.53M 19s 22700K .......... .......... .......... .......... .......... 8% 7.04M 19s 22750K .......... .......... .......... .......... .......... 8% 10.1M 19s 22800K .......... .......... .......... .......... .......... 8% 12.0M 19s 22850K .......... .......... .......... .......... .......... 8% 9.93M 19s 22900K .......... .......... .......... .......... .......... 8% 13.1M 19s 22950K .......... .......... .......... .......... .......... 8% 9.53M 19s 23000K .......... .......... .......... .......... .......... 8% 20.0M 19s 23050K .......... .......... .......... .......... .......... 8% 25.3M 19s 23100K .......... .......... .......... .......... .......... 8% 16.2M 19s 23150K .......... .......... .......... .......... .......... 8% 18.5M 19s 23200K .......... .......... .......... .......... .......... 8% 16.3M 19s 23250K .......... .......... .......... .......... .......... 8% 22.6M 19s 23300K .......... .......... .......... .......... .......... 8% 19.1M 19s 23350K .......... .......... .......... .......... .......... 8% 16.8M 19s 23400K .......... .......... .......... .......... .......... 8% 14.3M 19s 23450K .......... .......... .......... .......... .......... 8% 13.1M 19s 23500K .......... .......... .......... .......... .......... 8% 15.5M 19s 23550K .......... .......... .......... .......... .......... 9% 12.0M 19s 23600K .......... .......... .......... .......... .......... 9% 13.1M 19s 23650K .......... .......... .......... .......... .......... 9% 26.8M 19s 23700K .......... .......... .......... .......... .......... 9% 13.4M 19s 23750K .......... .......... .......... .......... .......... 9% 37.8M 19s 23800K .......... .......... .......... .......... .......... 9% 21.8M 19s 23850K .......... .......... .......... .......... .......... 9% 10.3M 19s 23900K .......... .......... .......... .......... .......... 9% 5.58M 19s 23950K .......... .......... .......... .......... .......... 9% 5.71M 19s 24000K .......... .......... .......... .......... .......... 9% 6.49M 19s 24050K .......... .......... .......... .......... .......... 9% 5.45M 19s 24100K .......... .......... .......... .......... .......... 9% 5.25M 19s 24150K .......... .......... .......... .......... .......... 9% 26.4M 19s 24200K .......... .......... .......... .......... .......... 9% 30.3M 19s 24250K .......... .......... .......... .......... .......... 9% 21.0M 19s 24300K .......... .......... .......... .......... .......... 9% 33.7M 19s 24350K .......... .......... .......... .......... .......... 9% 41.2M 19s 24400K .......... .......... .......... .......... .......... 9% 20.8M 19s 24450K .......... .......... .......... .......... .......... 9% 17.5M 19s 24500K .......... .......... .......... .......... .......... 9% 36.7M 19s 24550K .......... .......... .......... .......... .......... 9% 15.8M 19s 24600K .......... .......... .......... .......... .......... 9% 19.2M 19s 24650K .......... .......... .......... .......... .......... 9% 15.6M 19s 24700K .......... .......... .......... .......... .......... 9% 15.5M 19s 24750K .......... .......... .......... .......... .......... 9% 15.8M 19s 24800K .......... .......... .......... .......... .......... 9% 10.4M 19s 24850K .......... .......... .......... .......... .......... 9% 11.2M 19s 24900K .......... .......... .......... .......... .......... 9% 23.2M 19s 24950K .......... .......... .......... .......... .......... 9% 12.9M 19s 25000K .......... .......... .......... .......... .......... 9% 22.5M 19s 25050K .......... .......... .......... .......... .......... 9% 16.3M 19s 25100K .......... .......... .......... .......... .......... 9% 16.4M 19s 25150K .......... .......... .......... .......... .......... 9% 19.2M 19s 25200K .......... .......... .......... .......... .......... 9% 13.5M 19s 25250K .......... .......... .......... .......... .......... 9% 19.9M 19s 25300K .......... .......... .......... .......... .......... 9% 21.9M 19s 25350K .......... .......... .......... .......... .......... 9% 19.8M 19s 25400K .......... .......... .......... .......... .......... 9% 20.9M 19s 25450K .......... .......... .......... .......... .......... 9% 13.2M 19s 25500K .......... .......... .......... .......... .......... 9% 21.0M 19s 25550K .......... .......... .......... .......... .......... 9% 19.6M 19s 25600K .......... .......... .......... .......... .......... 9% 17.5M 19s 25650K .......... .......... .......... .......... .......... 9% 23.1M 19s 25700K .......... .......... .......... .......... .......... 9% 17.7M 19s 25750K .......... .......... .......... .......... .......... 9% 18.1M 19s 25800K .......... .......... .......... .......... .......... 9% 19.9M 19s 25850K .......... .......... .......... .......... .......... 9% 12.2M 19s 25900K .......... .......... .......... .......... .......... 9% 19.5M 19s 25950K .......... .......... .......... .......... .......... 9% 16.4M 18s 26000K .......... .......... .......... .......... .......... 9% 15.5M 18s 26050K .......... .......... .......... .......... .......... 9% 7.72M 19s 26100K .......... .......... .......... .......... .......... 9% 5.21M 19s 26150K .......... .......... .......... .......... .......... 9% 6.90M 19s 26200K .......... .......... .......... .......... .......... 10% 8.41M 19s 26250K .......... .......... .......... .......... .......... 10% 10.2M 19s 26300K .......... .......... .......... .......... .......... 10% 7.78M 19s 26350K .......... .......... .......... .......... .......... 10% 10.4M 19s 26400K .......... .......... .......... .......... .......... 10% 11.9M 19s 26450K .......... .......... .......... .......... .......... 10% 21.0M 19s 26500K .......... .......... .......... .......... .......... 10% 26.8M 19s 26550K .......... .......... .......... .......... .......... 10% 33.6M 19s 26600K .......... .......... .......... .......... .......... 10% 24.6M 19s 26650K .......... .......... .......... .......... .......... 10% 23.0M 18s 26700K .......... .......... .......... .......... .......... 10% 22.1M 18s 26750K .......... .......... .......... .......... .......... 10% 31.7M 18s 26800K .......... .......... .......... .......... .......... 10% 24.0M 18s 26850K .......... .......... .......... .......... .......... 10% 18.2M 18s 26900K .......... .......... .......... .......... .......... 10% 19.1M 18s 26950K .......... .......... .......... .......... .......... 10% 33.6M 18s 27000K .......... .......... .......... .......... .......... 10% 21.2M 18s 27050K .......... .......... .......... .......... .......... 10% 21.4M 18s 27100K .......... .......... .......... .......... .......... 10% 20.2M 18s 27150K .......... .......... .......... .......... .......... 10% 25.5M 18s 27200K .......... .......... .......... .......... .......... 10% 16.4M 18s 27250K .......... .......... .......... .......... .......... 10% 53.1M 18s 27300K .......... .......... .......... .......... .......... 10% 23.4M 18s 27350K .......... .......... .......... .......... .......... 10% 15.6M 18s 27400K .......... .......... .......... .......... .......... 10% 18.9M 18s 27450K .......... .......... .......... .......... .......... 10% 12.9M 18s 27500K .......... .......... .......... .......... .......... 10% 10.9M 18s 27550K .......... .......... .......... .......... .......... 10% 18.8M 18s 27600K .......... .......... .......... .......... .......... 10% 9.08M 18s 27650K .......... .......... .......... .......... .......... 10% 6.73M 18s 27700K .......... .......... .......... .......... .......... 10% 8.02M 18s 27750K .......... .......... .......... .......... .......... 10% 9.55M 18s 27800K .......... .......... .......... .......... .......... 10% 10.7M 18s 27850K .......... .......... .......... .......... .......... 10% 8.81M 18s 27900K .......... .......... .......... .......... .......... 10% 7.04M 18s 27950K .......... .......... .......... .......... .......... 10% 6.69M 18s 28000K .......... .......... .......... .......... .......... 10% 16.0M 18s 28050K .......... .......... .......... .......... .......... 10% 9.29M 18s 28100K .......... .......... .......... .......... .......... 10% 11.6M 18s 28150K .......... .......... .......... .......... .......... 10% 14.3M 18s 28200K .......... .......... .......... .......... .......... 10% 10.4M 18s 28250K .......... .......... .......... .......... .......... 10% 14.6M 18s 28300K .......... .......... .......... .......... .......... 10% 12.9M 18s 28350K .......... .......... .......... .......... .......... 10% 9.03M 18s 28400K .......... .......... .......... .......... .......... 10% 10.2M 18s 28450K .......... .......... .......... .......... .......... 10% 8.33M 18s 28500K .......... .......... .......... .......... .......... 10% 10.8M 18s 28550K .......... .......... .......... .......... .......... 10% 9.13M 18s 28600K .......... .......... .......... .......... .......... 10% 7.00M 18s 28650K .......... .......... .......... .......... .......... 10% 16.7M 18s 28700K .......... .......... .......... .......... .......... 10% 12.6M 18s 28750K .......... .......... .......... .......... .......... 10% 12.2M 18s 28800K .......... .......... .......... .......... .......... 11% 13.8M 18s 28850K .......... .......... .......... .......... .......... 11% 8.56M 18s 28900K .......... .......... .......... .......... .......... 11% 10.4M 18s 28950K .......... .......... .......... .......... .......... 11% 7.55M 18s 29000K .......... .......... .......... .......... .......... 11% 17.7M 18s 29050K .......... .......... .......... .......... .......... 11% 17.0M 18s 29100K .......... .......... .......... .......... .......... 11% 13.8M 18s 29150K .......... .......... .......... .......... .......... 11% 21.3M 18s 29200K .......... .......... .......... .......... .......... 11% 13.7M 18s 29250K .......... .......... .......... .......... .......... 11% 13.9M 18s 29300K .......... .......... .......... .......... .......... 11% 16.7M 18s 29350K .......... .......... .......... .......... .......... 11% 13.9M 18s 29400K .......... .......... .......... .......... .......... 11% 11.0M 18s 29450K .......... .......... .......... .......... .......... 11% 14.4M 18s 29500K .......... .......... .......... .......... .......... 11% 9.64M 18s 29550K .......... .......... .......... .......... .......... 11% 15.8M 18s 29600K .......... .......... .......... .......... .......... 11% 13.7M 18s 29650K .......... .......... .......... .......... .......... 11% 18.4M 18s 29700K .......... .......... .......... .......... .......... 11% 12.6M 18s 29750K .......... .......... .......... .......... .......... 11% 18.7M 18s 29800K .......... .......... .......... .......... .......... 11% 18.2M 18s 29850K .......... .......... .......... .......... .......... 11% 19.6M 18s 29900K .......... .......... .......... .......... .......... 11% 10.5M 18s 29950K .......... .......... .......... .......... .......... 11% 10.5M 18s 30000K .......... .......... .......... .......... .......... 11% 13.4M 18s 30050K .......... .......... .......... .......... .......... 11% 11.6M 18s 30100K .......... .......... .......... .......... .......... 11% 11.1M 18s 30150K .......... .......... .......... .......... .......... 11% 13.2M 18s 30200K .......... .......... .......... .......... .......... 11% 11.2M 18s 30250K .......... .......... .......... .......... .......... 11% 7.53M 18s 30300K .......... .......... .......... .......... .......... 11% 144M 18s 30350K .......... .......... .......... .......... .......... 11% 16.3M 18s 30400K .......... .......... .......... .......... .......... 11% 14.9M 18s 30450K .......... .......... .......... .......... .......... 11% 14.4M 18s 30500K .......... .......... .......... .......... .......... 11% 13.7M 18s 30550K .......... .......... .......... .......... .......... 11% 18.2M 18s 30600K .......... .......... .......... .......... .......... 11% 11.3M 18s 30650K .......... .......... .......... .......... .......... 11% 8.10M 18s 30700K .......... .......... .......... .......... .......... 11% 4.70M 18s 30750K .......... .......... .......... .......... .......... 11% 5.73M 18s 30800K .......... .......... .......... .......... .......... 11% 6.34M 18s 30850K .......... .......... .......... .......... .......... 11% 4.58M 18s 30900K .......... .......... .......... .......... .......... 11% 6.16M 18s 30950K .......... .......... .......... .......... .......... 11% 7.78M 18s 31000K .......... .......... .......... .......... .......... 11% 7.63M 18s 31050K .......... .......... .......... .......... .......... 11% 8.09M 18s 31100K .......... .......... .......... .......... .......... 11% 5.77M 18s 31150K .......... .......... .......... .......... .......... 11% 1.94M 19s 31200K .......... .......... .......... .......... .......... 11% 3.87M 19s 31250K .......... .......... .......... .......... .......... 11% 3.80M 19s 31300K .......... .......... .......... .......... .......... 11% 4.12M 19s 31350K .......... .......... .......... .......... .......... 11% 4.88M 19s 31400K .......... .......... .......... .......... .......... 11% 6.61M 19s 31450K .......... .......... .......... .......... .......... 12% 4.04M 19s 31500K .......... .......... .......... .......... .......... 12% 3.15M 19s 31550K .......... .......... .......... .......... .......... 12% 4.00M 19s 31600K .......... .......... .......... .......... .......... 12% 4.10M 19s 31650K .......... .......... .......... .......... .......... 12% 7.60M 19s 31700K .......... .......... .......... .......... .......... 12% 25.0M 19s 31750K .......... .......... .......... .......... .......... 12% 27.7M 19s 31800K .......... .......... .......... .......... .......... 12% 22.1M 19s 31850K .......... .......... .......... .......... .......... 12% 27.3M 19s 31900K .......... .......... .......... .......... .......... 12% 35.5M 19s 31950K .......... .......... .......... .......... .......... 12% 11.9M 19s 32000K .......... .......... .......... .......... .......... 12% 14.8M 19s 32050K .......... .......... .......... .......... .......... 12% 14.8M 19s 32100K .......... .......... .......... .......... .......... 12% 10.2M 19s 32150K .......... .......... .......... .......... .......... 12% 12.1M 19s 32200K .......... .......... .......... .......... .......... 12% 9.44M 19s 32250K .......... .......... .......... .......... .......... 12% 11.3M 19s 32300K .......... .......... .......... .......... .......... 12% 13.6M 19s 32350K .......... .......... .......... .......... .......... 12% 9.00M 19s 32400K .......... .......... .......... .......... .......... 12% 10.8M 19s 32450K .......... .......... .......... .......... .......... 12% 12.7M 19s 32500K .......... .......... .......... .......... .......... 12% 11.4M 19s 32550K .......... .......... .......... .......... .......... 12% 12.9M 19s 32600K .......... .......... .......... .......... .......... 12% 8.06M 19s 32650K .......... .......... .......... .......... .......... 12% 10.9M 19s 32700K .......... .......... .......... .......... .......... 12% 12.7M 19s 32750K .......... .......... .......... .......... .......... 12% 13.0M 19s 32800K .......... .......... .......... .......... .......... 12% 15.9M 19s 32850K .......... .......... .......... .......... .......... 12% 15.6M 19s 32900K .......... .......... .......... .......... .......... 12% 17.3M 19s 32950K .......... .......... .......... .......... .......... 12% 17.0M 19s 33000K .......... .......... .......... .......... .......... 12% 19.6M 19s 33050K .......... .......... .......... .......... .......... 12% 19.6M 19s 33100K .......... .......... .......... .......... .......... 12% 12.3M 19s 33150K .......... .......... .......... .......... .......... 12% 9.40M 19s 33200K .......... .......... .......... .......... .......... 12% 11.4M 19s 33250K .......... .......... .......... .......... .......... 12% 14.3M 19s 33300K .......... .......... .......... .......... .......... 12% 11.1M 19s 33350K .......... .......... .......... .......... .......... 12% 6.58M 19s 33400K .......... .......... .......... .......... .......... 12% 4.74M 19s 33450K .......... .......... .......... .......... .......... 12% 3.61M 19s 33500K .......... .......... .......... .......... .......... 12% 4.27M 19s 33550K .......... .......... .......... .......... .......... 12% 5.14M 19s 33600K .......... .......... .......... .......... .......... 12% 19.9M 19s 33650K .......... .......... .......... .......... .......... 12% 21.6M 19s 33700K .......... .......... .......... .......... .......... 12% 17.7M 19s 33750K .......... .......... .......... .......... .......... 12% 36.1M 19s 33800K .......... .......... .......... .......... .......... 12% 23.8M 19s 33850K .......... .......... .......... .......... .......... 12% 14.2M 19s 33900K .......... .......... .......... .......... .......... 12% 26.3M 19s 33950K .......... .......... .......... .......... .......... 12% 9.19M 19s 34000K .......... .......... .......... .......... .......... 12% 7.19M 19s 34050K .......... .......... .......... .......... .......... 13% 10.7M 19s 34100K .......... .......... .......... .......... .......... 13% 7.42M 19s 34150K .......... .......... .......... .......... .......... 13% 8.00M 19s 34200K .......... .......... .......... .......... .......... 13% 4.63M 19s 34250K .......... .......... .......... .......... .......... 13% 3.49M 19s 34300K .......... .......... .......... .......... .......... 13% 3.60M 19s 34350K .......... .......... .......... .......... .......... 13% 4.05M 19s 34400K .......... .......... .......... .......... .......... 13% 4.88M 19s 34450K .......... .......... .......... .......... .......... 13% 13.7M 19s 34500K .......... .......... .......... .......... .......... 13% 14.4M 19s 34550K .......... .......... .......... .......... .......... 13% 12.8M 19s 34600K .......... .......... .......... .......... .......... 13% 10.4M 19s 34650K .......... .......... .......... .......... .......... 13% 5.65M 19s 34700K .......... .......... .......... .......... .......... 13% 4.38M 19s 34750K .......... .......... .......... .......... .......... 13% 1.76M 19s 34800K .......... .......... .......... .......... .......... 13% 6.87M 19s 34850K .......... .......... .......... .......... .......... 13% 8.46M 19s 34900K .......... .......... .......... .......... .......... 13% 6.07M 19s 34950K .......... .......... .......... .......... .......... 13% 4.60M 19s 35000K .......... .......... .......... .......... .......... 13% 1.85M 20s 35050K .......... .......... .......... .......... .......... 13% 4.25M 20s 35100K .......... .......... .......... .......... .......... 13% 2.34M 20s 35150K .......... .......... .......... .......... .......... 13% 4.15M 20s 35200K .......... .......... .......... .......... .......... 13% 29.2M 20s 35250K .......... .......... .......... .......... .......... 13% 25.6M 20s 35300K .......... .......... .......... .......... .......... 13% 13.4M 20s 35350K .......... .......... .......... .......... .......... 13% 43.9M 20s 35400K .......... .......... .......... .......... .......... 13% 17.7M 20s 35450K .......... .......... .......... .......... .......... 13% 15.3M 20s 35500K .......... .......... .......... .......... .......... 13% 18.4M 20s 35550K .......... .......... .......... .......... .......... 13% 18.0M 20s 35600K .......... .......... .......... .......... .......... 13% 10.1M 20s 35650K .......... .......... .......... .......... .......... 13% 13.2M 20s 35700K .......... .......... .......... .......... .......... 13% 9.75M 20s 35750K .......... .......... .......... .......... .......... 13% 9.26M 20s 35800K .......... .......... .......... .......... .......... 13% 10.4M 20s 35850K .......... .......... .......... .......... .......... 13% 10.2M 20s 35900K .......... .......... .......... .......... .......... 13% 10.1M 20s 35950K .......... .......... .......... .......... .......... 13% 8.44M 20s 36000K .......... .......... .......... .......... .......... 13% 9.81M 20s 36050K .......... .......... .......... .......... .......... 13% 9.23M 20s 36100K .......... .......... .......... .......... .......... 13% 9.17M 20s 36150K .......... .......... .......... .......... .......... 13% 7.80M 20s 36200K .......... .......... .......... .......... .......... 13% 5.81M 20s 36250K .......... .......... .......... .......... .......... 13% 17.4M 20s 36300K .......... .......... .......... .......... .......... 13% 24.6M 20s 36350K .......... .......... .......... .......... .......... 13% 14.4M 20s 36400K .......... .......... .......... .......... .......... 13% 13.3M 20s 36450K .......... .......... .......... .......... .......... 13% 9.41M 20s 36500K .......... .......... .......... .......... .......... 13% 12.0M 20s 36550K .......... .......... .......... .......... .......... 13% 6.08M 20s 36600K .......... .......... .......... .......... .......... 13% 5.61M 20s 36650K .......... .......... .......... .......... .......... 13% 6.79M 20s 36700K .......... .......... .......... .......... .......... 14% 6.60M 20s 36750K .......... .......... .......... .......... .......... 14% 7.92M 20s 36800K .......... .......... .......... .......... .......... 14% 12.9M 20s 36850K .......... .......... .......... .......... .......... 14% 15.1M 20s 36900K .......... .......... .......... .......... .......... 14% 11.8M 20s 36950K .......... .......... .......... .......... .......... 14% 15.1M 20s 37000K .......... .......... .......... .......... .......... 14% 13.5M 20s 37050K .......... .......... .......... .......... .......... 14% 17.6M 20s 37100K .......... .......... .......... .......... .......... 14% 13.1M 20s 37150K .......... .......... .......... .......... .......... 14% 13.1M 20s 37200K .......... .......... .......... .......... .......... 14% 8.35M 20s 37250K .......... .......... .......... .......... .......... 14% 14.5M 20s 37300K .......... .......... .......... .......... .......... 14% 11.2M 20s 37350K .......... .......... .......... .......... .......... 14% 9.89M 20s 37400K .......... .......... .......... .......... .......... 14% 9.30M 20s 37450K .......... .......... .......... .......... .......... 14% 6.38M 20s 37500K .......... .......... .......... .......... .......... 14% 10.5M 20s 37550K .......... .......... .......... .......... .......... 14% 6.76M 20s 37600K .......... .......... .......... .......... .......... 14% 4.75M 20s 37650K .......... .......... .......... .......... .......... 14% 5.49M 20s 37700K .......... .......... .......... .......... .......... 14% 4.15M 20s 37750K .......... .......... .......... .......... .......... 14% 6.29M 20s 37800K .......... .......... .......... .......... .......... 14% 12.8M 20s 37850K .......... .......... .......... .......... .......... 14% 8.24M 20s 37900K .......... .......... .......... .......... .......... 14% 8.41M 20s 37950K .......... .......... .......... .......... .......... 14% 4.81M 20s 38000K .......... .......... .......... .......... .......... 14% 5.15M 20s 38050K .......... .......... .......... .......... .......... 14% 5.98M 20s 38100K .......... .......... .......... .......... .......... 14% 5.83M 20s 38150K .......... .......... .......... .......... .......... 14% 4.56M 20s 38200K .......... .......... .......... .......... .......... 14% 3.79M 20s 38250K .......... .......... .......... .......... .......... 14% 3.28M 20s 38300K .......... .......... .......... .......... .......... 14% 3.45M 20s 38350K .......... .......... .......... .......... .......... 14% 4.36M 20s 38400K .......... .......... .......... .......... .......... 14% 12.3M 20s 38450K .......... .......... .......... .......... .......... 14% 9.24M 20s 38500K .......... .......... .......... .......... .......... 14% 13.2M 20s 38550K .......... .......... .......... .......... .......... 14% 9.59M 20s 38600K .......... .......... .......... .......... .......... 14% 7.27M 20s 38650K .......... .......... .......... .......... .......... 14% 9.40M 20s 38700K .......... .......... .......... .......... .......... 14% 6.19M 20s 38750K .......... .......... .......... .......... .......... 14% 7.99M 20s 38800K .......... .......... .......... .......... .......... 14% 7.07M 20s 38850K .......... .......... .......... .......... .......... 14% 7.11M 20s 38900K .......... .......... .......... .......... .......... 14% 12.8M 20s 38950K .......... .......... .......... .......... .......... 14% 8.69M 20s 39000K .......... .......... .......... .......... .......... 14% 31.9M 20s 39050K .......... .......... .......... .......... .......... 14% 12.8M 20s 39100K .......... .......... .......... .......... .......... 14% 13.4M 20s 39150K .......... .......... .......... .......... .......... 14% 12.5M 20s 39200K .......... .......... .......... .......... .......... 14% 8.77M 20s 39250K .......... .......... .......... .......... .......... 14% 13.0M 20s 39300K .......... .......... .......... .......... .......... 15% 12.1M 20s 39350K .......... .......... .......... .......... .......... 15% 5.28M 20s 39400K .......... .......... .......... .......... .......... 15% 7.65M 20s 39450K .......... .......... .......... .......... .......... 15% 4.59M 20s 39500K .......... .......... .......... .......... .......... 15% 5.71M 20s 39550K .......... .......... .......... .......... .......... 15% 2.72M 20s 39600K .......... .......... .......... .......... .......... 15% 2.35M 20s 39650K .......... .......... .......... .......... .......... 15% 5.64M 20s 39700K .......... .......... .......... .......... .......... 15% 21.4M 20s 39750K .......... .......... .......... .......... .......... 15% 12.0M 20s 39800K .......... .......... .......... .......... .......... 15% 10.7M 20s 39850K .......... .......... .......... .......... .......... 15% 8.24M 20s 39900K .......... .......... .......... .......... .......... 15% 18.9M 20s 39950K .......... .......... .......... .......... .......... 15% 10.2M 20s 40000K .......... .......... .......... .......... .......... 15% 11.6M 20s 40050K .......... .......... .......... .......... .......... 15% 12.8M 20s 40100K .......... .......... .......... .......... .......... 15% 10.6M 20s 40150K .......... .......... .......... .......... .......... 15% 9.41M 20s 40200K .......... .......... .......... .......... .......... 15% 11.1M 20s 40250K .......... .......... .......... .......... .......... 15% 12.7M 20s 40300K .......... .......... .......... .......... .......... 15% 9.61M 20s 40350K .......... .......... .......... .......... .......... 15% 5.37M 20s 40400K .......... .......... .......... .......... .......... 15% 6.64M 20s 40450K .......... .......... .......... .......... .......... 15% 5.87M 20s 40500K .......... .......... .......... .......... .......... 15% 9.99M 20s 40550K .......... .......... .......... .......... .......... 15% 20.6M 20s 40600K .......... .......... .......... .......... .......... 15% 9.43M 20s 40650K .......... .......... .......... .......... .......... 15% 8.50M 20s 40700K .......... .......... .......... .......... .......... 15% 10.4M 20s 40750K .......... .......... .......... .......... .......... 15% 7.27M 20s 40800K .......... .......... .......... .......... .......... 15% 14.8M 20s 40850K .......... .......... .......... .......... .......... 15% 7.09M 20s 40900K .......... .......... .......... .......... .......... 15% 6.37M 20s 40950K .......... .......... .......... .......... .......... 15% 6.53M 20s 41000K .......... .......... .......... .......... .......... 15% 6.71M 20s 41050K .......... .......... .......... .......... .......... 15% 6.76M 20s 41100K .......... .......... .......... .......... .......... 15% 5.24M 20s 41150K .......... .......... .......... .......... .......... 15% 4.54M 20s 41200K .......... .......... .......... .......... .......... 15% 4.39M 20s 41250K .......... .......... .......... .......... .......... 15% 5.55M 20s 41300K .......... .......... .......... .......... .......... 15% 6.20M 20s 41350K .......... .......... .......... .......... .......... 15% 8.61M 20s 41400K .......... .......... .......... .......... .......... 15% 7.23M 20s 41450K .......... .......... .......... .......... .......... 15% 25.5M 20s 41500K .......... .......... .......... .......... .......... 15% 11.4M 20s 41550K .......... .......... .......... .......... .......... 15% 14.5M 20s 41600K .......... .......... .......... .......... .......... 15% 10.3M 20s 41650K .......... .......... .......... .......... .......... 15% 9.90M 20s 41700K .......... .......... .......... .......... .......... 15% 11.3M 20s 41750K .......... .......... .......... .......... .......... 15% 7.30M 20s 41800K .......... .......... .......... .......... .......... 15% 8.28M 20s 41850K .......... .......... .......... .......... .......... 15% 6.84M 20s 41900K .......... .......... .......... .......... .......... 15% 7.39M 20s 41950K .......... .......... .......... .......... .......... 16% 5.03M 20s 42000K .......... .......... .......... .......... .......... 16% 4.92M 20s 42050K .......... .......... .......... .......... .......... 16% 5.31M 20s 42100K .......... .......... .......... .......... .......... 16% 3.45M 20s 42150K .......... .......... .......... .......... .......... 16% 6.67M 20s 42200K .......... .......... .......... .......... .......... 16% 7.90M 20s 42250K .......... .......... .......... .......... .......... 16% 10.3M 20s 42300K .......... .......... .......... .......... .......... 16% 9.66M 20s 42350K .......... .......... .......... .......... .......... 16% 7.87M 20s 42400K .......... .......... .......... .......... .......... 16% 8.73M 20s 42450K .......... .......... .......... .......... .......... 16% 6.60M 20s 42500K .......... .......... .......... .......... .......... 16% 66.6M 20s 42550K .......... .......... .......... .......... .......... 16% 11.3M 20s 42600K .......... .......... .......... .......... .......... 16% 7.29M 20s 42650K .......... .......... .......... .......... .......... 16% 14.8M 20s 42700K .......... .......... .......... .......... .......... 16% 8.33M 20s 42750K .......... .......... .......... .......... .......... 16% 12.2M 20s 42800K .......... .......... .......... .......... .......... 16% 7.76M 20s 42850K .......... .......... .......... .......... .......... 16% 6.13M 20s 42900K .......... .......... .......... .......... .......... 16% 5.88M 20s 42950K .......... .......... .......... .......... .......... 16% 221K 22s 43000K .......... .......... .......... .......... .......... 16% 6.35M 22s 43050K .......... .......... .......... .......... .......... 16% 7.19M 22s 43100K .......... .......... .......... .......... .......... 16% 4.63M 22s 43150K .......... .......... .......... .......... .......... 16% 4.25M 22s 43200K .......... .......... .......... .......... .......... 16% 5.08M 22s 43250K .......... .......... .......... .......... .......... 16% 15.1M 22s 43300K .......... .......... .......... .......... .......... 16% 15.4M 22s 43350K .......... .......... .......... .......... .......... 16% 6.17M 22s 43400K .......... .......... .......... .......... .......... 16% 9.50M 22s 43450K .......... .......... .......... .......... .......... 16% 7.44M 22s 43500K .......... .......... .......... .......... .......... 16% 8.14M 22s 43550K .......... .......... .......... .......... .......... 16% 10.3M 22s 43600K .......... .......... .......... .......... .......... 16% 7.41M 22s 43650K .......... .......... .......... .......... .......... 16% 7.25M 22s 43700K .......... .......... .......... .......... .......... 16% 7.33M 22s 43750K .......... .......... .......... .......... .......... 16% 6.79M 22s 43800K .......... .......... .......... .......... .......... 16% 6.84M 22s 43850K .......... .......... .......... .......... .......... 16% 3.54M 22s 43900K .......... .......... .......... .......... .......... 16% 4.68M 22s 43950K .......... .......... .......... .......... .......... 16% 2.00M 22s 44000K .......... .......... .......... .......... .......... 16% 2.19M 22s 44050K .......... .......... .......... .......... .......... 16% 3.13M 22s 44100K .......... .......... .......... .......... .......... 16% 6.88M 22s 44150K .......... .......... .......... .......... .......... 16% 8.63M 22s 44200K .......... .......... .......... .......... .......... 16% 7.22M 22s 44250K .......... .......... .......... .......... .......... 16% 5.63M 22s 44300K .......... .......... .......... .......... .......... 16% 4.14M 22s 44350K .......... .......... .......... .......... .......... 16% 3.86M 22s 44400K .......... .......... .......... .......... .......... 16% 4.36M 22s 44450K .......... .......... .......... .......... .......... 16% 7.16M 22s 44500K .......... .......... .......... .......... .......... 16% 15.8M 22s 44550K .......... .......... .......... .......... .......... 17% 10.6M 22s 44600K .......... .......... .......... .......... .......... 17% 8.56M 22s 44650K .......... .......... .......... .......... .......... 17% 16.4M 22s 44700K .......... .......... .......... .......... .......... 17% 9.11M 22s 44750K .......... .......... .......... .......... .......... 17% 9.80M 22s 44800K .......... .......... .......... .......... .......... 17% 7.30M 22s 44850K .......... .......... .......... .......... .......... 17% 4.16M 22s 44900K .......... .......... .......... .......... .......... 17% 15.8M 22s 44950K .......... .......... .......... .......... .......... 17% 5.63M 22s 45000K .......... .......... .......... .......... .......... 17% 6.21M 22s 45050K .......... .......... .......... .......... .......... 17% 5.81M 22s 45100K .......... .......... .......... .......... .......... 17% 6.35M 22s 45150K .......... .......... .......... .......... .......... 17% 5.62M 22s 45200K .......... .......... .......... .......... .......... 17% 9.90M 22s 45250K .......... .......... .......... .......... .......... 17% 7.61M 22s 45300K .......... .......... .......... .......... .......... 17% 13.1M 22s 45350K .......... .......... .......... .......... .......... 17% 8.09M 22s 45400K .......... .......... .......... .......... .......... 17% 7.27M 22s 45450K .......... .......... .......... .......... .......... 17% 5.45M 22s 45500K .......... .......... .......... .......... .......... 17% 5.47M 22s 45550K .......... .......... .......... .......... .......... 17% 5.89M 22s 45600K .......... .......... .......... .......... .......... 17% 5.16M 22s 45650K .......... .......... .......... .......... .......... 17% 9.16M 22s 45700K .......... .......... .......... .......... .......... 17% 6.95M 22s 45750K .......... .......... .......... .......... .......... 17% 8.49M 22s 45800K .......... .......... .......... .......... .......... 17% 8.83M 22s 45850K .......... .......... .......... .......... .......... 17% 7.80M 22s 45900K .......... .......... .......... .......... .......... 17% 12.3M 22s 45950K .......... .......... .......... .......... .......... 17% 8.95M 22s 46000K .......... .......... .......... .......... .......... 17% 15.4M 22s 46050K .......... .......... .......... .......... .......... 17% 12.9M 22s 46100K .......... .......... .......... .......... .......... 17% 25.1M 22s 46150K .......... .......... .......... .......... .......... 17% 22.3M 22s 46200K .......... .......... .......... .......... .......... 17% 13.1M 22s 46250K .......... .......... .......... .......... .......... 17% 19.3M 22s 46300K .......... .......... .......... .......... .......... 17% 20.0M 22s 46350K .......... .......... .......... .......... .......... 17% 19.1M 22s 46400K .......... .......... .......... .......... .......... 17% 17.4M 22s 46450K .......... .......... .......... .......... .......... 17% 13.2M 22s 46500K .......... .......... .......... .......... .......... 17% 16.2M 22s 46550K .......... .......... .......... .......... .......... 17% 7.17M 22s 46600K .......... .......... .......... .......... .......... 17% 14.6M 22s 46650K .......... .......... .......... .......... .......... 17% 12.2M 22s 46700K .......... .......... .......... .......... .......... 17% 9.18M 22s 46750K .......... .......... .......... .......... .......... 17% 7.73M 22s 46800K .......... .......... .......... .......... .......... 17% 8.26M 22s 46850K .......... .......... .......... .......... .......... 17% 4.99M 22s 46900K .......... .......... .......... .......... .......... 17% 7.01M 22s 46950K .......... .......... .......... .......... .......... 17% 5.50M 22s 47000K .......... .......... .......... .......... .......... 17% 8.78M 22s 47050K .......... .......... .......... .......... .......... 17% 8.31M 22s 47100K .......... .......... .......... .......... .......... 17% 5.31M 22s 47150K .......... .......... .......... .......... .......... 18% 6.01M 22s 47200K .......... .......... .......... .......... .......... 18% 6.92M 22s 47250K .......... .......... .......... .......... .......... 18% 15.8M 22s 47300K .......... .......... .......... .......... .......... 18% 14.6M 22s 47350K .......... .......... .......... .......... .......... 18% 14.1M 22s 47400K .......... .......... .......... .......... .......... 18% 17.0M 22s 47450K .......... .......... .......... .......... .......... 18% 13.2M 22s 47500K .......... .......... .......... .......... .......... 18% 12.2M 22s 47550K .......... .......... .......... .......... .......... 18% 8.19M 22s 47600K .......... .......... .......... .......... .......... 18% 9.39M 22s 47650K .......... .......... .......... .......... .......... 18% 9.34M 22s 47700K .......... .......... .......... .......... .......... 18% 5.13M 22s 47750K .......... .......... .......... .......... .......... 18% 8.96M 22s 47800K .......... .......... .......... .......... .......... 18% 8.33M 22s 47850K .......... .......... .......... .......... .......... 18% 9.73M 22s 47900K .......... .......... .......... .......... .......... 18% 20.3M 22s 47950K .......... .......... .......... .......... .......... 18% 11.0M 22s 48000K .......... .......... .......... .......... .......... 18% 19.8M 22s 48050K .......... .......... .......... .......... .......... 18% 18.8M 22s 48100K .......... .......... .......... .......... .......... 18% 18.1M 22s 48150K .......... .......... .......... .......... .......... 18% 19.3M 22s 48200K .......... .......... .......... .......... .......... 18% 10.1M 22s 48250K .......... .......... .......... .......... .......... 18% 8.83M 22s 48300K .......... .......... .......... .......... .......... 18% 41.1M 22s 48350K .......... .......... .......... .......... .......... 18% 12.7M 22s 48400K .......... .......... .......... .......... .......... 18% 9.65M 22s 48450K .......... .......... .......... .......... .......... 18% 10.6M 22s 48500K .......... .......... .......... .......... .......... 18% 17.8M 22s 48550K .......... .......... .......... .......... .......... 18% 10.7M 22s 48600K .......... .......... .......... .......... .......... 18% 10.2M 22s 48650K .......... .......... .......... .......... .......... 18% 17.9M 22s 48700K .......... .......... .......... .......... .......... 18% 10.2M 22s 48750K .......... .......... .......... .......... .......... 18% 19.2M 22s 48800K .......... .......... .......... .......... .......... 18% 21.1M 22s 48850K .......... .......... .......... .......... .......... 18% 16.6M 22s 48900K .......... .......... .......... .......... .......... 18% 25.4M 22s 48950K .......... .......... .......... .......... .......... 18% 19.9M 22s 49000K .......... .......... .......... .......... .......... 18% 18.7M 22s 49050K .......... .......... .......... .......... .......... 18% 22.2M 22s 49100K .......... .......... .......... .......... .......... 18% 54.1M 21s 49150K .......... .......... .......... .......... .......... 18% 19.5M 21s 49200K .......... .......... .......... .......... .......... 18% 17.5M 21s 49250K .......... .......... .......... .......... .......... 18% 19.2M 21s 49300K .......... .......... .......... .......... .......... 18% 18.6M 21s 49350K .......... .......... .......... .......... .......... 18% 8.52M 21s 49400K .......... .......... .......... .......... .......... 18% 130M 21s 49450K .......... .......... .......... .......... .......... 18% 16.8M 21s 49500K .......... .......... .......... .......... .......... 18% 13.6M 21s 49550K .......... .......... .......... .......... .......... 18% 20.5M 21s 49600K .......... .......... .......... .......... .......... 18% 15.5M 21s 49650K .......... .......... .......... .......... .......... 18% 11.8M 21s 49700K .......... .......... .......... .......... .......... 18% 12.0M 21s 49750K .......... .......... .......... .......... .......... 18% 12.7M 21s 49800K .......... .......... .......... .......... .......... 19% 18.6M 21s 49850K .......... .......... .......... .......... .......... 19% 12.4M 21s 49900K .......... .......... .......... .......... .......... 19% 12.3M 21s 49950K .......... .......... .......... .......... .......... 19% 12.6M 21s 50000K .......... .......... .......... .......... .......... 19% 12.0M 21s 50050K .......... .......... .......... .......... .......... 19% 17.9M 21s 50100K .......... .......... .......... .......... .......... 19% 12.2M 21s 50150K .......... .......... .......... .......... .......... 19% 8.33M 21s 50200K .......... .......... .......... .......... .......... 19% 53.0M 21s 50250K .......... .......... .......... .......... .......... 19% 20.6M 21s 50300K .......... .......... .......... .......... .......... 19% 108M 21s 50350K .......... .......... .......... .......... .......... 19% 9.48M 21s 50400K .......... .......... .......... .......... .......... 19% 8.26M 21s 50450K .......... .......... .......... .......... .......... 19% 7.62M 21s 50500K .......... .......... .......... .......... .......... 19% 5.67M 21s 50550K .......... .......... .......... .......... .......... 19% 7.25M 21s 50600K .......... .......... .......... .......... .......... 19% 5.43M 21s 50650K .......... .......... .......... .......... .......... 19% 5.60M 21s 50700K .......... .......... .......... .......... .......... 19% 7.46M 21s 50750K .......... .......... .......... .......... .......... 19% 10.7M 21s 50800K .......... .......... .......... .......... .......... 19% 10.9M 21s 50850K .......... .......... .......... .......... .......... 19% 9.29M 21s 50900K .......... .......... .......... .......... .......... 19% 11.6M 21s 50950K .......... .......... .......... .......... .......... 19% 6.57M 21s 51000K .......... .......... .......... .......... .......... 19% 19.0M 21s 51050K .......... .......... .......... .......... .......... 19% 24.7M 21s 51100K .......... .......... .......... .......... .......... 19% 15.6M 21s 51150K .......... .......... .......... .......... .......... 19% 20.4M 21s 51200K .......... .......... .......... .......... .......... 19% 24.5M 21s 51250K .......... .......... .......... .......... .......... 19% 15.3M 21s 51300K .......... .......... .......... .......... .......... 19% 15.1M 21s 51350K .......... .......... .......... .......... .......... 19% 18.0M 21s 51400K .......... .......... .......... .......... .......... 19% 14.2M 21s 51450K .......... .......... .......... .......... .......... 19% 10.5M 21s 51500K .......... .......... .......... .......... .......... 19% 15.9M 21s 51550K .......... .......... .......... .......... .......... 19% 28.4M 21s 51600K .......... .......... .......... .......... .......... 19% 12.2M 21s 51650K .......... .......... .......... .......... .......... 19% 14.5M 21s 51700K .......... .......... .......... .......... .......... 19% 7.61M 21s 51750K .......... .......... .......... .......... .......... 19% 8.78M 21s 51800K .......... .......... .......... .......... .......... 19% 13.9M 21s 51850K .......... .......... .......... .......... .......... 19% 6.66M 21s 51900K .......... .......... .......... .......... .......... 19% 7.26M 21s 51950K .......... .......... .......... .......... .......... 19% 4.86M 21s 52000K .......... .......... .......... .......... .......... 19% 7.06M 21s 52050K .......... .......... .......... .......... .......... 19% 6.63M 21s 52100K .......... .......... .......... .......... .......... 19% 6.13M 21s 52150K .......... .......... .......... .......... .......... 19% 3.71M 21s 52200K .......... .......... .......... .......... .......... 19% 3.39M 21s 52250K .......... .......... .......... .......... .......... 19% 3.22M 21s 52300K .......... .......... .......... .......... .......... 19% 2.83M 21s 52350K .......... .......... .......... .......... .......... 19% 1.90M 21s 52400K .......... .......... .......... .......... .......... 20% 2.17M 21s 52450K .......... .......... .......... .......... .......... 20% 2.49M 21s 52500K .......... .......... .......... .......... .......... 20% 15.0M 21s 52550K .......... .......... .......... .......... .......... 20% 15.9M 21s 52600K .......... .......... .......... .......... .......... 20% 7.62M 21s 52650K .......... .......... .......... .......... .......... 20% 9.01M 21s 52700K .......... .......... .......... .......... .......... 20% 6.35M 21s 52750K .......... .......... .......... .......... .......... 20% 6.94M 21s 52800K .......... .......... .......... .......... .......... 20% 8.23M 21s 52850K .......... .......... .......... .......... .......... 20% 7.45M 21s 52900K .......... .......... .......... .......... .......... 20% 6.95M 21s 52950K .......... .......... .......... .......... .......... 20% 7.75M 21s 53000K .......... .......... .......... .......... .......... 20% 6.96M 21s 53050K .......... .......... .......... .......... .......... 20% 9.10M 21s 53100K .......... .......... .......... .......... .......... 20% 13.6M 21s 53150K .......... .......... .......... .......... .......... 20% 9.46M 21s 53200K .......... .......... .......... .......... .......... 20% 7.48M 21s 53250K .......... .......... .......... .......... .......... 20% 6.42M 21s 53300K .......... .......... .......... .......... .......... 20% 8.05M 21s 53350K .......... .......... .......... .......... .......... 20% 6.37M 21s 53400K .......... .......... .......... .......... .......... 20% 6.50M 21s 53450K .......... .......... .......... .......... .......... 20% 7.27M 21s 53500K .......... .......... .......... .......... .......... 20% 7.04M 21s 53550K .......... .......... .......... .......... .......... 20% 9.04M 21s 53600K .......... .......... .......... .......... .......... 20% 12.0M 21s 53650K .......... .......... .......... .......... .......... 20% 6.94M 21s 53700K .......... .......... .......... .......... .......... 20% 6.60M 21s 53750K .......... .......... .......... .......... .......... 20% 5.19M 21s 53800K .......... .......... .......... .......... .......... 20% 5.35M 21s 53850K .......... .......... .......... .......... .......... 20% 4.36M 21s 53900K .......... .......... .......... .......... .......... 20% 3.50M 21s 53950K .......... .......... .......... .......... .......... 20% 6.91M 21s 54000K .......... .......... .......... .......... .......... 20% 4.78M 21s 54050K .......... .......... .......... .......... .......... 20% 6.07M 21s 54100K .......... .......... .......... .......... .......... 20% 4.47M 21s 54150K .......... .......... .......... .......... .......... 20% 6.57M 21s 54200K .......... .......... .......... .......... .......... 20% 4.05M 21s 54250K .......... .......... .......... .......... .......... 20% 11.1M 21s 54300K .......... .......... .......... .......... .......... 20% 11.6M 21s 54350K .......... .......... .......... .......... .......... 20% 8.38M 21s 54400K .......... .......... .......... .......... .......... 20% 11.4M 21s 54450K .......... .......... .......... .......... .......... 20% 6.46M 21s 54500K .......... .......... .......... .......... .......... 20% 21.4M 21s 54550K .......... .......... .......... .......... .......... 20% 11.2M 21s 54600K .......... .......... .......... .......... .......... 20% 11.6M 21s 54650K .......... .......... .......... .......... .......... 20% 12.6M 21s 54700K .......... .......... .......... .......... .......... 20% 19.2M 21s 54750K .......... .......... .......... .......... .......... 20% 21.4M 21s 54800K .......... .......... .......... .......... .......... 20% 20.6M 21s 54850K .......... .......... .......... .......... .......... 20% 18.8M 21s 54900K .......... .......... .......... .......... .......... 20% 19.5M 21s 54950K .......... .......... .......... .......... .......... 20% 9.14M 21s 55000K .......... .......... .......... .......... .......... 20% 20.3M 21s 55050K .......... .......... .......... .......... .......... 21% 12.7M 21s 55100K .......... .......... .......... .......... .......... 21% 10.7M 21s 55150K .......... .......... .......... .......... .......... 21% 12.7M 21s 55200K .......... .......... .......... .......... .......... 21% 10.1M 21s 55250K .......... .......... .......... .......... .......... 21% 12.3M 21s 55300K .......... .......... .......... .......... .......... 21% 12.6M 21s 55350K .......... .......... .......... .......... .......... 21% 9.07M 21s 55400K .......... .......... .......... .......... .......... 21% 11.4M 21s 55450K .......... .......... .......... .......... .......... 21% 7.34M 21s 55500K .......... .......... .......... .......... .......... 21% 5.81M 21s 55550K .......... .......... .......... .......... .......... 21% 4.92M 21s 55600K .......... .......... .......... .......... .......... 21% 4.82M 21s 55650K .......... .......... .......... .......... .......... 21% 8.95M 21s 55700K .......... .......... .......... .......... .......... 21% 5.92M 21s 55750K .......... .......... .......... .......... .......... 21% 8.72M 21s 55800K .......... .......... .......... .......... .......... 21% 31.1M 21s 55850K .......... .......... .......... .......... .......... 21% 15.5M 21s 55900K .......... .......... .......... .......... .......... 21% 8.74M 21s 55950K .......... .......... .......... .......... .......... 21% 18.6M 21s 56000K .......... .......... .......... .......... .......... 21% 13.6M 21s 56050K .......... .......... .......... .......... .......... 21% 10.8M 21s 56100K .......... .......... .......... .......... .......... 21% 8.25M 21s 56150K .......... .......... .......... .......... .......... 21% 10.3M 21s 56200K .......... .......... .......... .......... .......... 21% 8.79M 21s 56250K .......... .......... .......... .......... .......... 21% 9.23M 21s 56300K .......... .......... .......... .......... .......... 21% 12.2M 21s 56350K .......... .......... .......... .......... .......... 21% 7.70M 21s 56400K .......... .......... .......... .......... .......... 21% 8.23M 21s 56450K .......... .......... .......... .......... .......... 21% 5.05M 21s 56500K .......... .......... .......... .......... .......... 21% 35.1M 21s 56550K .......... .......... .......... .......... .......... 21% 12.3M 21s 56600K .......... .......... .......... .......... .......... 21% 11.6M 21s 56650K .......... .......... .......... .......... .......... 21% 11.9M 21s 56700K .......... .......... .......... .......... .......... 21% 11.8M 21s 56750K .......... .......... .......... .......... .......... 21% 9.68M 21s 56800K .......... .......... .......... .......... .......... 21% 6.99M 21s 56850K .......... .......... .......... .......... .......... 21% 6.09M 21s 56900K .......... .......... .......... .......... .......... 21% 3.47M 21s 56950K .......... .......... .......... .......... .......... 21% 100M 21s 57000K .......... .......... .......... .......... .......... 21% 23.1M 21s 57050K .......... .......... .......... .......... .......... 21% 14.0M 21s 57100K .......... .......... .......... .......... .......... 21% 9.46M 21s 57150K .......... .......... .......... .......... .......... 21% 16.3M 21s 57200K .......... .......... .......... .......... .......... 21% 6.45M 21s 57250K .......... .......... .......... .......... .......... 21% 8.47M 21s 57300K .......... .......... .......... .......... .......... 21% 8.56M 21s 57350K .......... .......... .......... .......... .......... 21% 5.57M 21s 57400K .......... .......... .......... .......... .......... 21% 2.72M 21s 57450K .......... .......... .......... .......... .......... 21% 9.12M 21s 57500K .......... .......... .......... .......... .......... 21% 5.08M 21s 57550K .......... .......... .......... .......... .......... 21% 7.83M 21s 57600K .......... .......... .......... .......... .......... 21% 17.3M 21s 57650K .......... .......... .......... .......... .......... 22% 18.9M 21s 57700K .......... .......... .......... .......... .......... 22% 13.9M 21s 57750K .......... .......... .......... .......... .......... 22% 7.22M 21s 57800K .......... .......... .......... .......... .......... 22% 31.3M 21s 57850K .......... .......... .......... .......... .......... 22% 19.8M 21s 57900K .......... .......... .......... .......... .......... 22% 10.3M 21s 57950K .......... .......... .......... .......... .......... 22% 7.24M 21s 58000K .......... .......... .......... .......... .......... 22% 6.86M 21s 58050K .......... .......... .......... .......... .......... 22% 216K 22s 58100K .......... .......... .......... .......... .......... 22% 2.95M 22s 58150K .......... .......... .......... .......... .......... 22% 5.60M 22s 58200K .......... .......... .......... .......... .......... 22% 7.73M 22s 58250K .......... .......... .......... .......... .......... 22% 9.38M 22s 58300K .......... .......... .......... .......... .......... 22% 10.3M 22s 58350K .......... .......... .......... .......... .......... 22% 8.53M 22s 58400K .......... .......... .......... .......... .......... 22% 9.56M 22s 58450K .......... .......... .......... .......... .......... 22% 4.50M 22s 58500K .......... .......... .......... .......... .......... 22% 4.58M 22s 58550K .......... .......... .......... .......... .......... 22% 4.00M 22s 58600K .......... .......... .......... .......... .......... 22% 4.64M 22s 58650K .......... .......... .......... .......... .......... 22% 9.84M 22s 58700K .......... .......... .......... .......... .......... 22% 6.98M 22s 58750K .......... .......... .......... .......... .......... 22% 9.48M 22s 58800K .......... .......... .......... .......... .......... 22% 5.64M 22s 58850K .......... .......... .......... .......... .......... 22% 4.72M 22s 58900K .......... .......... .......... .......... .......... 22% 4.82M 22s 58950K .......... .......... .......... .......... .......... 22% 5.03M 22s 59000K .......... .......... .......... .......... .......... 22% 6.49M 22s 59050K .......... .......... .......... .......... .......... 22% 4.45M 22s 59100K .......... .......... .......... .......... .......... 22% 4.13M 22s 59150K .......... .......... .......... .......... .......... 22% 4.51M 22s 59200K .......... .......... .......... .......... .......... 22% 3.35M 22s 59250K .......... .......... .......... .......... .......... 22% 4.91M 22s 59300K .......... .......... .......... .......... .......... 22% 4.16M 22s 59350K .......... .......... .......... .......... .......... 22% 5.95M 22s 59400K .......... .......... .......... .......... .......... 22% 14.1M 22s 59450K .......... .......... .......... .......... .......... 22% 13.2M 22s 59500K .......... .......... .......... .......... .......... 22% 13.1M 22s 59550K .......... .......... .......... .......... .......... 22% 12.5M 22s 59600K .......... .......... .......... .......... .......... 22% 11.4M 22s 59650K .......... .......... .......... .......... .......... 22% 12.3M 22s 59700K .......... .......... .......... .......... .......... 22% 9.35M 22s 59750K .......... .......... .......... .......... .......... 22% 9.25M 22s 59800K .......... .......... .......... .......... .......... 22% 5.97M 22s 59850K .......... .......... .......... .......... .......... 22% 6.13M 22s 59900K .......... .......... .......... .......... .......... 22% 8.51M 22s 59950K .......... .......... .......... .......... .......... 22% 5.03M 22s 60000K .......... .......... .......... .......... .......... 22% 5.39M 22s 60050K .......... .......... .......... .......... .......... 22% 4.67M 22s 60100K .......... .......... .......... .......... .......... 22% 3.90M 22s 60150K .......... .......... .......... .......... .......... 22% 1.11M 22s 60200K .......... .......... .......... .......... .......... 22% 1.43M 22s 60250K .......... .......... .......... .......... .......... 22% 7.05M 22s 60300K .......... .......... .......... .......... .......... 23% 3.99M 22s 60350K .......... .......... .......... .......... .......... 23% 3.09M 22s 60400K .......... .......... .......... .......... .......... 23% 5.13M 22s 60450K .......... .......... .......... .......... .......... 23% 7.06M 22s 60500K .......... .......... .......... .......... .......... 23% 7.38M 22s 60550K .......... .......... .......... .......... .......... 23% 15.7M 22s 60600K .......... .......... .......... .......... .......... 23% 10.0M 22s 60650K .......... .......... .......... .......... .......... 23% 10.4M 22s 60700K .......... .......... .......... .......... .......... 23% 8.82M 22s 60750K .......... .......... .......... .......... .......... 23% 7.65M 22s 60800K .......... .......... .......... .......... .......... 23% 9.46M 22s 60850K .......... .......... .......... .......... .......... 23% 7.73M 22s 60900K .......... .......... .......... .......... .......... 23% 7.50M 22s 60950K .......... .......... .......... .......... .......... 23% 3.06M 22s 61000K .......... .......... .......... .......... .......... 23% 3.22M 22s 61050K .......... .......... .......... .......... .......... 23% 3.14M 22s 61100K .......... .......... .......... .......... .......... 23% 3.58M 22s 61150K .......... .......... .......... .......... .......... 23% 3.64M 22s 61200K .......... .......... .......... .......... .......... 23% 6.64M 22s 61250K .......... .......... .......... .......... .......... 23% 10.2M 22s 61300K .......... .......... .......... .......... .......... 23% 40.0M 22s 61350K .......... .......... .......... .......... .......... 23% 15.6M 22s 61400K .......... .......... .......... .......... .......... 23% 16.7M 22s 61450K .......... .......... .......... .......... .......... 23% 15.9M 22s 61500K .......... .......... .......... .......... .......... 23% 12.7M 22s 61550K .......... .......... .......... .......... .......... 23% 10.3M 22s 61600K .......... .......... .......... .......... .......... 23% 13.8M 22s 61650K .......... .......... .......... .......... .......... 23% 9.79M 22s 61700K .......... .......... .......... .......... .......... 23% 11.8M 22s 61750K .......... .......... .......... .......... .......... 23% 6.56M 22s 61800K .......... .......... .......... .......... .......... 23% 9.82M 22s 61850K .......... .......... .......... .......... .......... 23% 6.47M 22s 61900K .......... .......... .......... .......... .......... 23% 6.61M 22s 61950K .......... .......... .......... .......... .......... 23% 5.30M 22s 62000K .......... .......... .......... .......... .......... 23% 5.03M 22s 62050K .......... .......... .......... .......... .......... 23% 4.05M 22s 62100K .......... .......... .......... .......... .......... 23% 2.86M 22s 62150K .......... .......... .......... .......... .......... 23% 3.87M 22s 62200K .......... .......... .......... .......... .......... 23% 3.77M 22s 62250K .......... .......... .......... .......... .......... 23% 16.4M 22s 62300K .......... .......... .......... .......... .......... 23% 9.31M 22s 62350K .......... .......... .......... .......... .......... 23% 17.1M 22s 62400K .......... .......... .......... .......... .......... 23% 13.8M 22s 62450K .......... .......... .......... .......... .......... 23% 11.5M 22s 62500K .......... .......... .......... .......... .......... 23% 10.2M 22s 62550K .......... .......... .......... .......... .......... 23% 8.83M 22s 62600K .......... .......... .......... .......... .......... 23% 8.24M 22s 62650K .......... .......... .......... .......... .......... 23% 11.0M 22s 62700K .......... .......... .......... .......... .......... 23% 8.94M 22s 62750K .......... .......... .......... .......... .......... 23% 7.47M 22s 62800K .......... .......... .......... .......... .......... 23% 8.18M 22s 62850K .......... .......... .......... .......... .......... 23% 8.89M 22s 62900K .......... .......... .......... .......... .......... 24% 5.51M 22s 62950K .......... .......... .......... .......... .......... 24% 3.62M 22s 63000K .......... .......... .......... .......... .......... 24% 6.05M 22s 63050K .......... .......... .......... .......... .......... 24% 6.05M 22s 63100K .......... .......... .......... .......... .......... 24% 5.42M 22s 63150K .......... .......... .......... .......... .......... 24% 5.03M 22s 63200K .......... .......... .......... .......... .......... 24% 6.11M 22s 63250K .......... .......... .......... .......... .......... 24% 24.7M 22s 63300K .......... .......... .......... .......... .......... 24% 12.0M 22s 63350K .......... .......... .......... .......... .......... 24% 17.6M 22s 63400K .......... .......... .......... .......... .......... 24% 17.4M 22s 63450K .......... .......... .......... .......... .......... 24% 10.9M 22s 63500K .......... .......... .......... .......... .......... 24% 20.3M 22s 63550K .......... .......... .......... .......... .......... 24% 18.3M 22s 63600K .......... .......... .......... .......... .......... 24% 7.39M 22s 63650K .......... .......... .......... .......... .......... 24% 17.3M 22s 63700K .......... .......... .......... .......... .......... 24% 9.77M 22s 63750K .......... .......... .......... .......... .......... 24% 9.46M 22s 63800K .......... .......... .......... .......... .......... 24% 10.7M 22s 63850K .......... .......... .......... .......... .......... 24% 6.19M 22s 63900K .......... .......... .......... .......... .......... 24% 4.77M 22s 63950K .......... .......... .......... .......... .......... 24% 8.47M 22s 64000K .......... .......... .......... .......... .......... 24% 8.09M 22s 64050K .......... .......... .......... .......... .......... 24% 5.97M 22s 64100K .......... .......... .......... .......... .......... 24% 6.63M 22s 64150K .......... .......... .......... .......... .......... 24% 6.07M 22s 64200K .......... .......... .......... .......... .......... 24% 4.33M 22s 64250K .......... .......... .......... .......... .......... 24% 4.60M 22s 64300K .......... .......... .......... .......... .......... 24% 10.3M 22s 64350K .......... .......... .......... .......... .......... 24% 10.2M 22s 64400K .......... .......... .......... .......... .......... 24% 8.66M 22s 64450K .......... .......... .......... .......... .......... 24% 7.01M 22s 64500K .......... .......... .......... .......... .......... 24% 7.55M 22s 64550K .......... .......... .......... .......... .......... 24% 7.59M 22s 64600K .......... .......... .......... .......... .......... 24% 6.16M 22s 64650K .......... .......... .......... .......... .......... 24% 6.32M 22s 64700K .......... .......... .......... .......... .......... 24% 5.90M 22s 64750K .......... .......... .......... .......... .......... 24% 7.21M 22s 64800K .......... .......... .......... .......... .......... 24% 7.63M 22s 64850K .......... .......... .......... .......... .......... 24% 4.69M 22s 64900K .......... .......... .......... .......... .......... 24% 4.85M 22s 64950K .......... .......... .......... .......... .......... 24% 4.68M 22s 65000K .......... .......... .......... .......... .......... 24% 4.96M 22s 65050K .......... .......... .......... .......... .......... 24% 3.39M 22s 65100K .......... .......... .......... .......... .......... 24% 1.72M 22s 65150K .......... .......... .......... .......... .......... 24% 2.60M 22s 65200K .......... .......... .......... .......... .......... 24% 5.48M 22s 65250K .......... .......... .......... .......... .......... 24% 7.39M 22s 65300K .......... .......... .......... .......... .......... 24% 6.33M 22s 65350K .......... .......... .......... .......... .......... 24% 6.53M 22s 65400K .......... .......... .......... .......... .......... 24% 8.10M 22s 65450K .......... .......... .......... .......... .......... 24% 11.5M 22s 65500K .......... .......... .......... .......... .......... 25% 10.1M 22s 65550K .......... .......... .......... .......... .......... 25% 10.3M 22s 65600K .......... .......... .......... .......... .......... 25% 9.58M 22s 65650K .......... .......... .......... .......... .......... 25% 9.09M 22s 65700K .......... .......... .......... .......... .......... 25% 9.22M 22s 65750K .......... .......... .......... .......... .......... 25% 8.40M 22s 65800K .......... .......... .......... .......... .......... 25% 9.33M 22s 65850K .......... .......... .......... .......... .......... 25% 9.08M 22s 65900K .......... .......... .......... .......... .......... 25% 8.59M 22s 65950K .......... .......... .......... .......... .......... 25% 8.27M 22s 66000K .......... .......... .......... .......... .......... 25% 5.88M 22s 66050K .......... .......... .......... .......... .......... 25% 3.68M 22s 66100K .......... .......... .......... .......... .......... 25% 4.22M 22s 66150K .......... .......... .......... .......... .......... 25% 4.58M 22s 66200K .......... .......... .......... .......... .......... 25% 4.87M 22s 66250K .......... .......... .......... .......... .......... 25% 7.08M 22s 66300K .......... .......... .......... .......... .......... 25% 10.0M 22s 66350K .......... .......... .......... .......... .......... 25% 6.72M 22s 66400K .......... .......... .......... .......... .......... 25% 4.81M 22s 66450K .......... .......... .......... .......... .......... 25% 5.44M 22s 66500K .......... .......... .......... .......... .......... 25% 8.18M 22s 66550K .......... .......... .......... .......... .......... 25% 5.36M 22s 66600K .......... .......... .......... .......... .......... 25% 3.78M 22s 66650K .......... .......... .......... .......... .......... 25% 5.44M 22s 66700K .......... .......... .......... .......... .......... 25% 6.74M 22s 66750K .......... .......... .......... .......... .......... 25% 13.5M 22s 66800K .......... .......... .......... .......... .......... 25% 19.5M 22s 66850K .......... .......... .......... .......... .......... 25% 9.85M 22s 66900K .......... .......... .......... .......... .......... 25% 15.6M 22s 66950K .......... .......... .......... .......... .......... 25% 8.43M 22s 67000K .......... .......... .......... .......... .......... 25% 8.01M 22s 67050K .......... .......... .......... .......... .......... 25% 9.62M 22s 67100K .......... .......... .......... .......... .......... 25% 6.07M 22s 67150K .......... .......... .......... .......... .......... 25% 6.54M 22s 67200K .......... .......... .......... .......... .......... 25% 8.46M 22s 67250K .......... .......... .......... .......... .......... 25% 11.0M 22s 67300K .......... .......... .......... .......... .......... 25% 6.34M 22s 67350K .......... .......... .......... .......... .......... 25% 4.27M 22s 67400K .......... .......... .......... .......... .......... 25% 7.19M 22s 67450K .......... .......... .......... .......... .......... 25% 4.57M 22s 67500K .......... .......... .......... .......... .......... 25% 5.07M 22s 67550K .......... .......... .......... .......... .......... 25% 5.60M 22s 67600K .......... .......... .......... .......... .......... 25% 8.75M 22s 67650K .......... .......... .......... .......... .......... 25% 13.9M 22s 67700K .......... .......... .......... .......... .......... 25% 12.6M 22s 67750K .......... .......... .......... .......... .......... 25% 13.8M 22s 67800K .......... .......... .......... .......... .......... 25% 14.8M 22s 67850K .......... .......... .......... .......... .......... 25% 10.2M 22s 67900K .......... .......... .......... .......... .......... 25% 22.6M 22s 67950K .......... .......... .......... .......... .......... 25% 6.26M 22s 68000K .......... .......... .......... .......... .......... 25% 15.4M 22s 68050K .......... .......... .......... .......... .......... 25% 7.93M 22s 68100K .......... .......... .......... .......... .......... 25% 7.48M 22s 68150K .......... .......... .......... .......... .......... 26% 7.61M 22s 68200K .......... .......... .......... .......... .......... 26% 3.62M 22s 68250K .......... .......... .......... .......... .......... 26% 2.59M 22s 68300K .......... .......... .......... .......... .......... 26% 3.15M 22s 68350K .......... .......... .......... .......... .......... 26% 2.97M 22s 68400K .......... .......... .......... .......... .......... 26% 6.50M 22s 68450K .......... .......... .......... .......... .......... 26% 6.92M 22s 68500K .......... .......... .......... .......... .......... 26% 7.18M 22s 68550K .......... .......... .......... .......... .......... 26% 7.87M 22s 68600K .......... .......... .......... .......... .......... 26% 5.51M 22s 68650K .......... .......... .......... .......... .......... 26% 7.81M 22s 68700K .......... .......... .......... .......... .......... 26% 7.13M 22s 68750K .......... .......... .......... .......... .......... 26% 6.35M 22s 68800K .......... .......... .......... .......... .......... 26% 6.07M 22s 68850K .......... .......... .......... .......... .......... 26% 4.55M 22s 68900K .......... .......... .......... .......... .......... 26% 4.15M 22s 68950K .......... .......... .......... .......... .......... 26% 4.21M 22s 69000K .......... .......... .......... .......... .......... 26% 5.64M 22s 69050K .......... .......... .......... .......... .......... 26% 10.3M 22s 69100K .......... .......... .......... .......... .......... 26% 7.03M 22s 69150K .......... .......... .......... .......... .......... 26% 5.63M 22s 69200K .......... .......... .......... .......... .......... 26% 4.72M 22s 69250K .......... .......... .......... .......... .......... 26% 6.42M 22s 69300K .......... .......... .......... .......... .......... 26% 6.46M 22s 69350K .......... .......... .......... .......... .......... 26% 6.11M 22s 69400K .......... .......... .......... .......... .......... 26% 16.7M 22s 69450K .......... .......... .......... .......... .......... 26% 7.99M 22s 69500K .......... .......... .......... .......... .......... 26% 13.2M 22s 69550K .......... .......... .......... .......... .......... 26% 7.97M 22s 69600K .......... .......... .......... .......... .......... 26% 6.04M 22s 69650K .......... .......... .......... .......... .......... 26% 7.15M 22s 69700K .......... .......... .......... .......... .......... 26% 8.61M 22s 69750K .......... .......... .......... .......... .......... 26% 6.69M 22s 69800K .......... .......... .......... .......... .......... 26% 5.90M 22s 69850K .......... .......... .......... .......... .......... 26% 12.3M 22s 69900K .......... .......... .......... .......... .......... 26% 19.4M 22s 69950K .......... .......... .......... .......... .......... 26% 10.7M 22s 70000K .......... .......... .......... .......... .......... 26% 8.74M 22s 70050K .......... .......... .......... .......... .......... 26% 14.8M 22s 70100K .......... .......... .......... .......... .......... 26% 12.1M 22s 70150K .......... .......... .......... .......... .......... 26% 16.0M 22s 70200K .......... .......... .......... .......... .......... 26% 10.7M 22s 70250K .......... .......... .......... .......... .......... 26% 12.0M 22s 70300K .......... .......... .......... .......... .......... 26% 7.61M 22s 70350K .......... .......... .......... .......... .......... 26% 7.70M 22s 70400K .......... .......... .......... .......... .......... 26% 9.16M 22s 70450K .......... .......... .......... .......... .......... 26% 8.71M 22s 70500K .......... .......... .......... .......... .......... 26% 9.56M 22s 70550K .......... .......... .......... .......... .......... 26% 19.0M 22s 70600K .......... .......... .......... .......... .......... 26% 11.9M 22s 70650K .......... .......... .......... .......... .......... 26% 13.0M 22s 70700K .......... .......... .......... .......... .......... 26% 16.3M 22s 70750K .......... .......... .......... .......... .......... 27% 13.2M 22s 70800K .......... .......... .......... .......... .......... 27% 16.8M 22s 70850K .......... .......... .......... .......... .......... 27% 8.21M 22s 70900K .......... .......... .......... .......... .......... 27% 18.9M 22s 70950K .......... .......... .......... .......... .......... 27% 10.1M 22s 71000K .......... .......... .......... .......... .......... 27% 12.2M 22s 71050K .......... .......... .......... .......... .......... 27% 20.3M 22s 71100K .......... .......... .......... .......... .......... 27% 18.6M 22s 71150K .......... .......... .......... .......... .......... 27% 13.5M 22s 71200K .......... .......... .......... .......... .......... 27% 20.9M 22s 71250K .......... .......... .......... .......... .......... 27% 18.7M 22s 71300K .......... .......... .......... .......... .......... 27% 21.5M 22s 71350K .......... .......... .......... .......... .......... 27% 14.4M 22s 71400K .......... .......... .......... .......... .......... 27% 16.7M 22s 71450K .......... .......... .......... .......... .......... 27% 11.6M 22s 71500K .......... .......... .......... .......... .......... 27% 15.4M 22s 71550K .......... .......... .......... .......... .......... 27% 14.3M 22s 71600K .......... .......... .......... .......... .......... 27% 12.3M 22s 71650K .......... .......... .......... .......... .......... 27% 14.9M 22s 71700K .......... .......... .......... .......... .......... 27% 14.6M 22s 71750K .......... .......... .......... .......... .......... 27% 12.9M 22s 71800K .......... .......... .......... .......... .......... 27% 15.9M 22s 71850K .......... .......... .......... .......... .......... 27% 17.4M 22s 71900K .......... .......... .......... .......... .......... 27% 5.86M 22s 71950K .......... .......... .......... .......... .......... 27% 105M 22s 72000K .......... .......... .......... .......... .......... 27% 22.5M 22s 72050K .......... .......... .......... .......... .......... 27% 50.7M 22s 72100K .......... .......... .......... .......... .......... 27% 107M 22s 72150K .......... .......... .......... .......... .......... 27% 31.7M 22s 72200K .......... .......... .......... .......... .......... 27% 23.8M 22s 72250K .......... .......... .......... .......... .......... 27% 17.6M 22s 72300K .......... .......... .......... .......... .......... 27% 65.3M 22s 72350K .......... .......... .......... .......... .......... 27% 19.6M 22s 72400K .......... .......... .......... .......... .......... 27% 30.6M 22s 72450K .......... .......... .......... .......... .......... 27% 16.3M 22s 72500K .......... .......... .......... .......... .......... 27% 12.1M 22s 72550K .......... .......... .......... .......... .......... 27% 9.53M 22s 72600K .......... .......... .......... .......... .......... 27% 6.30M 22s 72650K .......... .......... .......... .......... .......... 27% 7.47M 22s 72700K .......... .......... .......... .......... .......... 27% 5.00M 22s 72750K .......... .......... .......... .......... .......... 27% 5.13M 22s 72800K .......... .......... .......... .......... .......... 27% 5.14M 22s 72850K .......... .......... .......... .......... .......... 27% 4.34M 22s 72900K .......... .......... .......... .......... .......... 27% 11.3M 22s 72950K .......... .......... .......... .......... .......... 27% 7.61M 22s 73000K .......... .......... .......... .......... .......... 27% 9.18M 22s 73050K .......... .......... .......... .......... .......... 27% 8.50M 22s 73100K .......... .......... .......... .......... .......... 27% 8.77M 22s 73150K .......... .......... .......... .......... .......... 27% 9.17M 22s 73200K .......... .......... .......... .......... .......... 27% 6.88M 22s 73250K .......... .......... .......... .......... .......... 27% 5.69M 22s 73300K .......... .......... .......... .......... .......... 27% 15.3M 22s 73350K .......... .......... .......... .......... .......... 27% 12.6M 21s 73400K .......... .......... .......... .......... .......... 28% 26.4M 21s 73450K .......... .......... .......... .......... .......... 28% 14.7M 21s 73500K .......... .......... .......... .......... .......... 28% 25.2M 21s 73550K .......... .......... .......... .......... .......... 28% 26.7M 21s 73600K .......... .......... .......... .......... .......... 28% 16.6M 21s 73650K .......... .......... .......... .......... .......... 28% 29.9M 21s 73700K .......... .......... .......... .......... .......... 28% 24.8M 21s 73750K .......... .......... .......... .......... .......... 28% 32.2M 21s 73800K .......... .......... .......... .......... .......... 28% 17.2M 21s 73850K .......... .......... .......... .......... .......... 28% 28.7M 21s 73900K .......... .......... .......... .......... .......... 28% 29.6M 21s 73950K .......... .......... .......... .......... .......... 28% 16.7M 21s 74000K .......... .......... .......... .......... .......... 28% 24.3M 21s 74050K .......... .......... .......... .......... .......... 28% 24.8M 21s 74100K .......... .......... .......... .......... .......... 28% 22.9M 21s 74150K .......... .......... .......... .......... .......... 28% 13.2M 21s 74200K .......... .......... .......... .......... .......... 28% 26.7M 21s 74250K .......... .......... .......... .......... .......... 28% 12.3M 21s 74300K .......... .......... .......... .......... .......... 28% 20.1M 21s 74350K .......... .......... .......... .......... .......... 28% 13.6M 21s 74400K .......... .......... .......... .......... .......... 28% 10.4M 21s 74450K .......... .......... .......... .......... .......... 28% 7.58M 21s 74500K .......... .......... .......... .......... .......... 28% 8.50M 21s 74550K .......... .......... .......... .......... .......... 28% 7.66M 21s 74600K .......... .......... .......... .......... .......... 28% 5.79M 21s 74650K .......... .......... .......... .......... .......... 28% 9.09M 21s 74700K .......... .......... .......... .......... .......... 28% 7.03M 21s 74750K .......... .......... .......... .......... .......... 28% 7.15M 21s 74800K .......... .......... .......... .......... .......... 28% 5.33M 21s 74850K .......... .......... .......... .......... .......... 28% 3.10M 21s 74900K .......... .......... .......... .......... .......... 28% 3.28M 21s 74950K .......... .......... .......... .......... .......... 28% 5.01M 21s 75000K .......... .......... .......... .......... .......... 28% 22.2M 21s 75050K .......... .......... .......... .......... .......... 28% 16.5M 21s 75100K .......... .......... .......... .......... .......... 28% 19.3M 21s 75150K .......... .......... .......... .......... .......... 28% 16.4M 21s 75200K .......... .......... .......... .......... .......... 28% 11.5M 21s 75250K .......... .......... .......... .......... .......... 28% 26.4M 21s 75300K .......... .......... .......... .......... .......... 28% 12.5M 21s 75350K .......... .......... .......... .......... .......... 28% 13.8M 21s 75400K .......... .......... .......... .......... .......... 28% 8.97M 21s 75450K .......... .......... .......... .......... .......... 28% 9.90M 21s 75500K .......... .......... .......... .......... .......... 28% 10.6M 21s 75550K .......... .......... .......... .......... .......... 28% 11.6M 21s 75600K .......... .......... .......... .......... .......... 28% 10.7M 21s 75650K .......... .......... .......... .......... .......... 28% 10.7M 21s 75700K .......... .......... .......... .......... .......... 28% 9.16M 21s 75750K .......... .......... .......... .......... .......... 28% 14.5M 21s 75800K .......... .......... .......... .......... .......... 28% 11.8M 21s 75850K .......... .......... .......... .......... .......... 28% 10.6M 21s 75900K .......... .......... .......... .......... .......... 28% 15.1M 21s 75950K .......... .......... .......... .......... .......... 28% 11.7M 21s 76000K .......... .......... .......... .......... .......... 29% 20.7M 21s 76050K .......... .......... .......... .......... .......... 29% 26.2M 21s 76100K .......... .......... .......... .......... .......... 29% 14.5M 21s 76150K .......... .......... .......... .......... .......... 29% 13.1M 21s 76200K .......... .......... .......... .......... .......... 29% 14.2M 21s 76250K .......... .......... .......... .......... .......... 29% 14.8M 21s 76300K .......... .......... .......... .......... .......... 29% 9.40M 21s 76350K .......... .......... .......... .......... .......... 29% 9.41M 21s 76400K .......... .......... .......... .......... .......... 29% 10.5M 21s 76450K .......... .......... .......... .......... .......... 29% 8.71M 21s 76500K .......... .......... .......... .......... .......... 29% 6.50M 21s 76550K .......... .......... .......... .......... .......... 29% 6.14M 21s 76600K .......... .......... .......... .......... .......... 29% 5.22M 21s 76650K .......... .......... .......... .......... .......... 29% 5.44M 21s 76700K .......... .......... .......... .......... .......... 29% 3.67M 21s 76750K .......... .......... .......... .......... .......... 29% 4.75M 21s 76800K .......... .......... .......... .......... .......... 29% 5.00M 21s 76850K .......... .......... .......... .......... .......... 29% 5.61M 21s 76900K .......... .......... .......... .......... .......... 29% 12.1M 21s 76950K .......... .......... .......... .......... .......... 29% 11.8M 21s 77000K .......... .......... .......... .......... .......... 29% 9.42M 21s 77050K .......... .......... .......... .......... .......... 29% 13.3M 21s 77100K .......... .......... .......... .......... .......... 29% 8.96M 21s 77150K .......... .......... .......... .......... .......... 29% 12.7M 21s 77200K .......... .......... .......... .......... .......... 29% 9.04M 21s 77250K .......... .......... .......... .......... .......... 29% 11.5M 21s 77300K .......... .......... .......... .......... .......... 29% 11.5M 21s 77350K .......... .......... .......... .......... .......... 29% 6.57M 21s 77400K .......... .......... .......... .......... .......... 29% 5.29M 21s 77450K .......... .......... .......... .......... .......... 29% 5.73M 21s 77500K .......... .......... .......... .......... .......... 29% 7.37M 21s 77550K .......... .......... .......... .......... .......... 29% 7.27M 21s 77600K .......... .......... .......... .......... .......... 29% 5.10M 21s 77650K .......... .......... .......... .......... .......... 29% 14.7M 21s 77700K .......... .......... .......... .......... .......... 29% 16.0M 21s 77750K .......... .......... .......... .......... .......... 29% 31.0M 21s 77800K .......... .......... .......... .......... .......... 29% 20.3M 21s 77850K .......... .......... .......... .......... .......... 29% 15.2M 21s 77900K .......... .......... .......... .......... .......... 29% 17.6M 21s 77950K .......... .......... .......... .......... .......... 29% 14.6M 21s 78000K .......... .......... .......... .......... .......... 29% 12.1M 21s 78050K .......... .......... .......... .......... .......... 29% 8.40M 21s 78100K .......... .......... .......... .......... .......... 29% 10.8M 21s 78150K .......... .......... .......... .......... .......... 29% 10.6M 21s 78200K .......... .......... .......... .......... .......... 29% 10.7M 21s 78250K .......... .......... .......... .......... .......... 29% 13.1M 21s 78300K .......... .......... .......... .......... .......... 29% 9.90M 21s 78350K .......... .......... .......... .......... .......... 29% 7.90M 21s 78400K .......... .......... .......... .......... .......... 29% 12.2M 21s 78450K .......... .......... .......... .......... .......... 29% 8.41M 21s 78500K .......... .......... .......... .......... .......... 29% 10.9M 21s 78550K .......... .......... .......... .......... .......... 29% 10.9M 21s 78600K .......... .......... .......... .......... .......... 29% 7.23M 21s 78650K .......... .......... .......... .......... .......... 30% 8.75M 21s 78700K .......... .......... .......... .......... .......... 30% 4.42M 21s 78750K .......... .......... .......... .......... .......... 30% 6.37M 21s 78800K .......... .......... .......... .......... .......... 30% 6.38M 21s 78850K .......... .......... .......... .......... .......... 30% 5.67M 21s 78900K .......... .......... .......... .......... .......... 30% 11.0M 21s 78950K .......... .......... .......... .......... .......... 30% 9.31M 21s 79000K .......... .......... .......... .......... .......... 30% 10.2M 21s 79050K .......... .......... .......... .......... .......... 30% 10.4M 21s 79100K .......... .......... .......... .......... .......... 30% 7.40M 21s 79150K .......... .......... .......... .......... .......... 30% 15.8M 21s 79200K .......... .......... .......... .......... .......... 30% 14.9M 21s 79250K .......... .......... .......... .......... .......... 30% 21.2M 21s 79300K .......... .......... .......... .......... .......... 30% 16.2M 21s 79350K .......... .......... .......... .......... .......... 30% 16.5M 21s 79400K .......... .......... .......... .......... .......... 30% 16.4M 21s 79450K .......... .......... .......... .......... .......... 30% 16.4M 21s 79500K .......... .......... .......... .......... .......... 30% 18.9M 21s 79550K .......... .......... .......... .......... .......... 30% 13.1M 21s 79600K .......... .......... .......... .......... .......... 30% 15.7M 21s 79650K .......... .......... .......... .......... .......... 30% 14.9M 21s 79700K .......... .......... .......... .......... .......... 30% 7.73M 21s 79750K .......... .......... .......... .......... .......... 30% 36.2M 21s 79800K .......... .......... .......... .......... .......... 30% 30.7M 21s 79850K .......... .......... .......... .......... .......... 30% 7.37M 21s 79900K .......... .......... .......... .......... .......... 30% 13.8M 20s 79950K .......... .......... .......... .......... .......... 30% 13.7M 20s 80000K .......... .......... .......... .......... .......... 30% 17.1M 20s 80050K .......... .......... .......... .......... .......... 30% 18.5M 20s 80100K .......... .......... .......... .......... .......... 30% 16.7M 20s 80150K .......... .......... .......... .......... .......... 30% 15.7M 20s 80200K .......... .......... .......... .......... .......... 30% 13.7M 20s 80250K .......... .......... .......... .......... .......... 30% 9.34M 20s 80300K .......... .......... .......... .......... .......... 30% 11.9M 20s 80350K .......... .......... .......... .......... .......... 30% 11.3M 20s 80400K .......... .......... .......... .......... .......... 30% 9.58M 20s 80450K .......... .......... .......... .......... .......... 30% 12.1M 20s 80500K .......... .......... .......... .......... .......... 30% 12.5M 20s 80550K .......... .......... .......... .......... .......... 30% 9.00M 20s 80600K .......... .......... .......... .......... .......... 30% 3.97M 20s 80650K .......... .......... .......... .......... .......... 30% 225K 21s 80700K .......... .......... .......... .......... .......... 30% 4.38M 21s 80750K .......... .......... .......... .......... .......... 30% 5.60M 21s 80800K .......... .......... .......... .......... .......... 30% 135M 21s 80850K .......... .......... .......... .......... .......... 30% 14.9M 21s 80900K .......... .......... .......... .......... .......... 30% 12.0M 21s 80950K .......... .......... .......... .......... .......... 30% 12.4M 21s 81000K .......... .......... .......... .......... .......... 30% 11.4M 21s 81050K .......... .......... .......... .......... .......... 30% 10.4M 21s 81100K .......... .......... .......... .......... .......... 30% 7.34M 21s 81150K .......... .......... .......... .......... .......... 30% 6.47M 21s 81200K .......... .......... .......... .......... .......... 30% 5.85M 21s 81250K .......... .......... .......... .......... .......... 31% 5.88M 21s 81300K .......... .......... .......... .......... .......... 31% 6.31M 21s 81350K .......... .......... .......... .......... .......... 31% 16.1M 21s 81400K .......... .......... .......... .......... .......... 31% 19.1M 21s 81450K .......... .......... .......... .......... .......... 31% 23.8M 21s 81500K .......... .......... .......... .......... .......... 31% 32.9M 21s 81550K .......... .......... .......... .......... .......... 31% 15.4M 21s 81600K .......... .......... .......... .......... .......... 31% 34.1M 21s 81650K .......... .......... .......... .......... .......... 31% 23.0M 21s 81700K .......... .......... .......... .......... .......... 31% 12.1M 21s 81750K .......... .......... .......... .......... .......... 31% 10.8M 21s 81800K .......... .......... .......... .......... .......... 31% 17.3M 21s 81850K .......... .......... .......... .......... .......... 31% 8.37M 21s 81900K .......... .......... .......... .......... .......... 31% 34.3M 21s 81950K .......... .......... .......... .......... .......... 31% 10.7M 21s 82000K .......... .......... .......... .......... .......... 31% 17.2M 21s 82050K .......... .......... .......... .......... .......... 31% 16.2M 21s 82100K .......... .......... .......... .......... .......... 31% 12.0M 21s 82150K .......... .......... .......... .......... .......... 31% 16.2M 21s 82200K .......... .......... .......... .......... .......... 31% 25.3M 21s 82250K .......... .......... .......... .......... .......... 31% 15.2M 21s 82300K .......... .......... .......... .......... .......... 31% 28.5M 21s 82350K .......... .......... .......... .......... .......... 31% 11.9M 21s 82400K .......... .......... .......... .......... .......... 31% 14.6M 21s 82450K .......... .......... .......... .......... .......... 31% 9.76M 21s 82500K .......... .......... .......... .......... .......... 31% 16.6M 21s 82550K .......... .......... .......... .......... .......... 31% 13.7M 21s 82600K .......... .......... .......... .......... .......... 31% 17.7M 20s 82650K .......... .......... .......... .......... .......... 31% 22.0M 20s 82700K .......... .......... .......... .......... .......... 31% 16.6M 20s 82750K .......... .......... .......... .......... .......... 31% 21.1M 20s 82800K .......... .......... .......... .......... .......... 31% 19.2M 20s 82850K .......... .......... .......... .......... .......... 31% 12.9M 20s 82900K .......... .......... .......... .......... .......... 31% 14.5M 20s 82950K .......... .......... .......... .......... .......... 31% 14.0M 20s 83000K .......... .......... .......... .......... .......... 31% 6.66M 20s 83050K .......... .......... .......... .......... .......... 31% 20.0M 20s 83100K .......... .......... .......... .......... .......... 31% 8.86M 20s 83150K .......... .......... .......... .......... .......... 31% 10.2M 20s 83200K .......... .......... .......... .......... .......... 31% 7.93M 20s 83250K .......... .......... .......... .......... .......... 31% 8.11M 20s 83300K .......... .......... .......... .......... .......... 31% 6.62M 20s 83350K .......... .......... .......... .......... .......... 31% 4.49M 20s 83400K .......... .......... .......... .......... .......... 31% 4.95M 20s 83450K .......... .......... .......... .......... .......... 31% 3.46M 20s 83500K .......... .......... .......... .......... .......... 31% 5.79M 20s 83550K .......... .......... .......... .......... .......... 31% 6.59M 20s 83600K .......... .......... .......... .......... .......... 31% 7.74M 20s 83650K .......... .......... .......... .......... .......... 31% 9.99M 20s 83700K .......... .......... .......... .......... .......... 31% 7.23M 20s 83750K .......... .......... .......... .......... .......... 31% 8.18M 20s 83800K .......... .......... .......... .......... .......... 31% 7.61M 20s 83850K .......... .......... .......... .......... .......... 31% 5.82M 20s 83900K .......... .......... .......... .......... .......... 32% 7.54M 20s 83950K .......... .......... .......... .......... .......... 32% 6.58M 20s 84000K .......... .......... .......... .......... .......... 32% 7.47M 20s 84050K .......... .......... .......... .......... .......... 32% 7.14M 20s 84100K .......... .......... .......... .......... .......... 32% 5.58M 20s 84150K .......... .......... .......... .......... .......... 32% 6.07M 20s 84200K .......... .......... .......... .......... .......... 32% 7.50M 20s 84250K .......... .......... .......... .......... .......... 32% 6.69M 20s 84300K .......... .......... .......... .......... .......... 32% 5.32M 20s 84350K .......... .......... .......... .......... .......... 32% 6.16M 20s 84400K .......... .......... .......... .......... .......... 32% 4.88M 20s 84450K .......... .......... .......... .......... .......... 32% 759K 20s 84500K .......... .......... .......... .......... .......... 32% 2.31M 20s 84550K .......... .......... .......... .......... .......... 32% 7.75M 20s 84600K .......... .......... .......... .......... .......... 32% 7.13M 20s 84650K .......... .......... .......... .......... .......... 32% 11.3M 20s 84700K .......... .......... .......... .......... .......... 32% 5.88M 20s 84750K .......... .......... .......... .......... .......... 32% 8.73M 20s 84800K .......... .......... .......... .......... .......... 32% 9.13M 20s 84850K .......... .......... .......... .......... .......... 32% 6.53M 20s 84900K .......... .......... .......... .......... .......... 32% 7.62M 20s 84950K .......... .......... .......... .......... .......... 32% 6.18M 20s 85000K .......... .......... .......... .......... .......... 32% 6.16M 20s 85050K .......... .......... .......... .......... .......... 32% 4.92M 20s 85100K .......... .......... .......... .......... .......... 32% 6.05M 20s 85150K .......... .......... .......... .......... .......... 32% 5.85M 20s 85200K .......... .......... .......... .......... .......... 32% 6.83M 20s 85250K .......... .......... .......... .......... .......... 32% 9.64M 20s 85300K .......... .......... .......... .......... .......... 32% 5.66M 20s 85350K .......... .......... .......... .......... .......... 32% 3.67M 20s 85400K .......... .......... .......... .......... .......... 32% 3.07M 20s 85450K .......... .......... .......... .......... .......... 32% 2.53M 20s 85500K .......... .......... .......... .......... .......... 32% 3.86M 21s 85550K .......... .......... .......... .......... .......... 32% 10.1M 20s 85600K .......... .......... .......... .......... .......... 32% 9.29M 20s 85650K .......... .......... .......... .......... .......... 32% 12.7M 20s 85700K .......... .......... .......... .......... .......... 32% 9.94M 20s 85750K .......... .......... .......... .......... .......... 32% 13.7M 20s 85800K .......... .......... .......... .......... .......... 32% 10.9M 20s 85850K .......... .......... .......... .......... .......... 32% 13.1M 20s 85900K .......... .......... .......... .......... .......... 32% 10.3M 20s 85950K .......... .......... .......... .......... .......... 32% 10.9M 20s 86000K .......... .......... .......... .......... .......... 32% 10.5M 20s 86050K .......... .......... .......... .......... .......... 32% 8.06M 20s 86100K .......... .......... .......... .......... .......... 32% 12.0M 20s 86150K .......... .......... .......... .......... .......... 32% 9.18M 20s 86200K .......... .......... .......... .......... .......... 32% 7.46M 20s 86250K .......... .......... .......... .......... .......... 32% 6.76M 20s 86300K .......... .......... .......... .......... .......... 32% 5.45M 20s 86350K .......... .......... .......... .......... .......... 32% 4.72M 20s 86400K .......... .......... .......... .......... .......... 32% 4.86M 20s 86450K .......... .......... .......... .......... .......... 32% 4.73M 20s 86500K .......... .......... .......... .......... .......... 33% 5.81M 20s 86550K .......... .......... .......... .......... .......... 33% 7.20M 20s 86600K .......... .......... .......... .......... .......... 33% 6.40M 20s 86650K .......... .......... .......... .......... .......... 33% 8.49M 20s 86700K .......... .......... .......... .......... .......... 33% 8.75M 20s 86750K .......... .......... .......... .......... .......... 33% 10.2M 20s 86800K .......... .......... .......... .......... .......... 33% 8.11M 20s 86850K .......... .......... .......... .......... .......... 33% 9.71M 20s 86900K .......... .......... .......... .......... .......... 33% 9.37M 20s 86950K .......... .......... .......... .......... .......... 33% 7.03M 20s 87000K .......... .......... .......... .......... .......... 33% 14.0M 20s 87050K .......... .......... .......... .......... .......... 33% 11.5M 20s 87100K .......... .......... .......... .......... .......... 33% 9.02M 20s 87150K .......... .......... .......... .......... .......... 33% 6.83M 20s 87200K .......... .......... .......... .......... .......... 33% 4.35M 20s 87250K .......... .......... .......... .......... .......... 33% 5.81M 20s 87300K .......... .......... .......... .......... .......... 33% 4.06M 20s 87350K .......... .......... .......... .......... .......... 33% 2.58M 20s 87400K .......... .......... .......... .......... .......... 33% 2.53M 20s 87450K .......... .......... .......... .......... .......... 33% 10.4M 20s 87500K .......... .......... .......... .......... .......... 33% 25.2M 20s 87550K .......... .......... .......... .......... .......... 33% 27.4M 20s 87600K .......... .......... .......... .......... .......... 33% 31.0M 20s 87650K .......... .......... .......... .......... .......... 33% 37.1M 20s 87700K .......... .......... .......... .......... .......... 33% 7.24M 20s 87750K .......... .......... .......... .......... .......... 33% 43.1M 20s 87800K .......... .......... .......... .......... .......... 33% 47.8M 20s 87850K .......... .......... .......... .......... .......... 33% 46.7M 20s 87900K .......... .......... .......... .......... .......... 33% 56.1M 20s 87950K .......... .......... .......... .......... .......... 33% 56.8M 20s 88000K .......... .......... .......... .......... .......... 33% 32.6M 20s 88050K .......... .......... .......... .......... .......... 33% 33.2M 20s 88100K .......... .......... .......... .......... .......... 33% 28.3M 20s 88150K .......... .......... .......... .......... .......... 33% 55.3M 20s 88200K .......... .......... .......... .......... .......... 33% 27.5M 20s 88250K .......... .......... .......... .......... .......... 33% 23.0M 20s 88300K .......... .......... .......... .......... .......... 33% 31.0M 20s 88350K .......... .......... .......... .......... .......... 33% 26.4M 20s 88400K .......... .......... .......... .......... .......... 33% 10.7M 20s 88450K .......... .......... .......... .......... .......... 33% 51.8M 20s 88500K .......... .......... .......... .......... .......... 33% 33.0M 20s 88550K .......... .......... .......... .......... .......... 33% 21.7M 20s 88600K .......... .......... .......... .......... .......... 33% 12.9M 20s 88650K .......... .......... .......... .......... .......... 33% 21.4M 20s 88700K .......... .......... .......... .......... .......... 33% 24.2M 20s 88750K .......... .......... .......... .......... .......... 33% 8.57M 20s 88800K .......... .......... .......... .......... .......... 33% 101M 20s 88850K .......... .......... .......... .......... .......... 33% 34.5M 20s 88900K .......... .......... .......... .......... .......... 33% 14.5M 20s 88950K .......... .......... .......... .......... .......... 33% 13.1M 20s 89000K .......... .......... .......... .......... .......... 33% 26.5M 20s 89050K .......... .......... .......... .......... .......... 33% 16.6M 20s 89100K .......... .......... .......... .......... .......... 34% 15.5M 20s 89150K .......... .......... .......... .......... .......... 34% 23.4M 20s 89200K .......... .......... .......... .......... .......... 34% 15.4M 20s 89250K .......... .......... .......... .......... .......... 34% 28.7M 20s 89300K .......... .......... .......... .......... .......... 34% 13.4M 20s 89350K .......... .......... .......... .......... .......... 34% 11.2M 20s 89400K .......... .......... .......... .......... .......... 34% 17.2M 20s 89450K .......... .......... .......... .......... .......... 34% 8.71M 20s 89500K .......... .......... .......... .......... .......... 34% 16.7M 20s 89550K .......... .......... .......... .......... .......... 34% 16.3M 20s 89600K .......... .......... .......... .......... .......... 34% 16.9M 20s 89650K .......... .......... .......... .......... .......... 34% 19.0M 20s 89700K .......... .......... .......... .......... .......... 34% 14.6M 20s 89750K .......... .......... .......... .......... .......... 34% 19.8M 20s 89800K .......... .......... .......... .......... .......... 34% 17.8M 20s 89850K .......... .......... .......... .......... .......... 34% 9.97M 20s 89900K .......... .......... .......... .......... .......... 34% 30.8M 20s 89950K .......... .......... .......... .......... .......... 34% 11.7M 20s 90000K .......... .......... .......... .......... .......... 34% 21.3M 20s 90050K .......... .......... .......... .......... .......... 34% 17.9M 20s 90100K .......... .......... .......... .......... .......... 34% 14.6M 20s 90150K .......... .......... .......... .......... .......... 34% 18.1M 20s 90200K .......... .......... .......... .......... .......... 34% 15.4M 20s 90250K .......... .......... .......... .......... .......... 34% 16.2M 20s 90300K .......... .......... .......... .......... .......... 34% 15.4M 20s 90350K .......... .......... .......... .......... .......... 34% 13.5M 20s 90400K .......... .......... .......... .......... .......... 34% 16.2M 20s 90450K .......... .......... .......... .......... .......... 34% 12.8M 20s 90500K .......... .......... .......... .......... .......... 34% 14.4M 20s 90550K .......... .......... .......... .......... .......... 34% 14.1M 20s 90600K .......... .......... .......... .......... .......... 34% 13.4M 20s 90650K .......... .......... .......... .......... .......... 34% 12.8M 20s 90700K .......... .......... .......... .......... .......... 34% 14.1M 20s 90750K .......... .......... .......... .......... .......... 34% 17.3M 20s 90800K .......... .......... .......... .......... .......... 34% 13.8M 20s 90850K .......... .......... .......... .......... .......... 34% 10.5M 20s 90900K .......... .......... .......... .......... .......... 34% 13.2M 20s 90950K .......... .......... .......... .......... .......... 34% 12.5M 20s 91000K .......... .......... .......... .......... .......... 34% 11.6M 20s 91050K .......... .......... .......... .......... .......... 34% 11.8M 20s 91100K .......... .......... .......... .......... .......... 34% 11.5M 20s 91150K .......... .......... .......... .......... .......... 34% 8.96M 20s 91200K .......... .......... .......... .......... .......... 34% 15.0M 20s 91250K .......... .......... .......... .......... .......... 34% 6.94M 20s 91300K .......... .......... .......... .......... .......... 34% 51.4M 19s 91350K .......... .......... .......... .......... .......... 34% 7.59M 19s 91400K .......... .......... .......... .......... .......... 34% 8.90M 19s 91450K .......... .......... .......... .......... .......... 34% 5.45M 19s 91500K .......... .......... .......... .......... .......... 34% 6.62M 19s 91550K .......... .......... .......... .......... .......... 34% 5.56M 19s 91600K .......... .......... .......... .......... .......... 34% 5.52M 19s 91650K .......... .......... .......... .......... .......... 34% 5.30M 19s 91700K .......... .......... .......... .......... .......... 34% 5.62M 19s 91750K .......... .......... .......... .......... .......... 35% 8.73M 19s 91800K .......... .......... .......... .......... .......... 35% 9.01M 19s 91850K .......... .......... .......... .......... .......... 35% 6.45M 19s 91900K .......... .......... .......... .......... .......... 35% 6.73M 19s 91950K .......... .......... .......... .......... .......... 35% 6.38M 19s 92000K .......... .......... .......... .......... .......... 35% 5.29M 19s 92050K .......... .......... .......... .......... .......... 35% 6.37M 19s 92100K .......... .......... .......... .......... .......... 35% 7.26M 19s 92150K .......... .......... .......... .......... .......... 35% 9.39M 19s 92200K .......... .......... .......... .......... .......... 35% 13.4M 19s 92250K .......... .......... .......... .......... .......... 35% 24.8M 19s 92300K .......... .......... .......... .......... .......... 35% 17.4M 19s 92350K .......... .......... .......... .......... .......... 35% 20.0M 19s 92400K .......... .......... .......... .......... .......... 35% 24.0M 19s 92450K .......... .......... .......... .......... .......... 35% 18.0M 19s 92500K .......... .......... .......... .......... .......... 35% 28.5M 19s 92550K .......... .......... .......... .......... .......... 35% 15.0M 19s 92600K .......... .......... .......... .......... .......... 35% 17.0M 19s 92650K .......... .......... .......... .......... .......... 35% 11.5M 19s 92700K .......... .......... .......... .......... .......... 35% 11.2M 19s 92750K .......... .......... .......... .......... .......... 35% 6.62M 19s 92800K .......... .......... .......... .......... .......... 35% 4.85M 19s 92850K .......... .......... .......... .......... .......... 35% 3.81M 19s 92900K .......... .......... .......... .......... .......... 35% 4.74M 19s 92950K .......... .......... .......... .......... .......... 35% 4.65M 19s 93000K .......... .......... .......... .......... .......... 35% 7.43M 19s 93050K .......... .......... .......... .......... .......... 35% 6.67M 19s 93100K .......... .......... .......... .......... .......... 35% 8.95M 19s 93150K .......... .......... .......... .......... .......... 35% 11.1M 19s 93200K .......... .......... .......... .......... .......... 35% 5.15M 19s 93250K .......... .......... .......... .......... .......... 35% 4.08M 19s 93300K .......... .......... .......... .......... .......... 35% 3.60M 19s 93350K .......... .......... .......... .......... .......... 35% 4.69M 19s 93400K .......... .......... .......... .......... .......... 35% 7.42M 19s 93450K .......... .......... .......... .......... .......... 35% 8.91M 19s 93500K .......... .......... .......... .......... .......... 35% 10.2M 19s 93550K .......... .......... .......... .......... .......... 35% 9.00M 19s 93600K .......... .......... .......... .......... .......... 35% 9.48M 19s 93650K .......... .......... .......... .......... .......... 35% 11.0M 19s 93700K .......... .......... .......... .......... .......... 35% 9.37M 19s 93750K .......... .......... .......... .......... .......... 35% 7.91M 19s 93800K .......... .......... .......... .......... .......... 35% 7.40M 19s 93850K .......... .......... .......... .......... .......... 35% 3.78M 19s 93900K .......... .......... .......... .......... .......... 35% 4.00M 19s 93950K .......... .......... .......... .......... .......... 35% 4.42M 19s 94000K .......... .......... .......... .......... .......... 35% 6.72M 19s 94050K .......... .......... .......... .......... .......... 35% 9.39M 19s 94100K .......... .......... .......... .......... .......... 35% 6.09M 19s 94150K .......... .......... .......... .......... .......... 35% 6.43M 19s 94200K .......... .......... .......... .......... .......... 35% 5.01M 19s 94250K .......... .......... .......... .......... .......... 35% 6.20M 19s 94300K .......... .......... .......... .......... .......... 35% 5.49M 19s 94350K .......... .......... .......... .......... .......... 36% 13.0M 19s 94400K .......... .......... .......... .......... .......... 36% 15.7M 19s 94450K .......... .......... .......... .......... .......... 36% 13.4M 19s 94500K .......... .......... .......... .......... .......... 36% 23.4M 19s 94550K .......... .......... .......... .......... .......... 36% 13.4M 19s 94600K .......... .......... .......... .......... .......... 36% 8.49M 19s 94650K .......... .......... .......... .......... .......... 36% 11.8M 19s 94700K .......... .......... .......... .......... .......... 36% 6.71M 19s 94750K .......... .......... .......... .......... .......... 36% 8.18M 19s 94800K .......... .......... .......... .......... .......... 36% 10.7M 19s 94850K .......... .......... .......... .......... .......... 36% 8.25M 19s 94900K .......... .......... .......... .......... .......... 36% 8.63M 19s 94950K .......... .......... .......... .......... .......... 36% 6.46M 19s 95000K .......... .......... .......... .......... .......... 36% 5.47M 19s 95050K .......... .......... .......... .......... .......... 36% 4.34M 19s 95100K .......... .......... .......... .......... .......... 36% 3.04M 19s 95150K .......... .......... .......... .......... .......... 36% 3.77M 19s 95200K .......... .......... .......... .......... .......... 36% 4.97M 19s 95250K .......... .......... .......... .......... .......... 36% 6.62M 19s 95300K .......... .......... .......... .......... .......... 36% 8.81M 19s 95350K .......... .......... .......... .......... .......... 36% 6.14M 19s 95400K .......... .......... .......... .......... .......... 36% 7.73M 19s 95450K .......... .......... .......... .......... .......... 36% 5.50M 19s 95500K .......... .......... .......... .......... .......... 36% 6.01M 19s 95550K .......... .......... .......... .......... .......... 36% 6.57M 19s 95600K .......... .......... .......... .......... .......... 36% 6.74M 19s 95650K .......... .......... .......... .......... .......... 36% 5.15M 19s 95700K .......... .......... .......... .......... .......... 36% 4.52M 19s 95750K .......... .......... .......... .......... .......... 36% 4.68M 19s 95800K .......... .......... .......... .......... .......... 36% 4.99M 19s 95850K .......... .......... .......... .......... .......... 36% 3.20M 19s 95900K .......... .......... .......... .......... .......... 36% 1.55M 19s 95950K .......... .......... .......... .......... .......... 36% 2.29M 19s 96000K .......... .......... .......... .......... .......... 36% 2.20M 19s 96050K .......... .......... .......... .......... .......... 36% 2.93M 19s 96100K .......... .......... .......... .......... .......... 36% 2.61M 19s 96150K .......... .......... .......... .......... .......... 36% 3.39M 19s 96200K .......... .......... .......... .......... .......... 36% 1.95M 19s 96250K .......... .......... .......... .......... .......... 36% 3.55M 19s 96300K .......... .......... .......... .......... .......... 36% 14.6M 19s 96350K .......... .......... .......... .......... .......... 36% 14.3M 19s 96400K .......... .......... .......... .......... .......... 36% 22.4M 19s 96450K .......... .......... .......... .......... .......... 36% 15.1M 19s 96500K .......... .......... .......... .......... .......... 36% 15.5M 19s 96550K .......... .......... .......... .......... .......... 36% 15.2M 19s 96600K .......... .......... .......... .......... .......... 36% 14.7M 19s 96650K .......... .......... .......... .......... .......... 36% 23.4M 19s 96700K .......... .......... .......... .......... .......... 36% 13.9M 19s 96750K .......... .......... .......... .......... .......... 36% 16.0M 19s 96800K .......... .......... .......... .......... .......... 36% 22.0M 19s 96850K .......... .......... .......... .......... .......... 36% 14.7M 19s 96900K .......... .......... .......... .......... .......... 36% 80.0M 19s 96950K .......... .......... .......... .......... .......... 36% 28.2M 19s 97000K .......... .......... .......... .......... .......... 37% 28.1M 19s 97050K .......... .......... .......... .......... .......... 37% 63.9M 19s 97100K .......... .......... .......... .......... .......... 37% 12.6M 19s 97150K .......... .......... .......... .......... .......... 37% 167M 19s 97200K .......... .......... .......... .......... .......... 37% 43.5M 19s 97250K .......... .......... .......... .......... .......... 37% 50.8M 19s 97300K .......... .......... .......... .......... .......... 37% 12.4M 19s 97350K .......... .......... .......... .......... .......... 37% 95.8M 19s 97400K .......... .......... .......... .......... .......... 37% 236K 19s 97450K .......... .......... .......... .......... .......... 37% 61.8M 19s 97500K .......... .......... .......... .......... .......... 37% 53.6M 19s 97550K .......... .......... .......... .......... .......... 37% 76.7M 19s 97600K .......... .......... .......... .......... .......... 37% 105M 19s 97650K .......... .......... .......... .......... .......... 37% 64.4M 19s 97700K .......... .......... .......... .......... .......... 37% 77.6M 19s 97750K .......... .......... .......... .......... .......... 37% 109M 19s 97800K .......... .......... .......... .......... .......... 37% 6.97M 19s 97850K .......... .......... .......... .......... .......... 37% 31.2M 19s 97900K .......... .......... .......... .......... .......... 37% 19.2M 19s 97950K .......... .......... .......... .......... .......... 37% 6.10M 19s 98000K .......... .......... .......... .......... .......... 37% 8.43M 19s 98050K .......... .......... .......... .......... .......... 37% 7.76M 19s 98100K .......... .......... .......... .......... .......... 37% 3.64M 19s 98150K .......... .......... .......... .......... .......... 37% 4.43M 19s 98200K .......... .......... .......... .......... .......... 37% 3.57M 19s 98250K .......... .......... .......... .......... .......... 37% 6.32M 19s 98300K .......... .......... .......... .......... .......... 37% 13.1M 19s 98350K .......... .......... .......... .......... .......... 37% 8.73M 19s 98400K .......... .......... .......... .......... .......... 37% 8.72M 19s 98450K .......... .......... .......... .......... .......... 37% 6.66M 19s 98500K .......... .......... .......... .......... .......... 37% 5.83M 19s 98550K .......... .......... .......... .......... .......... 37% 6.33M 19s 98600K .......... .......... .......... .......... .......... 37% 3.82M 19s 98650K .......... .......... .......... .......... .......... 37% 5.54M 19s 98700K .......... .......... .......... .......... .......... 37% 4.53M 19s 98750K .......... .......... .......... .......... .......... 37% 10.3M 19s 98800K .......... .......... .......... .......... .......... 37% 15.6M 19s 98850K .......... .......... .......... .......... .......... 37% 8.56M 19s 98900K .......... .......... .......... .......... .......... 37% 11.4M 19s 98950K .......... .......... .......... .......... .......... 37% 7.96M 19s 99000K .......... .......... .......... .......... .......... 37% 8.14M 19s 99050K .......... .......... .......... .......... .......... 37% 9.63M 19s 99100K .......... .......... .......... .......... .......... 37% 6.46M 19s 99150K .......... .......... .......... .......... .......... 37% 8.03M 19s 99200K .......... .......... .......... .......... .......... 37% 5.07M 19s 99250K .......... .......... .......... .......... .......... 37% 3.80M 19s 99300K .......... .......... .......... .......... .......... 37% 4.08M 19s 99350K .......... .......... .......... .......... .......... 37% 3.96M 19s 99400K .......... .......... .......... .......... .......... 37% 6.90M 19s 99450K .......... .......... .......... .......... .......... 37% 7.51M 19s 99500K .......... .......... .......... .......... .......... 37% 6.10M 19s 99550K .......... .......... .......... .......... .......... 37% 6.96M 19s 99600K .......... .......... .......... .......... .......... 38% 4.13M 19s 99650K .......... .......... .......... .......... .......... 38% 3.43M 19s 99700K .......... .......... .......... .......... .......... 38% 2.31M 19s 99750K .......... .......... .......... .......... .......... 38% 2.22M 19s 99800K .......... .......... .......... .......... .......... 38% 4.60M 19s 99850K .......... .......... .......... .......... .......... 38% 9.34M 19s 99900K .......... .......... .......... .......... .......... 38% 9.52M 19s 99950K .......... .......... .......... .......... .......... 38% 5.24M 19s 100000K .......... .......... .......... .......... .......... 38% 5.09M 19s 100050K .......... .......... .......... .......... .......... 38% 5.62M 19s 100100K .......... .......... .......... .......... .......... 38% 4.49M 19s 100150K .......... .......... .......... .......... .......... 38% 3.64M 19s 100200K .......... .......... .......... .......... .......... 38% 3.14M 19s 100250K .......... .......... .......... .......... .......... 38% 3.78M 19s 100300K .......... .......... .......... .......... .......... 38% 4.58M 19s 100350K .......... .......... .......... .......... .......... 38% 9.70M 19s 100400K .......... .......... .......... .......... .......... 38% 12.0M 19s 100450K .......... .......... .......... .......... .......... 38% 10.8M 19s 100500K .......... .......... .......... .......... .......... 38% 12.9M 19s 100550K .......... .......... .......... .......... .......... 38% 7.57M 19s 100600K .......... .......... .......... .......... .......... 38% 14.2M 19s 100650K .......... .......... .......... .......... .......... 38% 5.35M 19s 100700K .......... .......... .......... .......... .......... 38% 4.95M 19s 100750K .......... .......... .......... .......... .......... 38% 761K 19s 100800K .......... .......... .......... .......... .......... 38% 3.82M 19s 100850K .......... .......... .......... .......... .......... 38% 2.74M 19s 100900K .......... .......... .......... .......... .......... 38% 3.28M 19s 100950K .......... .......... .......... .......... .......... 38% 5.96M 19s 101000K .......... .......... .......... .......... .......... 38% 6.46M 19s 101050K .......... .......... .......... .......... .......... 38% 4.11M 19s 101100K .......... .......... .......... .......... .......... 38% 4.64M 19s 101150K .......... .......... .......... .......... .......... 38% 5.14M 19s 101200K .......... .......... .......... .......... .......... 38% 8.04M 19s 101250K .......... .......... .......... .......... .......... 38% 23.0M 19s 101300K .......... .......... .......... .......... .......... 38% 25.8M 19s 101350K .......... .......... .......... .......... .......... 38% 25.6M 19s 101400K .......... .......... .......... .......... .......... 38% 15.8M 19s 101450K .......... .......... .......... .......... .......... 38% 14.2M 19s 101500K .......... .......... .......... .......... .......... 38% 13.5M 19s 101550K .......... .......... .......... .......... .......... 38% 22.3M 19s 101600K .......... .......... .......... .......... .......... 38% 22.1M 19s 101650K .......... .......... .......... .......... .......... 38% 34.8M 19s 101700K .......... .......... .......... .......... .......... 38% 12.9M 19s 101750K .......... .......... .......... .......... .......... 38% 11.2M 19s 101800K .......... .......... .......... .......... .......... 38% 12.3M 19s 101850K .......... .......... .......... .......... .......... 38% 10.9M 19s 101900K .......... .......... .......... .......... .......... 38% 15.8M 19s 101950K .......... .......... .......... .......... .......... 38% 9.15M 19s 102000K .......... .......... .......... .......... .......... 38% 11.9M 19s 102050K .......... .......... .......... .......... .......... 38% 8.74M 19s 102100K .......... .......... .......... .......... .......... 38% 9.49M 19s 102150K .......... .......... .......... .......... .......... 38% 8.67M 19s 102200K .......... .......... .......... .......... .......... 38% 6.52M 19s 102250K .......... .......... .......... .......... .......... 39% 7.31M 19s 102300K .......... .......... .......... .......... .......... 39% 6.75M 19s 102350K .......... .......... .......... .......... .......... 39% 5.45M 19s 102400K .......... .......... .......... .......... .......... 39% 6.94M 19s 102450K .......... .......... .......... .......... .......... 39% 5.82M 19s 102500K .......... .......... .......... .......... .......... 39% 6.64M 19s 102550K .......... .......... .......... .......... .......... 39% 5.89M 19s 102600K .......... .......... .......... .......... .......... 39% 5.51M 19s 102650K .......... .......... .......... .......... .......... 39% 7.37M 19s 102700K .......... .......... .......... .......... .......... 39% 5.54M 19s 102750K .......... .......... .......... .......... .......... 39% 13.6M 19s 102800K .......... .......... .......... .......... .......... 39% 16.0M 19s 102850K .......... .......... .......... .......... .......... 39% 10.4M 19s 102900K .......... .......... .......... .......... .......... 39% 12.2M 19s 102950K .......... .......... .......... .......... .......... 39% 11.6M 19s 103000K .......... .......... .......... .......... .......... 39% 12.6M 19s 103050K .......... .......... .......... .......... .......... 39% 17.6M 19s 103100K .......... .......... .......... .......... .......... 39% 10.8M 19s 103150K .......... .......... .......... .......... .......... 39% 15.0M 19s 103200K .......... .......... .......... .......... .......... 39% 9.98M 19s 103250K .......... .......... .......... .......... .......... 39% 15.3M 19s 103300K .......... .......... .......... .......... .......... 39% 13.3M 19s 103350K .......... .......... .......... .......... .......... 39% 8.39M 19s 103400K .......... .......... .......... .......... .......... 39% 6.91M 19s 103450K .......... .......... .......... .......... .......... 39% 5.86M 19s 103500K .......... .......... .......... .......... .......... 39% 7.08M 19s 103550K .......... .......... .......... .......... .......... 39% 6.37M 19s 103600K .......... .......... .......... .......... .......... 39% 6.32M 19s 103650K .......... .......... .......... .......... .......... 39% 10.4M 19s 103700K .......... .......... .......... .......... .......... 39% 9.91M 19s 103750K .......... .......... .......... .......... .......... 39% 7.37M 19s 103800K .......... .......... .......... .......... .......... 39% 11.6M 19s 103850K .......... .......... .......... .......... .......... 39% 4.15M 19s 103900K .......... .......... .......... .......... .......... 39% 10.7M 19s 103950K .......... .......... .......... .......... .......... 39% 7.82M 19s 104000K .......... .......... .......... .......... .......... 39% 10.6M 19s 104050K .......... .......... .......... .......... .......... 39% 12.1M 19s 104100K .......... .......... .......... .......... .......... 39% 9.69M 19s 104150K .......... .......... .......... .......... .......... 39% 14.9M 19s 104200K .......... .......... .......... .......... .......... 39% 8.93M 19s 104250K .......... .......... .......... .......... .......... 39% 11.4M 19s 104300K .......... .......... .......... .......... .......... 39% 12.3M 19s 104350K .......... .......... .......... .......... .......... 39% 10.5M 19s 104400K .......... .......... .......... .......... .......... 39% 12.0M 19s 104450K .......... .......... .......... .......... .......... 39% 10.6M 19s 104500K .......... .......... .......... .......... .......... 39% 9.57M 19s 104550K .......... .......... .......... .......... .......... 39% 11.1M 19s 104600K .......... .......... .......... .......... .......... 39% 9.17M 19s 104650K .......... .......... .......... .......... .......... 39% 7.86M 19s 104700K .......... .......... .......... .......... .......... 39% 10.3M 19s 104750K .......... .......... .......... .......... .......... 39% 9.81M 19s 104800K .......... .......... .......... .......... .......... 39% 9.04M 19s 104850K .......... .......... .......... .......... .......... 40% 8.89M 19s 104900K .......... .......... .......... .......... .......... 40% 9.54M 19s 104950K .......... .......... .......... .......... .......... 40% 6.66M 19s 105000K .......... .......... .......... .......... .......... 40% 10.4M 19s 105050K .......... .......... .......... .......... .......... 40% 8.49M 19s 105100K .......... .......... .......... .......... .......... 40% 7.84M 19s 105150K .......... .......... .......... .......... .......... 40% 7.60M 19s 105200K .......... .......... .......... .......... .......... 40% 5.26M 19s 105250K .......... .......... .......... .......... .......... 40% 7.19M 19s 105300K .......... .......... .......... .......... .......... 40% 5.94M 19s 105350K .......... .......... .......... .......... .......... 40% 8.17M 19s 105400K .......... .......... .......... .......... .......... 40% 19.2M 19s 105450K .......... .......... .......... .......... .......... 40% 30.8M 19s 105500K .......... .......... .......... .......... .......... 40% 14.2M 19s 105550K .......... .......... .......... .......... .......... 40% 22.9M 19s 105600K .......... .......... .......... .......... .......... 40% 15.2M 19s 105650K .......... .......... .......... .......... .......... 40% 14.3M 19s 105700K .......... .......... .......... .......... .......... 40% 12.3M 19s 105750K .......... .......... .......... .......... .......... 40% 9.48M 19s 105800K .......... .......... .......... .......... .......... 40% 12.3M 19s 105850K .......... .......... .......... .......... .......... 40% 12.4M 19s 105900K .......... .......... .......... .......... .......... 40% 9.70M 19s 105950K .......... .......... .......... .......... .......... 40% 6.92M 19s 106000K .......... .......... .......... .......... .......... 40% 10.4M 19s 106050K .......... .......... .......... .......... .......... 40% 6.56M 19s 106100K .......... .......... .......... .......... .......... 40% 5.31M 19s 106150K .......... .......... .......... .......... .......... 40% 6.36M 19s 106200K .......... .......... .......... .......... .......... 40% 4.58M 19s 106250K .......... .......... .......... .......... .......... 40% 5.64M 19s 106300K .......... .......... .......... .......... .......... 40% 5.23M 19s 106350K .......... .......... .......... .......... .......... 40% 6.83M 19s 106400K .......... .......... .......... .......... .......... 40% 7.90M 19s 106450K .......... .......... .......... .......... .......... 40% 5.34M 19s 106500K .......... .......... .......... .......... .......... 40% 7.97M 19s 106550K .......... .......... .......... .......... .......... 40% 9.31M 19s 106600K .......... .......... .......... .......... .......... 40% 8.86M 19s 106650K .......... .......... .......... .......... .......... 40% 11.9M 19s 106700K .......... .......... .......... .......... .......... 40% 10.2M 19s 106750K .......... .......... .......... .......... .......... 40% 9.08M 19s 106800K .......... .......... .......... .......... .......... 40% 12.4M 19s 106850K .......... .......... .......... .......... .......... 40% 9.00M 19s 106900K .......... .......... .......... .......... .......... 40% 11.2M 19s 106950K .......... .......... .......... .......... .......... 40% 11.4M 19s 107000K .......... .......... .......... .......... .......... 40% 31.8M 19s 107050K .......... .......... .......... .......... .......... 40% 37.2M 19s 107100K .......... .......... .......... .......... .......... 40% 21.6M 19s 107150K .......... .......... .......... .......... .......... 40% 22.4M 18s 107200K .......... .......... .......... .......... .......... 40% 26.5M 18s 107250K .......... .......... .......... .......... .......... 40% 20.4M 18s 107300K .......... .......... .......... .......... .......... 40% 34.4M 18s 107350K .......... .......... .......... .......... .......... 40% 20.5M 18s 107400K .......... .......... .......... .......... .......... 40% 19.4M 18s 107450K .......... .......... .......... .......... .......... 41% 17.0M 18s 107500K .......... .......... .......... .......... .......... 41% 31.8M 18s 107550K .......... .......... .......... .......... .......... 41% 18.8M 18s 107600K .......... .......... .......... .......... .......... 41% 11.0M 18s 107650K .......... .......... .......... .......... .......... 41% 17.8M 18s 107700K .......... .......... .......... .......... .......... 41% 10.3M 18s 107750K .......... .......... .......... .......... .......... 41% 8.21M 18s 107800K .......... .......... .......... .......... .......... 41% 8.44M 18s 107850K .......... .......... .......... .......... .......... 41% 7.33M 18s 107900K .......... .......... .......... .......... .......... 41% 9.72M 18s 107950K .......... .......... .......... .......... .......... 41% 7.54M 18s 108000K .......... .......... .......... .......... .......... 41% 11.1M 18s 108050K .......... .......... .......... .......... .......... 41% 18.0M 18s 108100K .......... .......... .......... .......... .......... 41% 16.0M 18s 108150K .......... .......... .......... .......... .......... 41% 27.8M 18s 108200K .......... .......... .......... .......... .......... 41% 10.9M 18s 108250K .......... .......... .......... .......... .......... 41% 24.3M 18s 108300K .......... .......... .......... .......... .......... 41% 22.7M 18s 108350K .......... .......... .......... .......... .......... 41% 13.7M 18s 108400K .......... .......... .......... .......... .......... 41% 13.2M 18s 108450K .......... .......... .......... .......... .......... 41% 20.8M 18s 108500K .......... .......... .......... .......... .......... 41% 9.54M 18s 108550K .......... .......... .......... .......... .......... 41% 25.1M 18s 108600K .......... .......... .......... .......... .......... 41% 8.92M 18s 108650K .......... .......... .......... .......... .......... 41% 12.4M 18s 108700K .......... .......... .......... .......... .......... 41% 7.44M 18s 108750K .......... .......... .......... .......... .......... 41% 13.9M 18s 108800K .......... .......... .......... .......... .......... 41% 9.64M 18s 108850K .......... .......... .......... .......... .......... 41% 5.65M 18s 108900K .......... .......... .......... .......... .......... 41% 8.40M 18s 108950K .......... .......... .......... .......... .......... 41% 7.15M 18s 109000K .......... .......... .......... .......... .......... 41% 6.89M 18s 109050K .......... .......... .......... .......... .......... 41% 5.83M 18s 109100K .......... .......... .......... .......... .......... 41% 5.32M 18s 109150K .......... .......... .......... .......... .......... 41% 7.55M 18s 109200K .......... .......... .......... .......... .......... 41% 12.1M 18s 109250K .......... .......... .......... .......... .......... 41% 10.9M 18s 109300K .......... .......... .......... .......... .......... 41% 10.7M 18s 109350K .......... .......... .......... .......... .......... 41% 7.92M 18s 109400K .......... .......... .......... .......... .......... 41% 7.92M 18s 109450K .......... .......... .......... .......... .......... 41% 7.87M 18s 109500K .......... .......... .......... .......... .......... 41% 8.21M 18s 109550K .......... .......... .......... .......... .......... 41% 10.3M 18s 109600K .......... .......... .......... .......... .......... 41% 5.64M 18s 109650K .......... .......... .......... .......... .......... 41% 10.2M 18s 109700K .......... .......... .......... .......... .......... 41% 5.75M 18s 109750K .......... .......... .......... .......... .......... 41% 14.1M 18s 109800K .......... .......... .......... .......... .......... 41% 9.11M 18s 109850K .......... .......... .......... .......... .......... 41% 9.60M 18s 109900K .......... .......... .......... .......... .......... 41% 11.6M 18s 109950K .......... .......... .......... .......... .......... 41% 10.6M 18s 110000K .......... .......... .......... .......... .......... 41% 11.7M 18s 110050K .......... .......... .......... .......... .......... 41% 12.8M 18s 110100K .......... .......... .......... .......... .......... 42% 10.4M 18s 110150K .......... .......... .......... .......... .......... 42% 14.9M 18s 110200K .......... .......... .......... .......... .......... 42% 13.7M 18s 110250K .......... .......... .......... .......... .......... 42% 14.9M 18s 110300K .......... .......... .......... .......... .......... 42% 16.6M 18s 110350K .......... .......... .......... .......... .......... 42% 8.84M 18s 110400K .......... .......... .......... .......... .......... 42% 15.4M 18s 110450K .......... .......... .......... .......... .......... 42% 11.3M 18s 110500K .......... .......... .......... .......... .......... 42% 8.82M 18s 110550K .......... .......... .......... .......... .......... 42% 7.29M 18s 110600K .......... .......... .......... .......... .......... 42% 5.43M 18s 110650K .......... .......... .......... .......... .......... 42% 5.99M 18s 110700K .......... .......... .......... .......... .......... 42% 5.18M 18s 110750K .......... .......... .......... .......... .......... 42% 3.50M 18s 110800K .......... .......... .......... .......... .......... 42% 6.44M 18s 110850K .......... .......... .......... .......... .......... 42% 6.29M 18s 110900K .......... .......... .......... .......... .......... 42% 7.01M 18s 110950K .......... .......... .......... .......... .......... 42% 7.56M 18s 111000K .......... .......... .......... .......... .......... 42% 9.10M 18s 111050K .......... .......... .......... .......... .......... 42% 8.80M 18s 111100K .......... .......... .......... .......... .......... 42% 10.0M 18s 111150K .......... .......... .......... .......... .......... 42% 8.32M 18s 111200K .......... .......... .......... .......... .......... 42% 8.06M 18s 111250K .......... .......... .......... .......... .......... 42% 8.67M 18s 111300K .......... .......... .......... .......... .......... 42% 8.77M 18s 111350K .......... .......... .......... .......... .......... 42% 5.31M 18s 111400K .......... .......... .......... .......... .......... 42% 5.32M 18s 111450K .......... .......... .......... .......... .......... 42% 4.11M 18s 111500K .......... .......... .......... .......... .......... 42% 4.11M 18s 111550K .......... .......... .......... .......... .......... 42% 4.83M 18s 111600K .......... .......... .......... .......... .......... 42% 4.51M 18s 111650K .......... .......... .......... .......... .......... 42% 4.91M 18s 111700K .......... .......... .......... .......... .......... 42% 8.19M 18s 111750K .......... .......... .......... .......... .......... 42% 6.79M 18s 111800K .......... .......... .......... .......... .......... 42% 8.64M 18s 111850K .......... .......... .......... .......... .......... 42% 6.34M 18s 111900K .......... .......... .......... .......... .......... 42% 5.24M 18s 111950K .......... .......... .......... .......... .......... 42% 5.48M 18s 112000K .......... .......... .......... .......... .......... 42% 4.87M 18s 112050K .......... .......... .......... .......... .......... 42% 5.79M 18s 112100K .......... .......... .......... .......... .......... 42% 5.04M 18s 112150K .......... .......... .......... .......... .......... 42% 11.0M 18s 112200K .......... .......... .......... .......... .......... 42% 7.04M 18s 112250K .......... .......... .......... .......... .......... 42% 8.02M 18s 112300K .......... .......... .......... .......... .......... 42% 5.98M 18s 112350K .......... .......... .......... .......... .......... 42% 3.76M 18s 112400K .......... .......... .......... .......... .......... 42% 4.34M 18s 112450K .......... .......... .......... .......... .......... 42% 4.37M 18s 112500K .......... .......... .......... .......... .......... 42% 4.78M 18s 112550K .......... .......... .......... .......... .......... 42% 7.40M 18s 112600K .......... .......... .......... .......... .......... 42% 8.70M 18s 112650K .......... .......... .......... .......... .......... 42% 9.15M 18s 112700K .......... .......... .......... .......... .......... 43% 5.34M 18s 112750K .......... .......... .......... .......... .......... 43% 6.74M 18s 112800K .......... .......... .......... .......... .......... 43% 6.51M 18s 112850K .......... .......... .......... .......... .......... 43% 3.49M 18s 112900K .......... .......... .......... .......... .......... 43% 3.37M 18s 112950K .......... .......... .......... .......... .......... 43% 2.92M 18s 113000K .......... .......... .......... .......... .......... 43% 4.02M 18s 113050K .......... .......... .......... .......... .......... 43% 3.47M 18s 113100K .......... .......... .......... .......... .......... 43% 3.11M 18s 113150K .......... .......... .......... .......... .......... 43% 2.26M 18s 113200K .......... .......... .......... .......... .......... 43% 1.39M 18s 113250K .......... .......... .......... .......... .......... 43% 2.12M 18s 113300K .......... .......... .......... .......... .......... 43% 9.33M 18s 113350K .......... .......... .......... .......... .......... 43% 9.70M 18s 113400K .......... .......... .......... .......... .......... 43% 13.7M 18s 113450K .......... .......... .......... .......... .......... 43% 11.3M 18s 113500K .......... .......... .......... .......... .......... 43% 10.8M 18s 113550K .......... .......... .......... .......... .......... 43% 10.1M 18s 113600K .......... .......... .......... .......... .......... 43% 10.5M 18s 113650K .......... .......... .......... .......... .......... 43% 10.6M 18s 113700K .......... .......... .......... .......... .......... 43% 6.94M 18s 113750K .......... .......... .......... .......... .......... 43% 7.03M 18s 113800K .......... .......... .......... .......... .......... 43% 7.11M 18s 113850K .......... .......... .......... .......... .......... 43% 6.62M 18s 113900K .......... .......... .......... .......... .......... 43% 6.67M 18s 113950K .......... .......... .......... .......... .......... 43% 9.20M 18s 114000K .......... .......... .......... .......... .......... 43% 9.39M 18s 114050K .......... .......... .......... .......... .......... 43% 11.0M 18s 114100K .......... .......... .......... .......... .......... 43% 6.92M 18s 114150K .......... .......... .......... .......... .......... 43% 14.9M 18s 114200K .......... .......... .......... .......... .......... 43% 7.59M 18s 114250K .......... .......... .......... .......... .......... 43% 7.42M 18s 114300K .......... .......... .......... .......... .......... 43% 8.01M 18s 114350K .......... .......... .......... .......... .......... 43% 6.26M 18s 114400K .......... .......... .......... .......... .......... 43% 6.85M 18s 114450K .......... .......... .......... .......... .......... 43% 5.29M 18s 114500K .......... .......... .......... .......... .......... 43% 5.51M 18s 114550K .......... .......... .......... .......... .......... 43% 5.71M 18s 114600K .......... .......... .......... .......... .......... 43% 6.25M 18s 114650K .......... .......... .......... .......... .......... 43% 6.45M 18s 114700K .......... .......... .......... .......... .......... 43% 4.97M 18s 114750K .......... .......... .......... .......... .......... 43% 6.88M 18s 114800K .......... .......... .......... .......... .......... 43% 4.99M 18s 114850K .......... .......... .......... .......... .......... 43% 4.49M 18s 114900K .......... .......... .......... .......... .......... 43% 10.4M 18s 114950K .......... .......... .......... .......... .......... 43% 11.2M 18s 115000K .......... .......... .......... .......... .......... 43% 12.0M 18s 115050K .......... .......... .......... .......... .......... 43% 8.14M 18s 115100K .......... .......... .......... .......... .......... 43% 7.27M 18s 115150K .......... .......... .......... .......... .......... 43% 7.52M 18s 115200K .......... .......... .......... .......... .......... 43% 7.28M 18s 115250K .......... .......... .......... .......... .......... 43% 7.70M 18s 115300K .......... .......... .......... .......... .......... 43% 12.1M 18s 115350K .......... .......... .......... .......... .......... 44% 7.42M 18s 115400K .......... .......... .......... .......... .......... 44% 28.5M 18s 115450K .......... .......... .......... .......... .......... 44% 12.6M 18s 115500K .......... .......... .......... .......... .......... 44% 16.5M 18s 115550K .......... .......... .......... .......... .......... 44% 10.1M 18s 115600K .......... .......... .......... .......... .......... 44% 12.0M 18s 115650K .......... .......... .......... .......... .......... 44% 6.64M 18s 115700K .......... .......... .......... .......... .......... 44% 4.06M 18s 115750K .......... .......... .......... .......... .......... 44% 5.76M 18s 115800K .......... .......... .......... .......... .......... 44% 6.17M 18s 115850K .......... .......... .......... .......... .......... 44% 3.85M 18s 115900K .......... .......... .......... .......... .......... 44% 5.74M 18s 115950K .......... .......... .......... .......... .......... 44% 3.87M 18s 116000K .......... .......... .......... .......... .......... 44% 4.92M 18s 116050K .......... .......... .......... .......... .......... 44% 4.16M 18s 116100K .......... .......... .......... .......... .......... 44% 3.61M 18s 116150K .......... .......... .......... .......... .......... 44% 9.20M 18s 116200K .......... .......... .......... .......... .......... 44% 8.09M 18s 116250K .......... .......... .......... .......... .......... 44% 8.28M 18s 116300K .......... .......... .......... .......... .......... 44% 8.32M 18s 116350K .......... .......... .......... .......... .......... 44% 7.64M 18s 116400K .......... .......... .......... .......... .......... 44% 9.59M 18s 116450K .......... .......... .......... .......... .......... 44% 7.31M 18s 116500K .......... .......... .......... .......... .......... 44% 6.12M 18s 116550K .......... .......... .......... .......... .......... 44% 6.01M 18s 116600K .......... .......... .......... .......... .......... 44% 3.35M 18s 116650K .......... .......... .......... .......... .......... 44% 2.07M 18s 116700K .......... .......... .......... .......... .......... 44% 209K 18s 116750K .......... .......... .......... .......... .......... 44% 1.10M 18s 116800K .......... .......... .......... .......... .......... 44% 3.24M 18s 116850K .......... .......... .......... .......... .......... 44% 14.2M 18s 116900K .......... .......... .......... .......... .......... 44% 13.7M 18s 116950K .......... .......... .......... .......... .......... 44% 14.1M 18s 117000K .......... .......... .......... .......... .......... 44% 13.3M 18s 117050K .......... .......... .......... .......... .......... 44% 11.3M 18s 117100K .......... .......... .......... .......... .......... 44% 9.17M 18s 117150K .......... .......... .......... .......... .......... 44% 9.65M 18s 117200K .......... .......... .......... .......... .......... 44% 10.7M 18s 117250K .......... .......... .......... .......... .......... 44% 11.8M 18s 117300K .......... .......... .......... .......... .......... 44% 9.93M 18s 117350K .......... .......... .......... .......... .......... 44% 8.43M 18s 117400K .......... .......... .......... .......... .......... 44% 8.64M 18s 117450K .......... .......... .......... .......... .......... 44% 6.45M 18s 117500K .......... .......... .......... .......... .......... 44% 7.28M 18s 117550K .......... .......... .......... .......... .......... 44% 7.98M 18s 117600K .......... .......... .......... .......... .......... 44% 6.35M 18s 117650K .......... .......... .......... .......... .......... 44% 8.95M 18s 117700K .......... .......... .......... .......... .......... 44% 18.4M 18s 117750K .......... .......... .......... .......... .......... 44% 21.8M 18s 117800K .......... .......... .......... .......... .......... 44% 14.6M 18s 117850K .......... .......... .......... .......... .......... 44% 30.1M 18s 117900K .......... .......... .......... .......... .......... 44% 16.9M 18s 117950K .......... .......... .......... .......... .......... 45% 19.7M 18s 118000K .......... .......... .......... .......... .......... 45% 12.9M 18s 118050K .......... .......... .......... .......... .......... 45% 14.2M 18s 118100K .......... .......... .......... .......... .......... 45% 8.34M 18s 118150K .......... .......... .......... .......... .......... 45% 8.46M 18s 118200K .......... .......... .......... .......... .......... 45% 4.77M 18s 118250K .......... .......... .......... .......... .......... 45% 5.79M 18s 118300K .......... .......... .......... .......... .......... 45% 3.30M 18s 118350K .......... .......... .......... .......... .......... 45% 3.18M 18s 118400K .......... .......... .......... .......... .......... 45% 3.29M 18s 118450K .......... .......... .......... .......... .......... 45% 3.21M 18s 118500K .......... .......... .......... .......... .......... 45% 3.81M 18s 118550K .......... .......... .......... .......... .......... 45% 5.78M 18s 118600K .......... .......... .......... .......... .......... 45% 7.90M 18s 118650K .......... .......... .......... .......... .......... 45% 7.03M 18s 118700K .......... .......... .......... .......... .......... 45% 6.83M 18s 118750K .......... .......... .......... .......... .......... 45% 6.51M 18s 118800K .......... .......... .......... .......... .......... 45% 6.89M 18s 118850K .......... .......... .......... .......... .......... 45% 5.96M 18s 118900K .......... .......... .......... .......... .......... 45% 8.24M 18s 118950K .......... .......... .......... .......... .......... 45% 6.24M 18s 119000K .......... .......... .......... .......... .......... 45% 7.00M 18s 119050K .......... .......... .......... .......... .......... 45% 7.79M 18s 119100K .......... .......... .......... .......... .......... 45% 7.22M 18s 119150K .......... .......... .......... .......... .......... 45% 6.77M 18s 119200K .......... .......... .......... .......... .......... 45% 3.67M 18s 119250K .......... .......... .......... .......... .......... 45% 4.44M 18s 119300K .......... .......... .......... .......... .......... 45% 4.19M 18s 119350K .......... .......... .......... .......... .......... 45% 7.26M 18s 119400K .......... .......... .......... .......... .......... 45% 18.9M 18s 119450K .......... .......... .......... .......... .......... 45% 14.8M 18s 119500K .......... .......... .......... .......... .......... 45% 18.5M 18s 119550K .......... .......... .......... .......... .......... 45% 17.1M 18s 119600K .......... .......... .......... .......... .......... 45% 12.1M 18s 119650K .......... .......... .......... .......... .......... 45% 13.9M 18s 119700K .......... .......... .......... .......... .......... 45% 10.5M 18s 119750K .......... .......... .......... .......... .......... 45% 13.3M 18s 119800K .......... .......... .......... .......... .......... 45% 11.7M 18s 119850K .......... .......... .......... .......... .......... 45% 9.71M 18s 119900K .......... .......... .......... .......... .......... 45% 10.1M 18s 119950K .......... .......... .......... .......... .......... 45% 7.03M 18s 120000K .......... .......... .......... .......... .......... 45% 7.43M 18s 120050K .......... .......... .......... .......... .......... 45% 7.66M 18s 120100K .......... .......... .......... .......... .......... 45% 6.24M 18s 120150K .......... .......... .......... .......... .......... 45% 4.24M 18s 120200K .......... .......... .......... .......... .......... 45% 4.34M 18s 120250K .......... .......... .......... .......... .......... 45% 5.16M 18s 120300K .......... .......... .......... .......... .......... 45% 4.83M 18s 120350K .......... .......... .......... .......... .......... 45% 7.11M 18s 120400K .......... .......... .......... .......... .......... 45% 25.5M 18s 120450K .......... .......... .......... .......... .......... 45% 12.2M 18s 120500K .......... .......... .......... .......... .......... 45% 13.4M 18s 120550K .......... .......... .......... .......... .......... 45% 10.6M 17s 120600K .......... .......... .......... .......... .......... 46% 8.49M 17s 120650K .......... .......... .......... .......... .......... 46% 18.2M 17s 120700K .......... .......... .......... .......... .......... 46% 7.08M 17s 120750K .......... .......... .......... .......... .......... 46% 9.96M 17s 120800K .......... .......... .......... .......... .......... 46% 8.30M 17s 120850K .......... .......... .......... .......... .......... 46% 7.36M 17s 120900K .......... .......... .......... .......... .......... 46% 9.96M 17s 120950K .......... .......... .......... .......... .......... 46% 8.65M 17s 121000K .......... .......... .......... .......... .......... 46% 9.06M 17s 121050K .......... .......... .......... .......... .......... 46% 9.47M 17s 121100K .......... .......... .......... .......... .......... 46% 13.5M 17s 121150K .......... .......... .......... .......... .......... 46% 16.0M 17s 121200K .......... .......... .......... .......... .......... 46% 3.27M 17s 121250K .......... .......... .......... .......... .......... 46% 132M 17s 121300K .......... .......... .......... .......... .......... 46% 14.7M 17s 121350K .......... .......... .......... .......... .......... 46% 5.32M 17s 121400K .......... .......... .......... .......... .......... 46% 9.61M 17s 121450K .......... .......... .......... .......... .......... 46% 6.51M 17s 121500K .......... .......... .......... .......... .......... 46% 11.2M 17s 121550K .......... .......... .......... .......... .......... 46% 9.10M 17s 121600K .......... .......... .......... .......... .......... 46% 12.5M 17s 121650K .......... .......... .......... .......... .......... 46% 9.18M 17s 121700K .......... .......... .......... .......... .......... 46% 10.2M 17s 121750K .......... .......... .......... .......... .......... 46% 11.9M 17s 121800K .......... .......... .......... .......... .......... 46% 8.00M 17s 121850K .......... .......... .......... .......... .......... 46% 8.26M 17s 121900K .......... .......... .......... .......... .......... 46% 7.40M 17s 121950K .......... .......... .......... .......... .......... 46% 6.22M 17s 122000K .......... .......... .......... .......... .......... 46% 8.51M 17s 122050K .......... .......... .......... .......... .......... 46% 7.13M 17s 122100K .......... .......... .......... .......... .......... 46% 6.35M 17s 122150K .......... .......... .......... .......... .......... 46% 6.80M 17s 122200K .......... .......... .......... .......... .......... 46% 7.53M 17s 122250K .......... .......... .......... .......... .......... 46% 11.8M 17s 122300K .......... .......... .......... .......... .......... 46% 11.4M 17s 122350K .......... .......... .......... .......... .......... 46% 6.16M 17s 122400K .......... .......... .......... .......... .......... 46% 7.99M 17s 122450K .......... .......... .......... .......... .......... 46% 5.92M 17s 122500K .......... .......... .......... .......... .......... 46% 6.89M 17s 122550K .......... .......... .......... .......... .......... 46% 6.08M 17s 122600K .......... .......... .......... .......... .......... 46% 12.4M 17s 122650K .......... .......... .......... .......... .......... 46% 14.9M 17s 122700K .......... .......... .......... .......... .......... 46% 8.44M 17s 122750K .......... .......... .......... .......... .......... 46% 13.3M 17s 122800K .......... .......... .......... .......... .......... 46% 11.9M 17s 122850K .......... .......... .......... .......... .......... 46% 8.46M 17s 122900K .......... .......... .......... .......... .......... 46% 11.9M 17s 122950K .......... .......... .......... .......... .......... 46% 7.73M 17s 123000K .......... .......... .......... .......... .......... 46% 9.43M 17s 123050K .......... .......... .......... .......... .......... 46% 8.35M 17s 123100K .......... .......... .......... .......... .......... 46% 6.71M 17s 123150K .......... .......... .......... .......... .......... 46% 7.37M 17s 123200K .......... .......... .......... .......... .......... 47% 4.01M 17s 123250K .......... .......... .......... .......... .......... 47% 6.24M 17s 123300K .......... .......... .......... .......... .......... 47% 6.76M 17s 123350K .......... .......... .......... .......... .......... 47% 6.51M 17s 123400K .......... .......... .......... .......... .......... 47% 6.29M 17s 123450K .......... .......... .......... .......... .......... 47% 6.90M 17s 123500K .......... .......... .......... .......... .......... 47% 13.9M 17s 123550K .......... .......... .......... .......... .......... 47% 34.0M 17s 123600K .......... .......... .......... .......... .......... 47% 17.3M 17s 123650K .......... .......... .......... .......... .......... 47% 26.1M 17s 123700K .......... .......... .......... .......... .......... 47% 15.8M 17s 123750K .......... .......... .......... .......... .......... 47% 27.0M 17s 123800K .......... .......... .......... .......... .......... 47% 27.4M 17s 123850K .......... .......... .......... .......... .......... 47% 15.9M 17s 123900K .......... .......... .......... .......... .......... 47% 28.5M 17s 123950K .......... .......... .......... .......... .......... 47% 16.0M 17s 124000K .......... .......... .......... .......... .......... 47% 13.0M 17s 124050K .......... .......... .......... .......... .......... 47% 61.2M 17s 124100K .......... .......... .......... .......... .......... 47% 16.4M 17s 124150K .......... .......... .......... .......... .......... 47% 13.9M 17s 124200K .......... .......... .......... .......... .......... 47% 20.5M 17s 124250K .......... .......... .......... .......... .......... 47% 16.5M 17s 124300K .......... .......... .......... .......... .......... 47% 9.40M 17s 124350K .......... .......... .......... .......... .......... 47% 12.5M 17s 124400K .......... .......... .......... .......... .......... 47% 11.3M 17s 124450K .......... .......... .......... .......... .......... 47% 6.18M 17s 124500K .......... .......... .......... .......... .......... 47% 8.08M 17s 124550K .......... .......... .......... .......... .......... 47% 8.68M 17s 124600K .......... .......... .......... .......... .......... 47% 6.81M 17s 124650K .......... .......... .......... .......... .......... 47% 7.23M 17s 124700K .......... .......... .......... .......... .......... 47% 25.9M 17s 124750K .......... .......... .......... .......... .......... 47% 13.6M 17s 124800K .......... .......... .......... .......... .......... 47% 15.0M 17s 124850K .......... .......... .......... .......... .......... 47% 12.8M 17s 124900K .......... .......... .......... .......... .......... 47% 16.3M 17s 124950K .......... .......... .......... .......... .......... 47% 7.81M 17s 125000K .......... .......... .......... .......... .......... 47% 27.8M 17s 125050K .......... .......... .......... .......... .......... 47% 11.0M 17s 125100K .......... .......... .......... .......... .......... 47% 8.27M 17s 125150K .......... .......... .......... .......... .......... 47% 9.19M 17s 125200K .......... .......... .......... .......... .......... 47% 12.0M 17s 125250K .......... .......... .......... .......... .......... 47% 7.37M 17s 125300K .......... .......... .......... .......... .......... 47% 8.85M 17s 125350K .......... .......... .......... .......... .......... 47% 5.75M 17s 125400K .......... .......... .......... .......... .......... 47% 6.41M 17s 125450K .......... .......... .......... .......... .......... 47% 3.18M 17s 125500K .......... .......... .......... .......... .......... 47% 4.77M 17s 125550K .......... .......... .......... .......... .......... 47% 5.35M 17s 125600K .......... .......... .......... .......... .......... 47% 4.12M 17s 125650K .......... .......... .......... .......... .......... 47% 15.1M 17s 125700K .......... .......... .......... .......... .......... 47% 16.3M 17s 125750K .......... .......... .......... .......... .......... 47% 16.1M 17s 125800K .......... .......... .......... .......... .......... 47% 24.6M 17s 125850K .......... .......... .......... .......... .......... 48% 13.8M 17s 125900K .......... .......... .......... .......... .......... 48% 10.7M 17s 125950K .......... .......... .......... .......... .......... 48% 17.0M 17s 126000K .......... .......... .......... .......... .......... 48% 19.5M 17s 126050K .......... .......... .......... .......... .......... 48% 13.8M 17s 126100K .......... .......... .......... .......... .......... 48% 8.11M 17s 126150K .......... .......... .......... .......... .......... 48% 9.74M 17s 126200K .......... .......... .......... .......... .......... 48% 7.80M 17s 126250K .......... .......... .......... .......... .......... 48% 6.25M 17s 126300K .......... .......... .......... .......... .......... 48% 8.37M 17s 126350K .......... .......... .......... .......... .......... 48% 5.77M 17s 126400K .......... .......... .......... .......... .......... 48% 6.47M 17s 126450K .......... .......... .......... .......... .......... 48% 5.91M 17s 126500K .......... .......... .......... .......... .......... 48% 9.94M 17s 126550K .......... .......... .......... .......... .......... 48% 14.1M 17s 126600K .......... .......... .......... .......... .......... 48% 14.7M 17s 126650K .......... .......... .......... .......... .......... 48% 16.3M 17s 126700K .......... .......... .......... .......... .......... 48% 7.77M 17s 126750K .......... .......... .......... .......... .......... 48% 21.3M 17s 126800K .......... .......... .......... .......... .......... 48% 8.34M 17s 126850K .......... .......... .......... .......... .......... 48% 8.82M 17s 126900K .......... .......... .......... .......... .......... 48% 8.88M 17s 126950K .......... .......... .......... .......... .......... 48% 8.93M 17s 127000K .......... .......... .......... .......... .......... 48% 8.65M 17s 127050K .......... .......... .......... .......... .......... 48% 13.2M 17s 127100K .......... .......... .......... .......... .......... 48% 7.99M 17s 127150K .......... .......... .......... .......... .......... 48% 10.8M 17s 127200K .......... .......... .......... .......... .......... 48% 9.61M 17s 127250K .......... .......... .......... .......... .......... 48% 154M 17s 127300K .......... .......... .......... .......... .......... 48% 17.7M 17s 127350K .......... .......... .......... .......... .......... 48% 18.0M 17s 127400K .......... .......... .......... .......... .......... 48% 28.7M 17s 127450K .......... .......... .......... .......... .......... 48% 12.3M 17s 127500K .......... .......... .......... .......... .......... 48% 16.8M 16s 127550K .......... .......... .......... .......... .......... 48% 12.8M 16s 127600K .......... .......... .......... .......... .......... 48% 7.04M 16s 127650K .......... .......... .......... .......... .......... 48% 4.14M 16s 127700K .......... .......... .......... .......... .......... 48% 3.26M 16s 127750K .......... .......... .......... .......... .......... 48% 3.94M 16s 127800K .......... .......... .......... .......... .......... 48% 3.94M 16s 127850K .......... .......... .......... .......... .......... 48% 2.28M 16s 127900K .......... .......... .......... .......... .......... 48% 3.16M 16s 127950K .......... .......... .......... .......... .......... 48% 10.4M 16s 128000K .......... .......... .......... .......... .......... 48% 17.1M 16s 128050K .......... .......... .......... .......... .......... 48% 17.9M 16s 128100K .......... .......... .......... .......... .......... 48% 18.7M 16s 128150K .......... .......... .......... .......... .......... 48% 26.4M 16s 128200K .......... .......... .......... .......... .......... 48% 10.5M 16s 128250K .......... .......... .......... .......... .......... 48% 11.3M 16s 128300K .......... .......... .......... .......... .......... 48% 11.8M 16s 128350K .......... .......... .......... .......... .......... 48% 8.38M 16s 128400K .......... .......... .......... .......... .......... 48% 6.83M 16s 128450K .......... .......... .......... .......... .......... 49% 8.65M 16s 128500K .......... .......... .......... .......... .......... 49% 8.14M 16s 128550K .......... .......... .......... .......... .......... 49% 9.19M 16s 128600K .......... .......... .......... .......... .......... 49% 7.69M 16s 128650K .......... .......... .......... .......... .......... 49% 12.7M 16s 128700K .......... .......... .......... .......... .......... 49% 24.1M 16s 128750K .......... .......... .......... .......... .......... 49% 25.5M 16s 128800K .......... .......... .......... .......... .......... 49% 21.5M 16s 128850K .......... .......... .......... .......... .......... 49% 23.9M 16s 128900K .......... .......... .......... .......... .......... 49% 16.8M 16s 128950K .......... .......... .......... .......... .......... 49% 25.1M 16s 129000K .......... .......... .......... .......... .......... 49% 15.3M 16s 129050K .......... .......... .......... .......... .......... 49% 9.71M 16s 129100K .......... .......... .......... .......... .......... 49% 22.7M 16s 129150K .......... .......... .......... .......... .......... 49% 9.41M 16s 129200K .......... .......... .......... .......... .......... 49% 9.48M 16s 129250K .......... .......... .......... .......... .......... 49% 11.8M 16s 129300K .......... .......... .......... .......... .......... 49% 10.4M 16s 129350K .......... .......... .......... .......... .......... 49% 10.3M 16s 129400K .......... .......... .......... .......... .......... 49% 14.0M 16s 129450K .......... .......... .......... .......... .......... 49% 9.87M 16s 129500K .......... .......... .......... .......... .......... 49% 10.1M 16s 129550K .......... .......... .......... .......... .......... 49% 11.8M 16s 129600K .......... .......... .......... .......... .......... 49% 10.5M 16s 129650K .......... .......... .......... .......... .......... 49% 14.3M 16s 129700K .......... .......... .......... .......... .......... 49% 5.52M 16s 129750K .......... .......... .......... .......... .......... 49% 5.19M 16s 129800K .......... .......... .......... .......... .......... 49% 5.42M 16s 129850K .......... .......... .......... .......... .......... 49% 4.35M 16s 129900K .......... .......... .......... .......... .......... 49% 6.95M 16s 129950K .......... .......... .......... .......... .......... 49% 10.7M 16s 130000K .......... .......... .......... .......... .......... 49% 20.7M 16s 130050K .......... .......... .......... .......... .......... 49% 11.8M 16s 130100K .......... .......... .......... .......... .......... 49% 8.90M 16s 130150K .......... .......... .......... .......... .......... 49% 15.5M 16s 130200K .......... .......... .......... .......... .......... 49% 4.83M 16s 130250K .......... .......... .......... .......... .......... 49% 25.6M 16s 130300K .......... .......... .......... .......... .......... 49% 7.37M 16s 130350K .......... .......... .......... .......... .......... 49% 5.36M 16s 130400K .......... .......... .......... .......... .......... 49% 7.04M 16s 130450K .......... .......... .......... .......... .......... 49% 6.47M 16s 130500K .......... .......... .......... .......... .......... 49% 8.30M 16s 130550K .......... .......... .......... .......... .......... 49% 7.88M 16s 130600K .......... .......... .......... .......... .......... 49% 4.40M 16s 130650K .......... .......... .......... .......... .......... 49% 1.61M 16s 130700K .......... .......... .......... .......... .......... 49% 278K 16s 130750K .......... .......... .......... .......... .......... 49% 824K 16s 130800K .......... .......... .......... .......... .......... 49% 3.10M 16s 130850K .......... .......... .......... .......... .......... 49% 2.47M 16s 130900K .......... .......... .......... .......... .......... 49% 6.93M 16s 130950K .......... .......... .......... .......... .......... 49% 9.08M 16s 131000K .......... .......... .......... .......... .......... 49% 14.6M 16s 131050K .......... .......... .......... .......... .......... 50% 16.7M 16s 131100K .......... .......... .......... .......... .......... 50% 13.9M 16s 131150K .......... .......... .......... .......... .......... 50% 15.5M 16s 131200K .......... .......... .......... .......... .......... 50% 11.0M 16s 131250K .......... .......... .......... .......... .......... 50% 12.7M 16s 131300K .......... .......... .......... .......... .......... 50% 15.9M 16s 131350K .......... .......... .......... .......... .......... 50% 10.8M 16s 131400K .......... .......... .......... .......... .......... 50% 7.99M 16s 131450K .......... .......... .......... .......... .......... 50% 13.3M 16s 131500K .......... .......... .......... .......... .......... 50% 11.2M 16s 131550K .......... .......... .......... .......... .......... 50% 10.5M 16s 131600K .......... .......... .......... .......... .......... 50% 8.49M 16s 131650K .......... .......... .......... .......... .......... 50% 6.47M 16s 131700K .......... .......... .......... .......... .......... 50% 8.03M 16s 131750K .......... .......... .......... .......... .......... 50% 6.73M 16s 131800K .......... .......... .......... .......... .......... 50% 5.97M 16s 131850K .......... .......... .......... .......... .......... 50% 6.70M 16s 131900K .......... .......... .......... .......... .......... 50% 9.94M 16s 131950K .......... .......... .......... .......... .......... 50% 7.72M 16s 132000K .......... .......... .......... .......... .......... 50% 6.83M 16s 132050K .......... .......... .......... .......... .......... 50% 10.1M 16s 132100K .......... .......... .......... .......... .......... 50% 16.8M 16s 132150K .......... .......... .......... .......... .......... 50% 8.47M 16s 132200K .......... .......... .......... .......... .......... 50% 8.14M 16s 132250K .......... .......... .......... .......... .......... 50% 8.22M 16s 132300K .......... .......... .......... .......... .......... 50% 9.12M 16s 132350K .......... .......... .......... .......... .......... 50% 7.63M 16s 132400K .......... .......... .......... .......... .......... 50% 1.00M 16s 132450K .......... .......... .......... .......... .......... 50% 138M 16s 132500K .......... .......... .......... .......... .......... 50% 319M 16s 132550K .......... .......... .......... .......... .......... 50% 27.5M 16s 132600K .......... .......... .......... .......... .......... 50% 12.4M 16s 132650K .......... .......... .......... .......... .......... 50% 8.40M 16s 132700K .......... .......... .......... .......... .......... 50% 12.0M 16s 132750K .......... .......... .......... .......... .......... 50% 7.82M 16s 132800K .......... .......... .......... .......... .......... 50% 5.09M 16s 132850K .......... .......... .......... .......... .......... 50% 3.85M 16s 132900K .......... .......... .......... .......... .......... 50% 3.73M 16s 132950K .......... .......... .......... .......... .......... 50% 4.99M 16s 133000K .......... .......... .......... .......... .......... 50% 3.83M 16s 133050K .......... .......... .......... .......... .......... 50% 5.17M 16s 133100K .......... .......... .......... .......... .......... 50% 3.98M 16s 133150K .......... .......... .......... .......... .......... 50% 4.04M 16s 133200K .......... .......... .......... .......... .......... 50% 7.34M 16s 133250K .......... .......... .......... .......... .......... 50% 6.44M 16s 133300K .......... .......... .......... .......... .......... 50% 18.3M 16s 133350K .......... .......... .......... .......... .......... 50% 14.3M 16s 133400K .......... .......... .......... .......... .......... 50% 10.8M 16s 133450K .......... .......... .......... .......... .......... 50% 30.8M 16s 133500K .......... .......... .......... .......... .......... 50% 10.2M 16s 133550K .......... .......... .......... .......... .......... 50% 8.95M 16s 133600K .......... .......... .......... .......... .......... 50% 7.06M 16s 133650K .......... .......... .......... .......... .......... 50% 6.63M 16s 133700K .......... .......... .......... .......... .......... 51% 6.19M 16s 133750K .......... .......... .......... .......... .......... 51% 6.56M 16s 133800K .......... .......... .......... .......... .......... 51% 5.97M 16s 133850K .......... .......... .......... .......... .......... 51% 6.99M 16s 133900K .......... .......... .......... .......... .......... 51% 13.7M 16s 133950K .......... .......... .......... .......... .......... 51% 11.9M 16s 134000K .......... .......... .......... .......... .......... 51% 39.1M 16s 134050K .......... .......... .......... .......... .......... 51% 12.1M 16s 134100K .......... .......... .......... .......... .......... 51% 9.50M 16s 134150K .......... .......... .......... .......... .......... 51% 6.12M 16s 134200K .......... .......... .......... .......... .......... 51% 4.34M 16s 134250K .......... .......... .......... .......... .......... 51% 5.18M 16s 134300K .......... .......... .......... .......... .......... 51% 4.39M 16s 134350K .......... .......... .......... .......... .......... 51% 3.95M 16s 134400K .......... .......... .......... .......... .......... 51% 4.39M 16s 134450K .......... .......... .......... .......... .......... 51% 5.09M 16s 134500K .......... .......... .......... .......... .......... 51% 4.81M 16s 134550K .......... .......... .......... .......... .......... 51% 5.64M 16s 134600K .......... .......... .......... .......... .......... 51% 4.25M 16s 134650K .......... .......... .......... .......... .......... 51% 9.35M 16s 134700K .......... .......... .......... .......... .......... 51% 6.98M 16s 134750K .......... .......... .......... .......... .......... 51% 6.84M 16s 134800K .......... .......... .......... .......... .......... 51% 6.01M 16s 134850K .......... .......... .......... .......... .......... 51% 5.94M 16s 134900K .......... .......... .......... .......... .......... 51% 12.2M 16s 134950K .......... .......... .......... .......... .......... 51% 12.5M 16s 135000K .......... .......... .......... .......... .......... 51% 15.0M 16s 135050K .......... .......... .......... .......... .......... 51% 11.3M 16s 135100K .......... .......... .......... .......... .......... 51% 11.0M 16s 135150K .......... .......... .......... .......... .......... 51% 9.76M 16s 135200K .......... .......... .......... .......... .......... 51% 8.65M 16s 135250K .......... .......... .......... .......... .......... 51% 9.41M 16s 135300K .......... .......... .......... .......... .......... 51% 7.45M 16s 135350K .......... .......... .......... .......... .......... 51% 6.99M 16s 135400K .......... .......... .......... .......... .......... 51% 6.12M 16s 135450K .......... .......... .......... .......... .......... 51% 5.47M 16s 135500K .......... .......... .......... .......... .......... 51% 5.11M 16s 135550K .......... .......... .......... .......... .......... 51% 5.43M 16s 135600K .......... .......... .......... .......... .......... 51% 4.78M 16s 135650K .......... .......... .......... .......... .......... 51% 6.10M 16s 135700K .......... .......... .......... .......... .......... 51% 4.72M 16s 135750K .......... .......... .......... .......... .......... 51% 5.96M 16s 135800K .......... .......... .......... .......... .......... 51% 6.47M 16s 135850K .......... .......... .......... .......... .......... 51% 12.1M 16s 135900K .......... .......... .......... .......... .......... 51% 12.4M 16s 135950K .......... .......... .......... .......... .......... 51% 8.46M 16s 136000K .......... .......... .......... .......... .......... 51% 14.1M 16s 136050K .......... .......... .......... .......... .......... 51% 12.8M 16s 136100K .......... .......... .......... .......... .......... 51% 7.64M 16s 136150K .......... .......... .......... .......... .......... 51% 7.66M 16s 136200K .......... .......... .......... .......... .......... 51% 5.63M 16s 136250K .......... .......... .......... .......... .......... 51% 6.59M 16s 136300K .......... .......... .......... .......... .......... 52% 11.0M 16s 136350K .......... .......... .......... .......... .......... 52% 7.32M 16s 136400K .......... .......... .......... .......... .......... 52% 8.69M 16s 136450K .......... .......... .......... .......... .......... 52% 5.98M 16s 136500K .......... .......... .......... .......... .......... 52% 7.33M 16s 136550K .......... .......... .......... .......... .......... 52% 6.05M 16s 136600K .......... .......... .......... .......... .......... 52% 2.74M 16s 136650K .......... .......... .......... .......... .......... 52% 3.07M 16s 136700K .......... .......... .......... .......... .......... 52% 2.77M 16s 136750K .......... .......... .......... .......... .......... 52% 9.19M 16s 136800K .......... .......... .......... .......... .......... 52% 23.4M 16s 136850K .......... .......... .......... .......... .......... 52% 9.53M 16s 136900K .......... .......... .......... .......... .......... 52% 18.3M 16s 136950K .......... .......... .......... .......... .......... 52% 18.1M 16s 137000K .......... .......... .......... .......... .......... 52% 10.4M 16s 137050K .......... .......... .......... .......... .......... 52% 19.4M 16s 137100K .......... .......... .......... .......... .......... 52% 11.5M 16s 137150K .......... .......... .......... .......... .......... 52% 14.3M 16s 137200K .......... .......... .......... .......... .......... 52% 12.4M 16s 137250K .......... .......... .......... .......... .......... 52% 11.2M 16s 137300K .......... .......... .......... .......... .......... 52% 14.2M 16s 137350K .......... .......... .......... .......... .......... 52% 10.4M 16s 137400K .......... .......... .......... .......... .......... 52% 8.77M 16s 137450K .......... .......... .......... .......... .......... 52% 10.3M 16s 137500K .......... .......... .......... .......... .......... 52% 13.4M 16s 137550K .......... .......... .......... .......... .......... 52% 13.0M 16s 137600K .......... .......... .......... .......... .......... 52% 7.56M 16s 137650K .......... .......... .......... .......... .......... 52% 8.00M 16s 137700K .......... .......... .......... .......... .......... 52% 7.38M 16s 137750K .......... .......... .......... .......... .......... 52% 7.55M 16s 137800K .......... .......... .......... .......... .......... 52% 9.45M 16s 137850K .......... .......... .......... .......... .......... 52% 5.97M 16s 137900K .......... .......... .......... .......... .......... 52% 6.65M 16s 137950K .......... .......... .......... .......... .......... 52% 5.71M 16s 138000K .......... .......... .......... .......... .......... 52% 7.27M 16s 138050K .......... .......... .......... .......... .......... 52% 4.25M 16s 138100K .......... .......... .......... .......... .......... 52% 2.03M 16s 138150K .......... .......... .......... .......... .......... 52% 2.30M 16s 138200K .......... .......... .......... .......... .......... 52% 8.66M 16s 138250K .......... .......... .......... .......... .......... 52% 11.7M 16s 138300K .......... .......... .......... .......... .......... 52% 12.4M 16s 138350K .......... .......... .......... .......... .......... 52% 11.7M 16s 138400K .......... .......... .......... .......... .......... 52% 13.3M 15s 138450K .......... .......... .......... .......... .......... 52% 7.86M 15s 138500K .......... .......... .......... .......... .......... 52% 9.40M 15s 138550K .......... .......... .......... .......... .......... 52% 8.40M 15s 138600K .......... .......... .......... .......... .......... 52% 8.81M 15s 138650K .......... .......... .......... .......... .......... 52% 9.58M 15s 138700K .......... .......... .......... .......... .......... 52% 6.49M 15s 138750K .......... .......... .......... .......... .......... 52% 7.21M 15s 138800K .......... .......... .......... .......... .......... 52% 7.01M 15s 138850K .......... .......... .......... .......... .......... 52% 5.12M 15s 138900K .......... .......... .......... .......... .......... 52% 8.65M 15s 138950K .......... .......... .......... .......... .......... 53% 5.30M 15s 139000K .......... .......... .......... .......... .......... 53% 7.10M 15s 139050K .......... .......... .......... .......... .......... 53% 12.2M 15s 139100K .......... .......... .......... .......... .......... 53% 7.24M 15s 139150K .......... .......... .......... .......... .......... 53% 8.42M 15s 139200K .......... .......... .......... .......... .......... 53% 5.06M 15s 139250K .......... .......... .......... .......... .......... 53% 11.9M 15s 139300K .......... .......... .......... .......... .......... 53% 7.75M 15s 139350K .......... .......... .......... .......... .......... 53% 5.35M 15s 139400K .......... .......... .......... .......... .......... 53% 7.69M 15s 139450K .......... .......... .......... .......... .......... 53% 9.31M 15s 139500K .......... .......... .......... .......... .......... 53% 11.6M 15s 139550K .......... .......... .......... .......... .......... 53% 10.2M 15s 139600K .......... .......... .......... .......... .......... 53% 9.56M 15s 139650K .......... .......... .......... .......... .......... 53% 9.39M 15s 139700K .......... .......... .......... .......... .......... 53% 6.67M 15s 139750K .......... .......... .......... .......... .......... 53% 6.17M 15s 139800K .......... .......... .......... .......... .......... 53% 7.82M 15s 139850K .......... .......... .......... .......... .......... 53% 4.37M 15s 139900K .......... .......... .......... .......... .......... 53% 4.92M 15s 139950K .......... .......... .......... .......... .......... 53% 4.77M 15s 140000K .......... .......... .......... .......... .......... 53% 4.56M 15s 140050K .......... .......... .......... .......... .......... 53% 3.94M 15s 140100K .......... .......... .......... .......... .......... 53% 3.39M 15s 140150K .......... .......... .......... .......... .......... 53% 3.94M 15s 140200K .......... .......... .......... .......... .......... 53% 6.08M 15s 140250K .......... .......... .......... .......... .......... 53% 7.55M 15s 140300K .......... .......... .......... .......... .......... 53% 4.57M 15s 140350K .......... .......... .......... .......... .......... 53% 4.37M 15s 140400K .......... .......... .......... .......... .......... 53% 4.18M 15s 140450K .......... .......... .......... .......... .......... 53% 3.86M 15s 140500K .......... .......... .......... .......... .......... 53% 11.0M 15s 140550K .......... .......... .......... .......... .......... 53% 12.7M 15s 140600K .......... .......... .......... .......... .......... 53% 9.62M 15s 140650K .......... .......... .......... .......... .......... 53% 8.94M 15s 140700K .......... .......... .......... .......... .......... 53% 13.4M 15s 140750K .......... .......... .......... .......... .......... 53% 13.6M 15s 140800K .......... .......... .......... .......... .......... 53% 8.59M 15s 140850K .......... .......... .......... .......... .......... 53% 12.6M 15s 140900K .......... .......... .......... .......... .......... 53% 11.4M 15s 140950K .......... .......... .......... .......... .......... 53% 10.7M 15s 141000K .......... .......... .......... .......... .......... 53% 13.6M 15s 141050K .......... .......... .......... .......... .......... 53% 14.7M 15s 141100K .......... .......... .......... .......... .......... 53% 12.1M 15s 141150K .......... .......... .......... .......... .......... 53% 10.7M 15s 141200K .......... .......... .......... .......... .......... 53% 13.9M 15s 141250K .......... .......... .......... .......... .......... 53% 7.04M 15s 141300K .......... .......... .......... .......... .......... 53% 9.06M 15s 141350K .......... .......... .......... .......... .......... 53% 7.60M 15s 141400K .......... .......... .......... .......... .......... 53% 10.7M 15s 141450K .......... .......... .......... .......... .......... 53% 9.85M 15s 141500K .......... .......... .......... .......... .......... 53% 8.05M 15s 141550K .......... .......... .......... .......... .......... 54% 13.5M 15s 141600K .......... .......... .......... .......... .......... 54% 7.07M 15s 141650K .......... .......... .......... .......... .......... 54% 8.36M 15s 141700K .......... .......... .......... .......... .......... 54% 8.46M 15s 141750K .......... .......... .......... .......... .......... 54% 11.3M 15s 141800K .......... .......... .......... .......... .......... 54% 15.1M 15s 141850K .......... .......... .......... .......... .......... 54% 10.7M 15s 141900K .......... .......... .......... .......... .......... 54% 7.87M 15s 141950K .......... .......... .......... .......... .......... 54% 3.56M 15s 142000K .......... .......... .......... .......... .......... 54% 4.22M 15s 142050K .......... .......... .......... .......... .......... 54% 7.60M 15s 142100K .......... .......... .......... .......... .......... 54% 27.3M 15s 142150K .......... .......... .......... .......... .......... 54% 10.0M 15s 142200K .......... .......... .......... .......... .......... 54% 32.4M 15s 142250K .......... .......... .......... .......... .......... 54% 15.6M 15s 142300K .......... .......... .......... .......... .......... 54% 19.1M 15s 142350K .......... .......... .......... .......... .......... 54% 11.1M 15s 142400K .......... .......... .......... .......... .......... 54% 21.4M 15s 142450K .......... .......... .......... .......... .......... 54% 6.54M 15s 142500K .......... .......... .......... .......... .......... 54% 10.7M 15s 142550K .......... .......... .......... .......... .......... 54% 11.3M 15s 142600K .......... .......... .......... .......... .......... 54% 10.6M 15s 142650K .......... .......... .......... .......... .......... 54% 11.6M 15s 142700K .......... .......... .......... .......... .......... 54% 10.4M 15s 142750K .......... .......... .......... .......... .......... 54% 12.4M 15s 142800K .......... .......... .......... .......... .......... 54% 10.3M 15s 142850K .......... .......... .......... .......... .......... 54% 10.7M 15s 142900K .......... .......... .......... .......... .......... 54% 13.7M 15s 142950K .......... .......... .......... .......... .......... 54% 9.13M 15s 143000K .......... .......... .......... .......... .......... 54% 8.30M 15s 143050K .......... .......... .......... .......... .......... 54% 12.4M 15s 143100K .......... .......... .......... .......... .......... 54% 6.04M 15s 143150K .......... .......... .......... .......... .......... 54% 7.67M 15s 143200K .......... .......... .......... .......... .......... 54% 7.82M 15s 143250K .......... .......... .......... .......... .......... 54% 7.79M 15s 143300K .......... .......... .......... .......... .......... 54% 10.2M 15s 143350K .......... .......... .......... .......... .......... 54% 14.8M 15s 143400K .......... .......... .......... .......... .......... 54% 26.9M 15s 143450K .......... .......... .......... .......... .......... 54% 26.5M 15s 143500K .......... .......... .......... .......... .......... 54% 22.0M 15s 143550K .......... .......... .......... .......... .......... 54% 14.5M 15s 143600K .......... .......... .......... .......... .......... 54% 17.5M 15s 143650K .......... .......... .......... .......... .......... 54% 16.6M 15s 143700K .......... .......... .......... .......... .......... 54% 11.3M 15s 143750K .......... .......... .......... .......... .......... 54% 14.1M 15s 143800K .......... .......... .......... .......... .......... 54% 8.12M 15s 143850K .......... .......... .......... .......... .......... 54% 20.4M 15s 143900K .......... .......... .......... .......... .......... 54% 13.0M 15s 143950K .......... .......... .......... .......... .......... 54% 12.5M 15s 144000K .......... .......... .......... .......... .......... 54% 11.8M 15s 144050K .......... .......... .......... .......... .......... 54% 12.1M 15s 144100K .......... .......... .......... .......... .......... 54% 9.55M 15s 144150K .......... .......... .......... .......... .......... 54% 7.21M 15s 144200K .......... .......... .......... .......... .......... 55% 5.96M 15s 144250K .......... .......... .......... .......... .......... 55% 5.84M 15s 144300K .......... .......... .......... .......... .......... 55% 4.42M 15s 144350K .......... .......... .......... .......... .......... 55% 4.50M 15s 144400K .......... .......... .......... .......... .......... 55% 5.14M 15s 144450K .......... .......... .......... .......... .......... 55% 4.47M 15s 144500K .......... .......... .......... .......... .......... 55% 8.31M 15s 144550K .......... .......... .......... .......... .......... 55% 8.38M 15s 144600K .......... .......... .......... .......... .......... 55% 7.62M 15s 144650K .......... .......... .......... .......... .......... 55% 8.96M 15s 144700K .......... .......... .......... .......... .......... 55% 7.55M 15s 144750K .......... .......... .......... .......... .......... 55% 5.62M 15s 144800K .......... .......... .......... .......... .......... 55% 3.52M 15s 144850K .......... .......... .......... .......... .......... 55% 2.48M 15s 144900K .......... .......... .......... .......... .......... 55% 2.31M 15s 144950K .......... .......... .......... .......... .......... 55% 815K 15s 145000K .......... .......... .......... .......... .......... 55% 4.25M 15s 145050K .......... .......... .......... .......... .......... 55% 4.24M 15s 145100K .......... .......... .......... .......... .......... 55% 10.5M 15s 145150K .......... .......... .......... .......... .......... 55% 15.9M 15s 145200K .......... .......... .......... .......... .......... 55% 34.9M 15s 145250K .......... .......... .......... .......... .......... 55% 31.0M 15s 145300K .......... .......... .......... .......... .......... 55% 19.0M 15s 145350K .......... .......... .......... .......... .......... 55% 18.1M 15s 145400K .......... .......... .......... .......... .......... 55% 17.2M 15s 145450K .......... .......... .......... .......... .......... 55% 24.3M 15s 145500K .......... .......... .......... .......... .......... 55% 11.9M 15s 145550K .......... .......... .......... .......... .......... 55% 15.8M 15s 145600K .......... .......... .......... .......... .......... 55% 11.0M 15s 145650K .......... .......... .......... .......... .......... 55% 9.87M 15s 145700K .......... .......... .......... .......... .......... 55% 12.2M 15s 145750K .......... .......... .......... .......... .......... 55% 9.15M 15s 145800K .......... .......... .......... .......... .......... 55% 11.8M 15s 145850K .......... .......... .......... .......... .......... 55% 9.56M 15s 145900K .......... .......... .......... .......... .......... 55% 11.4M 15s 145950K .......... .......... .......... .......... .......... 55% 10.6M 15s 146000K .......... .......... .......... .......... .......... 55% 12.0M 15s 146050K .......... .......... .......... .......... .......... 55% 12.6M 15s 146100K .......... .......... .......... .......... .......... 55% 12.0M 15s 146150K .......... .......... .......... .......... .......... 55% 8.39M 15s 146200K .......... .......... .......... .......... .......... 55% 6.57M 15s 146250K .......... .......... .......... .......... .......... 55% 6.27M 15s 146300K .......... .......... .......... .......... .......... 55% 4.49M 15s 146350K .......... .......... .......... .......... .......... 55% 3.67M 15s 146400K .......... .......... .......... .......... .......... 55% 4.79M 15s 146450K .......... .......... .......... .......... .......... 55% 3.88M 15s 146500K .......... .......... .......... .......... .......... 55% 1022K 15s 146550K .......... .......... .......... .......... .......... 55% 1.85M 15s 146600K .......... .......... .......... .......... .......... 55% 4.54M 15s 146650K .......... .......... .......... .......... .......... 55% 14.3M 15s 146700K .......... .......... .......... .......... .......... 55% 11.9M 15s 146750K .......... .......... .......... .......... .......... 55% 32.3M 15s 146800K .......... .......... .......... .......... .......... 56% 15.6M 15s 146850K .......... .......... .......... .......... .......... 56% 13.5M 15s 146900K .......... .......... .......... .......... .......... 56% 17.9M 14s 146950K .......... .......... .......... .......... .......... 56% 11.7M 14s 147000K .......... .......... .......... .......... .......... 56% 17.7M 14s 147050K .......... .......... .......... .......... .......... 56% 16.7M 14s 147100K .......... .......... .......... .......... .......... 56% 11.7M 14s 147150K .......... .......... .......... .......... .......... 56% 10.9M 14s 147200K .......... .......... .......... .......... .......... 56% 7.96M 14s 147250K .......... .......... .......... .......... .......... 56% 5.35M 14s 147300K .......... .......... .......... .......... .......... 56% 11.7M 14s 147350K .......... .......... .......... .......... .......... 56% 5.38M 14s 147400K .......... .......... .......... .......... .......... 56% 7.75M 14s 147450K .......... .......... .......... .......... .......... 56% 6.16M 14s 147500K .......... .......... .......... .......... .......... 56% 7.01M 14s 147550K .......... .......... .......... .......... .......... 56% 6.05M 14s 147600K .......... .......... .......... .......... .......... 56% 5.53M 14s 147650K .......... .......... .......... .......... .......... 56% 4.72M 14s 147700K .......... .......... .......... .......... .......... 56% 3.24M 14s 147750K .......... .......... .......... .......... .......... 56% 3.73M 14s 147800K .......... .......... .......... .......... .......... 56% 4.57M 14s 147850K .......... .......... .......... .......... .......... 56% 8.92M 14s 147900K .......... .......... .......... .......... .......... 56% 10.9M 14s 147950K .......... .......... .......... .......... .......... 56% 11.2M 14s 148000K .......... .......... .......... .......... .......... 56% 12.7M 14s 148050K .......... .......... .......... .......... .......... 56% 9.78M 14s 148100K .......... .......... .......... .......... .......... 56% 8.37M 14s 148150K .......... .......... .......... .......... .......... 56% 10.7M 14s 148200K .......... .......... .......... .......... .......... 56% 7.46M 14s 148250K .......... .......... .......... .......... .......... 56% 7.84M 14s 148300K .......... .......... .......... .......... .......... 56% 7.15M 14s 148350K .......... .......... .......... .......... .......... 56% 6.70M 14s 148400K .......... .......... .......... .......... .......... 56% 6.21M 14s 148450K .......... .......... .......... .......... .......... 56% 6.30M 14s 148500K .......... .......... .......... .......... .......... 56% 6.22M 14s 148550K .......... .......... .......... .......... .......... 56% 6.14M 14s 148600K .......... .......... .......... .......... .......... 56% 5.94M 14s 148650K .......... .......... .......... .......... .......... 56% 9.30M 14s 148700K .......... .......... .......... .......... .......... 56% 19.9M 14s 148750K .......... .......... .......... .......... .......... 56% 12.9M 14s 148800K .......... .......... .......... .......... .......... 56% 13.5M 14s 148850K .......... .......... .......... .......... .......... 56% 18.1M 14s 148900K .......... .......... .......... .......... .......... 56% 14.0M 14s 148950K .......... .......... .......... .......... .......... 56% 20.7M 14s 149000K .......... .......... .......... .......... .......... 56% 9.38M 14s 149050K .......... .......... .......... .......... .......... 56% 20.6M 14s 149100K .......... .......... .......... .......... .......... 56% 12.3M 14s 149150K .......... .......... .......... .......... .......... 56% 12.9M 14s 149200K .......... .......... .......... .......... .......... 56% 9.53M 14s 149250K .......... .......... .......... .......... .......... 56% 11.8M 14s 149300K .......... .......... .......... .......... .......... 56% 11.9M 14s 149350K .......... .......... .......... .......... .......... 56% 10.3M 14s 149400K .......... .......... .......... .......... .......... 57% 11.8M 14s 149450K .......... .......... .......... .......... .......... 57% 12.2M 14s 149500K .......... .......... .......... .......... .......... 57% 13.5M 14s 149550K .......... .......... .......... .......... .......... 57% 11.8M 14s 149600K .......... .......... .......... .......... .......... 57% 51.4M 14s 149650K .......... .......... .......... .......... .......... 57% 45.3M 14s 149700K .......... .......... .......... .......... .......... 57% 13.6M 14s 149750K .......... .......... .......... .......... .......... 57% 11.4M 14s 149800K .......... .......... .......... .......... .......... 57% 12.1M 14s 149850K .......... .......... .......... .......... .......... 57% 7.74M 14s 149900K .......... .......... .......... .......... .......... 57% 7.83M 14s 149950K .......... .......... .......... .......... .......... 57% 7.34M 14s 150000K .......... .......... .......... .......... .......... 57% 8.41M 14s 150050K .......... .......... .......... .......... .......... 57% 6.23M 14s 150100K .......... .......... .......... .......... .......... 57% 7.99M 14s 150150K .......... .......... .......... .......... .......... 57% 6.52M 14s 150200K .......... .......... .......... .......... .......... 57% 11.4M 14s 150250K .......... .......... .......... .......... .......... 57% 8.73M 14s 150300K .......... .......... .......... .......... .......... 57% 20.3M 14s 150350K .......... .......... .......... .......... .......... 57% 7.03M 14s 150400K .......... .......... .......... .......... .......... 57% 7.07M 14s 150450K .......... .......... .......... .......... .......... 57% 4.32M 14s 150500K .......... .......... .......... .......... .......... 57% 3.31M 14s 150550K .......... .......... .......... .......... .......... 57% 3.10M 14s 150600K .......... .......... .......... .......... .......... 57% 4.12M 14s 150650K .......... .......... .......... .......... .......... 57% 4.92M 14s 150700K .......... .......... .......... .......... .......... 57% 4.55M 14s 150750K .......... .......... .......... .......... .......... 57% 10.6M 14s 150800K .......... .......... .......... .......... .......... 57% 16.7M 14s 150850K .......... .......... .......... .......... .......... 57% 14.3M 14s 150900K .......... .......... .......... .......... .......... 57% 11.6M 14s 150950K .......... .......... .......... .......... .......... 57% 11.8M 14s 151000K .......... .......... .......... .......... .......... 57% 7.57M 14s 151050K .......... .......... .......... .......... .......... 57% 12.4M 14s 151100K .......... .......... .......... .......... .......... 57% 9.14M 14s 151150K .......... .......... .......... .......... .......... 57% 8.04M 14s 151200K .......... .......... .......... .......... .......... 57% 7.07M 14s 151250K .......... .......... .......... .......... .......... 57% 4.88M 14s 151300K .......... .......... .......... .......... .......... 57% 5.67M 14s 151350K .......... .......... .......... .......... .......... 57% 4.97M 14s 151400K .......... .......... .......... .......... .......... 57% 4.41M 14s 151450K .......... .......... .......... .......... .......... 57% 4.55M 14s 151500K .......... .......... .......... .......... .......... 57% 4.57M 14s 151550K .......... .......... .......... .......... .......... 57% 5.34M 14s 151600K .......... .......... .......... .......... .......... 57% 3.97M 14s 151650K .......... .......... .......... .......... .......... 57% 12.8M 14s 151700K .......... .......... .......... .......... .......... 57% 12.7M 14s 151750K .......... .......... .......... .......... .......... 57% 7.55M 14s 151800K .......... .......... .......... .......... .......... 57% 11.9M 14s 151850K .......... .......... .......... .......... .......... 57% 10.1M 14s 151900K .......... .......... .......... .......... .......... 57% 10.7M 14s 151950K .......... .......... .......... .......... .......... 57% 8.66M 14s 152000K .......... .......... .......... .......... .......... 57% 5.78M 14s 152050K .......... .......... .......... .......... .......... 58% 7.96M 14s 152100K .......... .......... .......... .......... .......... 58% 5.90M 14s 152150K .......... .......... .......... .......... .......... 58% 5.98M 14s 152200K .......... .......... .......... .......... .......... 58% 4.50M 14s 152250K .......... .......... .......... .......... .......... 58% 5.03M 14s 152300K .......... .......... .......... .......... .......... 58% 4.91M 14s 152350K .......... .......... .......... .......... .......... 58% 3.65M 14s 152400K .......... .......... .......... .......... .......... 58% 3.92M 14s 152450K .......... .......... .......... .......... .......... 58% 3.74M 14s 152500K .......... .......... .......... .......... .......... 58% 3.54M 14s 152550K .......... .......... .......... .......... .......... 58% 5.97M 14s 152600K .......... .......... .......... .......... .......... 58% 14.0M 14s 152650K .......... .......... .......... .......... .......... 58% 10.4M 14s 152700K .......... .......... .......... .......... .......... 58% 9.32M 14s 152750K .......... .......... .......... .......... .......... 58% 8.34M 14s 152800K .......... .......... .......... .......... .......... 58% 18.3M 14s 152850K .......... .......... .......... .......... .......... 58% 5.86M 14s 152900K .......... .......... .......... .......... .......... 58% 8.32M 14s 152950K .......... .......... .......... .......... .......... 58% 7.51M 14s 153000K .......... .......... .......... .......... .......... 58% 8.25M 14s 153050K .......... .......... .......... .......... .......... 58% 7.04M 14s 153100K .......... .......... .......... .......... .......... 58% 6.18M 14s 153150K .......... .......... .......... .......... .......... 58% 4.84M 14s 153200K .......... .......... .......... .......... .......... 58% 5.00M 14s 153250K .......... .......... .......... .......... .......... 58% 10.0M 14s 153300K .......... .......... .......... .......... .......... 58% 11.1M 14s 153350K .......... .......... .......... .......... .......... 58% 12.1M 14s 153400K .......... .......... .......... .......... .......... 58% 9.83M 14s 153450K .......... .......... .......... .......... .......... 58% 8.71M 14s 153500K .......... .......... .......... .......... .......... 58% 8.34M 14s 153550K .......... .......... .......... .......... .......... 58% 8.54M 14s 153600K .......... .......... .......... .......... .......... 58% 7.25M 14s 153650K .......... .......... .......... .......... .......... 58% 8.27M 14s 153700K .......... .......... .......... .......... .......... 58% 8.30M 14s 153750K .......... .......... .......... .......... .......... 58% 18.0M 14s 153800K .......... .......... .......... .......... .......... 58% 34.0M 14s 153850K .......... .......... .......... .......... .......... 58% 22.9M 14s 153900K .......... .......... .......... .......... .......... 58% 16.5M 14s 153950K .......... .......... .......... .......... .......... 58% 52.0M 14s 154000K .......... .......... .......... .......... .......... 58% 15.6M 14s 154050K .......... .......... .......... .......... .......... 58% 29.9M 14s 154100K .......... .......... .......... .......... .......... 58% 11.3M 14s 154150K .......... .......... .......... .......... .......... 58% 15.3M 14s 154200K .......... .......... .......... .......... .......... 58% 9.58M 14s 154250K .......... .......... .......... .......... .......... 58% 12.8M 14s 154300K .......... .......... .......... .......... .......... 58% 11.7M 14s 154350K .......... .......... .......... .......... .......... 58% 8.51M 14s 154400K .......... .......... .......... .......... .......... 58% 8.97M 14s 154450K .......... .......... .......... .......... .......... 58% 5.96M 14s 154500K .......... .......... .......... .......... .......... 58% 5.81M 14s 154550K .......... .......... .......... .......... .......... 58% 7.61M 14s 154600K .......... .......... .......... .......... .......... 58% 2.31M 14s 154650K .......... .......... .......... .......... .......... 59% 2.87M 14s 154700K .......... .......... .......... .......... .......... 59% 4.71M 14s 154750K .......... .......... .......... .......... .......... 59% 19.5M 14s 154800K .......... .......... .......... .......... .......... 59% 36.9M 14s 154850K .......... .......... .......... .......... .......... 59% 13.3M 14s 154900K .......... .......... .......... .......... .......... 59% 13.1M 14s 154950K .......... .......... .......... .......... .......... 59% 8.21M 13s 155000K .......... .......... .......... .......... .......... 59% 4.75M 13s 155050K .......... .......... .......... .......... .......... 59% 5.19M 13s 155100K .......... .......... .......... .......... .......... 59% 4.45M 13s 155150K .......... .......... .......... .......... .......... 59% 5.12M 13s 155200K .......... .......... .......... .......... .......... 59% 7.36M 13s 155250K .......... .......... .......... .......... .......... 59% 10.7M 13s 155300K .......... .......... .......... .......... .......... 59% 14.9M 13s 155350K .......... .......... .......... .......... .......... 59% 10.9M 13s 155400K .......... .......... .......... .......... .......... 59% 12.7M 13s 155450K .......... .......... .......... .......... .......... 59% 9.31M 13s 155500K .......... .......... .......... .......... .......... 59% 11.0M 13s 155550K .......... .......... .......... .......... .......... 59% 10.7M 13s 155600K .......... .......... .......... .......... .......... 59% 5.38M 13s 155650K .......... .......... .......... .......... .......... 59% 7.65M 13s 155700K .......... .......... .......... .......... .......... 59% 4.03M 13s 155750K .......... .......... .......... .......... .......... 59% 5.15M 13s 155800K .......... .......... .......... .......... .......... 59% 4.86M 13s 155850K .......... .......... .......... .......... .......... 59% 5.12M 13s 155900K .......... .......... .......... .......... .......... 59% 7.08M 13s 155950K .......... .......... .......... .......... .......... 59% 9.79M 13s 156000K .......... .......... .......... .......... .......... 59% 7.24M 13s 156050K .......... .......... .......... .......... .......... 59% 10.7M 13s 156100K .......... .......... .......... .......... .......... 59% 5.43M 13s 156150K .......... .......... .......... .......... .......... 59% 7.56M 13s 156200K .......... .......... .......... .......... .......... 59% 3.82M 13s 156250K .......... .......... .......... .......... .......... 59% 4.18M 13s 156300K .......... .......... .......... .......... .......... 59% 4.11M 13s 156350K .......... .......... .......... .......... .......... 59% 3.65M 13s 156400K .......... .......... .......... .......... .......... 59% 3.57M 13s 156450K .......... .......... .......... .......... .......... 59% 6.91M 13s 156500K .......... .......... .......... .......... .......... 59% 5.47M 13s 156550K .......... .......... .......... .......... .......... 59% 5.23M 13s 156600K .......... .......... .......... .......... .......... 59% 5.70M 13s 156650K .......... .......... .......... .......... .......... 59% 5.06M 13s 156700K .......... .......... .......... .......... .......... 59% 4.37M 13s 156750K .......... .......... .......... .......... .......... 59% 5.18M 13s 156800K .......... .......... .......... .......... .......... 59% 5.72M 13s 156850K .......... .......... .......... .......... .......... 59% 5.25M 13s 156900K .......... .......... .......... .......... .......... 59% 5.86M 13s 156950K .......... .......... .......... .......... .......... 59% 12.7M 13s 157000K .......... .......... .......... .......... .......... 59% 8.07M 13s 157050K .......... .......... .......... .......... .......... 59% 22.2M 13s 157100K .......... .......... .......... .......... .......... 59% 8.13M 13s 157150K .......... .......... .......... .......... .......... 59% 9.66M 13s 157200K .......... .......... .......... .......... .......... 59% 6.03M 13s 157250K .......... .......... .......... .......... .......... 59% 7.03M 13s 157300K .......... .......... .......... .......... .......... 60% 6.89M 13s 157350K .......... .......... .......... .......... .......... 60% 5.03M 13s 157400K .......... .......... .......... .......... .......... 60% 7.47M 13s 157450K .......... .......... .......... .......... .......... 60% 3.48M 13s 157500K .......... .......... .......... .......... .......... 60% 4.67M 13s 157550K .......... .......... .......... .......... .......... 60% 4.18M 13s 157600K .......... .......... .......... .......... .......... 60% 5.64M 13s 157650K .......... .......... .......... .......... .......... 60% 11.0M 13s 157700K .......... .......... .......... .......... .......... 60% 6.93M 13s 157750K .......... .......... .......... .......... .......... 60% 6.76M 13s 157800K .......... .......... .......... .......... .......... 60% 7.26M 13s 157850K .......... .......... .......... .......... .......... 60% 6.91M 13s 157900K .......... .......... .......... .......... .......... 60% 7.89M 13s 157950K .......... .......... .......... .......... .......... 60% 3.68M 13s 158000K .......... .......... .......... .......... .......... 60% 4.96M 13s 158050K .......... .......... .......... .......... .......... 60% 4.98M 13s 158100K .......... .......... .......... .......... .......... 60% 4.40M 13s 158150K .......... .......... .......... .......... .......... 60% 11.9M 13s 158200K .......... .......... .......... .......... .......... 60% 8.42M 13s 158250K .......... .......... .......... .......... .......... 60% 11.7M 13s 158300K .......... .......... .......... .......... .......... 60% 9.44M 13s 158350K .......... .......... .......... .......... .......... 60% 9.37M 13s 158400K .......... .......... .......... .......... .......... 60% 12.1M 13s 158450K .......... .......... .......... .......... .......... 60% 7.20M 13s 158500K .......... .......... .......... .......... .......... 60% 10.3M 13s 158550K .......... .......... .......... .......... .......... 60% 7.89M 13s 158600K .......... .......... .......... .......... .......... 60% 5.62M 13s 158650K .......... .......... .......... .......... .......... 60% 1.87M 13s 158700K .......... .......... .......... .......... .......... 60% 6.40M 13s 158750K .......... .......... .......... .......... .......... 60% 6.58M 13s 158800K .......... .......... .......... .......... .......... 60% 6.66M 13s 158850K .......... .......... .......... .......... .......... 60% 3.58M 13s 158900K .......... .......... .......... .......... .......... 60% 3.18M 13s 158950K .......... .......... .......... .......... .......... 60% 2.48M 13s 159000K .......... .......... .......... .......... .......... 60% 2.51M 13s 159050K .......... .......... .......... .......... .......... 60% 4.08M 13s 159100K .......... .......... .......... .......... .......... 60% 15.5M 13s 159150K .......... .......... .......... .......... .......... 60% 36.8M 13s 159200K .......... .......... .......... .......... .......... 60% 90.4M 13s 159250K .......... .......... .......... .......... .......... 60% 15.9M 13s 159300K .......... .......... .......... .......... .......... 60% 139M 13s 159350K .......... .......... .......... .......... .......... 60% 28.7M 13s 159400K .......... .......... .......... .......... .......... 60% 37.5M 13s 159450K .......... .......... .......... .......... .......... 60% 40.2M 13s 159500K .......... .......... .......... .......... .......... 60% 34.4M 13s 159550K .......... .......... .......... .......... .......... 60% 17.4M 13s 159600K .......... .......... .......... .......... .......... 60% 227M 13s 159650K .......... .......... .......... .......... .......... 60% 14.0M 13s 159700K .......... .......... .......... .......... .......... 60% 29.9M 13s 159750K .......... .......... .......... .......... .......... 60% 16.6M 13s 159800K .......... .......... .......... .......... .......... 60% 16.4M 13s 159850K .......... .......... .......... .......... .......... 60% 10.6M 13s 159900K .......... .......... .......... .......... .......... 61% 11.0M 13s 159950K .......... .......... .......... .......... .......... 61% 6.64M 13s 160000K .......... .......... .......... .......... .......... 61% 10.9M 13s 160050K .......... .......... .......... .......... .......... 61% 8.50M 13s 160100K .......... .......... .......... .......... .......... 61% 5.22M 13s 160150K .......... .......... .......... .......... .......... 61% 4.98M 13s 160200K .......... .......... .......... .......... .......... 61% 3.25M 13s 160250K .......... .......... .......... .......... .......... 61% 5.01M 13s 160300K .......... .......... .......... .......... .......... 61% 4.50M 13s 160350K .......... .......... .......... .......... .......... 61% 2.93M 13s 160400K .......... .......... .......... .......... .......... 61% 3.98M 13s 160450K .......... .......... .......... .......... .......... 61% 5.11M 13s 160500K .......... .......... .......... .......... .......... 61% 10.7M 13s 160550K .......... .......... .......... .......... .......... 61% 8.07M 13s 160600K .......... .......... .......... .......... .......... 61% 5.23M 13s 160650K .......... .......... .......... .......... .......... 61% 5.05M 13s 160700K .......... .......... .......... .......... .......... 61% 6.08M 13s 160750K .......... .......... .......... .......... .......... 61% 7.47M 13s 160800K .......... .......... .......... .......... .......... 61% 5.68M 13s 160850K .......... .......... .......... .......... .......... 61% 8.58M 13s 160900K .......... .......... .......... .......... .......... 61% 9.30M 13s 160950K .......... .......... .......... .......... .......... 61% 7.02M 13s 161000K .......... .......... .......... .......... .......... 61% 18.1M 13s 161050K .......... .......... .......... .......... .......... 61% 8.40M 13s 161100K .......... .......... .......... .......... .......... 61% 8.46M 13s 161150K .......... .......... .......... .......... .......... 61% 8.53M 13s 161200K .......... .......... .......... .......... .......... 61% 5.80M 13s 161250K .......... .......... .......... .......... .......... 61% 6.42M 13s 161300K .......... .......... .......... .......... .......... 61% 9.01M 13s 161350K .......... .......... .......... .......... .......... 61% 11.9M 13s 161400K .......... .......... .......... .......... .......... 61% 10.4M 13s 161450K .......... .......... .......... .......... .......... 61% 11.4M 13s 161500K .......... .......... .......... .......... .......... 61% 10.1M 13s 161550K .......... .......... .......... .......... .......... 61% 9.83M 13s 161600K .......... .......... .......... .......... .......... 61% 5.67M 13s 161650K .......... .......... .......... .......... .......... 61% 9.01M 13s 161700K .......... .......... .......... .......... .......... 61% 6.52M 13s 161750K .......... .......... .......... .......... .......... 61% 7.02M 13s 161800K .......... .......... .......... .......... .......... 61% 3.76M 13s 161850K .......... .......... .......... .......... .......... 61% 3.26M 13s 161900K .......... .......... .......... .......... .......... 61% 3.12M 13s 161950K .......... .......... .......... .......... .......... 61% 1.93M 13s 162000K .......... .......... .......... .......... .......... 61% 2.70M 13s 162050K .......... .......... .......... .......... .......... 61% 8.44M 13s 162100K .......... .......... .......... .......... .......... 61% 14.1M 13s 162150K .......... .......... .......... .......... .......... 61% 18.0M 13s 162200K .......... .......... .......... .......... .......... 61% 16.2M 13s 162250K .......... .......... .......... .......... .......... 61% 14.1M 13s 162300K .......... .......... .......... .......... .......... 61% 24.1M 13s 162350K .......... .......... .......... .......... .......... 61% 14.4M 13s 162400K .......... .......... .......... .......... .......... 61% 13.3M 13s 162450K .......... .......... .......... .......... .......... 61% 9.62M 13s 162500K .......... .......... .......... .......... .......... 61% 13.2M 13s 162550K .......... .......... .......... .......... .......... 62% 12.9M 13s 162600K .......... .......... .......... .......... .......... 62% 8.22M 13s 162650K .......... .......... .......... .......... .......... 62% 10.1M 13s 162700K .......... .......... .......... .......... .......... 62% 7.67M 13s 162750K .......... .......... .......... .......... .......... 62% 9.06M 13s 162800K .......... .......... .......... .......... .......... 62% 11.8M 13s 162850K .......... .......... .......... .......... .......... 62% 7.36M 13s 162900K .......... .......... .......... .......... .......... 62% 13.2M 13s 162950K .......... .......... .......... .......... .......... 62% 8.12M 13s 163000K .......... .......... .......... .......... .......... 62% 19.9M 13s 163050K .......... .......... .......... .......... .......... 62% 24.8M 13s 163100K .......... .......... .......... .......... .......... 62% 26.5M 13s 163150K .......... .......... .......... .......... .......... 62% 23.3M 13s 163200K .......... .......... .......... .......... .......... 62% 21.3M 13s 163250K .......... .......... .......... .......... .......... 62% 21.7M 13s 163300K .......... .......... .......... .......... .......... 62% 10.8M 13s 163350K .......... .......... .......... .......... .......... 62% 23.1M 13s 163400K .......... .......... .......... .......... .......... 62% 17.7M 13s 163450K .......... .......... .......... .......... .......... 62% 9.15M 13s 163500K .......... .......... .......... .......... .......... 62% 10.1M 13s 163550K .......... .......... .......... .......... .......... 62% 20.4M 12s 163600K .......... .......... .......... .......... .......... 62% 6.23M 12s 163650K .......... .......... .......... .......... .......... 62% 9.86M 12s 163700K .......... .......... .......... .......... .......... 62% 5.73M 12s 163750K .......... .......... .......... .......... .......... 62% 5.16M 12s 163800K .......... .......... .......... .......... .......... 62% 6.65M 12s 163850K .......... .......... .......... .......... .......... 62% 5.68M 12s 163900K .......... .......... .......... .......... .......... 62% 6.75M 12s 163950K .......... .......... .......... .......... .......... 62% 7.77M 12s 164000K .......... .......... .......... .......... .......... 62% 16.7M 12s 164050K .......... .......... .......... .......... .......... 62% 20.7M 12s 164100K .......... .......... .......... .......... .......... 62% 12.8M 12s 164150K .......... .......... .......... .......... .......... 62% 9.19M 12s 164200K .......... .......... .......... .......... .......... 62% 21.4M 12s 164250K .......... .......... .......... .......... .......... 62% 21.0M 12s 164300K .......... .......... .......... .......... .......... 62% 13.8M 12s 164350K .......... .......... .......... .......... .......... 62% 9.49M 12s 164400K .......... .......... .......... .......... .......... 62% 13.6M 12s 164450K .......... .......... .......... .......... .......... 62% 10.9M 12s 164500K .......... .......... .......... .......... .......... 62% 12.9M 12s 164550K .......... .......... .......... .......... .......... 62% 9.69M 12s 164600K .......... .......... .......... .......... .......... 62% 11.7M 12s 164650K .......... .......... .......... .......... .......... 62% 10.1M 12s 164700K .......... .......... .......... .......... .......... 62% 8.69M 12s 164750K .......... .......... .......... .......... .......... 62% 11.2M 12s 164800K .......... .......... .......... .......... .......... 62% 9.64M 12s 164850K .......... .......... .......... .......... .......... 62% 9.97M 12s 164900K .......... .......... .......... .......... .......... 62% 13.2M 12s 164950K .......... .......... .......... .......... .......... 62% 9.96M 12s 165000K .......... .......... .......... .......... .......... 62% 22.4M 12s 165050K .......... .......... .......... .......... .......... 62% 28.4M 12s 165100K .......... .......... .......... .......... .......... 62% 12.0M 12s 165150K .......... .......... .......... .......... .......... 63% 33.6M 12s 165200K .......... .......... .......... .......... .......... 63% 12.0M 12s 165250K .......... .......... .......... .......... .......... 63% 31.0M 12s 165300K .......... .......... .......... .......... .......... 63% 8.59M 12s 165350K .......... .......... .......... .......... .......... 63% 7.83M 12s 165400K .......... .......... .......... .......... .......... 63% 11.9M 12s 165450K .......... .......... .......... .......... .......... 63% 7.51M 12s 165500K .......... .......... .......... .......... .......... 63% 7.95M 12s 165550K .......... .......... .......... .......... .......... 63% 6.54M 12s 165600K .......... .......... .......... .......... .......... 63% 6.34M 12s 165650K .......... .......... .......... .......... .......... 63% 7.87M 12s 165700K .......... .......... .......... .......... .......... 63% 6.79M 12s 165750K .......... .......... .......... .......... .......... 63% 7.64M 12s 165800K .......... .......... .......... .......... .......... 63% 4.86M 12s 165850K .......... .......... .......... .......... .......... 63% 1.97M 12s 165900K .......... .......... .......... .......... .......... 63% 2.98M 12s 165950K .......... .......... .......... .......... .......... 63% 2.01M 12s 166000K .......... .......... .......... .......... .......... 63% 4.39M 12s 166050K .......... .......... .......... .......... .......... 63% 9.52M 12s 166100K .......... .......... .......... .......... .......... 63% 8.50M 12s 166150K .......... .......... .......... .......... .......... 63% 10.1M 12s 166200K .......... .......... .......... .......... .......... 63% 8.41M 12s 166250K .......... .......... .......... .......... .......... 63% 8.16M 12s 166300K .......... .......... .......... .......... .......... 63% 5.95M 12s 166350K .......... .......... .......... .......... .......... 63% 5.94M 12s 166400K .......... .......... .......... .......... .......... 63% 4.69M 12s 166450K .......... .......... .......... .......... .......... 63% 4.58M 12s 166500K .......... .......... .......... .......... .......... 63% 864K 12s 166550K .......... .......... .......... .......... .......... 63% 2.89M 12s 166600K .......... .......... .......... .......... .......... 63% 3.71M 12s 166650K .......... .......... .......... .......... .......... 63% 4.02M 12s 166700K .......... .......... .......... .......... .......... 63% 4.78M 12s 166750K .......... .......... .......... .......... .......... 63% 8.21M 12s 166800K .......... .......... .......... .......... .......... 63% 7.21M 12s 166850K .......... .......... .......... .......... .......... 63% 7.46M 12s 166900K .......... .......... .......... .......... .......... 63% 7.25M 12s 166950K .......... .......... .......... .......... .......... 63% 8.22M 12s 167000K .......... .......... .......... .......... .......... 63% 6.08M 12s 167050K .......... .......... .......... .......... .......... 63% 5.75M 12s 167100K .......... .......... .......... .......... .......... 63% 4.80M 12s 167150K .......... .......... .......... .......... .......... 63% 7.03M 12s 167200K .......... .......... .......... .......... .......... 63% 11.6M 12s 167250K .......... .......... .......... .......... .......... 63% 10.7M 12s 167300K .......... .......... .......... .......... .......... 63% 14.0M 12s 167350K .......... .......... .......... .......... .......... 63% 5.65M 12s 167400K .......... .......... .......... .......... .......... 63% 16.7M 12s 167450K .......... .......... .......... .......... .......... 63% 5.16M 12s 167500K .......... .......... .......... .......... .......... 63% 4.47M 12s 167550K .......... .......... .......... .......... .......... 63% 6.96M 12s 167600K .......... .......... .......... .......... .......... 63% 4.83M 12s 167650K .......... .......... .......... .......... .......... 63% 7.17M 12s 167700K .......... .......... .......... .......... .......... 63% 5.29M 12s 167750K .......... .......... .......... .......... .......... 63% 6.90M 12s 167800K .......... .......... .......... .......... .......... 64% 11.4M 12s 167850K .......... .......... .......... .......... .......... 64% 8.38M 12s 167900K .......... .......... .......... .......... .......... 64% 6.82M 12s 167950K .......... .......... .......... .......... .......... 64% 5.80M 12s 168000K .......... .......... .......... .......... .......... 64% 5.58M 12s 168050K .......... .......... .......... .......... .......... 64% 6.76M 12s 168100K .......... .......... .......... .......... .......... 64% 5.09M 12s 168150K .......... .......... .......... .......... .......... 64% 5.49M 12s 168200K .......... .......... .......... .......... .......... 64% 3.02M 12s 168250K .......... .......... .......... .......... .......... 64% 2.56M 12s 168300K .......... .......... .......... .......... .......... 64% 3.84M 12s 168350K .......... .......... .......... .......... .......... 64% 10.5M 12s 168400K .......... .......... .......... .......... .......... 64% 11.7M 12s 168450K .......... .......... .......... .......... .......... 64% 8.13M 12s 168500K .......... .......... .......... .......... .......... 64% 8.74M 12s 168550K .......... .......... .......... .......... .......... 64% 9.69M 12s 168600K .......... .......... .......... .......... .......... 64% 6.96M 12s 168650K .......... .......... .......... .......... .......... 64% 9.25M 12s 168700K .......... .......... .......... .......... .......... 64% 8.75M 12s 168750K .......... .......... .......... .......... .......... 64% 14.0M 12s 168800K .......... .......... .......... .......... .......... 64% 10.6M 12s 168850K .......... .......... .......... .......... .......... 64% 9.72M 12s 168900K .......... .......... .......... .......... .......... 64% 9.12M 12s 168950K .......... .......... .......... .......... .......... 64% 6.87M 12s 169000K .......... .......... .......... .......... .......... 64% 11.7M 12s 169050K .......... .......... .......... .......... .......... 64% 11.6M 12s 169100K .......... .......... .......... .......... .......... 64% 9.57M 12s 169150K .......... .......... .......... .......... .......... 64% 13.0M 12s 169200K .......... .......... .......... .......... .......... 64% 10.9M 12s 169250K .......... .......... .......... .......... .......... 64% 8.86M 12s 169300K .......... .......... .......... .......... .......... 64% 11.1M 12s 169350K .......... .......... .......... .......... .......... 64% 8.70M 12s 169400K .......... .......... .......... .......... .......... 64% 9.73M 12s 169450K .......... .......... .......... .......... .......... 64% 9.42M 12s 169500K .......... .......... .......... .......... .......... 64% 12.9M 12s 169550K .......... .......... .......... .......... .......... 64% 12.1M 12s 169600K .......... .......... .......... .......... .......... 64% 8.47M 12s 169650K .......... .......... .......... .......... .......... 64% 12.1M 12s 169700K .......... .......... .......... .......... .......... 64% 8.51M 12s 169750K .......... .......... .......... .......... .......... 64% 10.2M 12s 169800K .......... .......... .......... .......... .......... 64% 14.9M 12s 169850K .......... .......... .......... .......... .......... 64% 6.91M 12s 169900K .......... .......... .......... .......... .......... 64% 35.0M 12s 169950K .......... .......... .......... .......... .......... 64% 14.5M 12s 170000K .......... .......... .......... .......... .......... 64% 5.08M 12s 170050K .......... .......... .......... .......... .......... 64% 67.2M 12s 170100K .......... .......... .......... .......... .......... 64% 5.15M 12s 170150K .......... .......... .......... .......... .......... 64% 5.45M 12s 170200K .......... .......... .......... .......... .......... 64% 4.13M 12s 170250K .......... .......... .......... .......... .......... 64% 5.24M 12s 170300K .......... .......... .......... .......... .......... 64% 5.33M 12s 170350K .......... .......... .......... .......... .......... 64% 3.80M 12s 170400K .......... .......... .......... .......... .......... 65% 3.53M 12s 170450K .......... .......... .......... .......... .......... 65% 1.80M 12s 170500K .......... .......... .......... .......... .......... 65% 2.53M 12s 170550K .......... .......... .......... .......... .......... 65% 2.33M 12s 170600K .......... .......... .......... .......... .......... 65% 2.98M 12s 170650K .......... .......... .......... .......... .......... 65% 15.9M 12s 170700K .......... .......... .......... .......... .......... 65% 9.10M 12s 170750K .......... .......... .......... .......... .......... 65% 18.9M 12s 170800K .......... .......... .......... .......... .......... 65% 10.6M 12s 170850K .......... .......... .......... .......... .......... 65% 10.4M 12s 170900K .......... .......... .......... .......... .......... 65% 11.9M 12s 170950K .......... .......... .......... .......... .......... 65% 7.02M 12s 171000K .......... .......... .......... .......... .......... 65% 11.5M 12s 171050K .......... .......... .......... .......... .......... 65% 6.43M 12s 171100K .......... .......... .......... .......... .......... 65% 7.32M 12s 171150K .......... .......... .......... .......... .......... 65% 9.36M 12s 171200K .......... .......... .......... .......... .......... 65% 7.02M 12s 171250K .......... .......... .......... .......... .......... 65% 6.07M 12s 171300K .......... .......... .......... .......... .......... 65% 8.12M 12s 171350K .......... .......... .......... .......... .......... 65% 6.65M 12s 171400K .......... .......... .......... .......... .......... 65% 7.59M 12s 171450K .......... .......... .......... .......... .......... 65% 5.72M 12s 171500K .......... .......... .......... .......... .......... 65% 12.1M 12s 171550K .......... .......... .......... .......... .......... 65% 8.73M 12s 171600K .......... .......... .......... .......... .......... 65% 10.2M 12s 171650K .......... .......... .......... .......... .......... 65% 6.89M 12s 171700K .......... .......... .......... .......... .......... 65% 4.77M 12s 171750K .......... .......... .......... .......... .......... 65% 4.91M 12s 171800K .......... .......... .......... .......... .......... 65% 10.8M 12s 171850K .......... .......... .......... .......... .......... 65% 3.63M 12s 171900K .......... .......... .......... .......... .......... 65% 4.14M 12s 171950K .......... .......... .......... .......... .......... 65% 4.04M 12s 172000K .......... .......... .......... .......... .......... 65% 8.97M 12s 172050K .......... .......... .......... .......... .......... 65% 13.1M 12s 172100K .......... .......... .......... .......... .......... 65% 9.87M 12s 172150K .......... .......... .......... .......... .......... 65% 12.7M 11s 172200K .......... .......... .......... .......... .......... 65% 7.01M 11s 172250K .......... .......... .......... .......... .......... 65% 7.24M 11s 172300K .......... .......... .......... .......... .......... 65% 7.33M 11s 172350K .......... .......... .......... .......... .......... 65% 5.51M 11s 172400K .......... .......... .......... .......... .......... 65% 8.00M 11s 172450K .......... .......... .......... .......... .......... 65% 5.37M 11s 172500K .......... .......... .......... .......... .......... 65% 4.76M 11s 172550K .......... .......... .......... .......... .......... 65% 5.37M 11s 172600K .......... .......... .......... .......... .......... 65% 4.66M 11s 172650K .......... .......... .......... .......... .......... 65% 7.55M 11s 172700K .......... .......... .......... .......... .......... 65% 13.4M 11s 172750K .......... .......... .......... .......... .......... 65% 20.4M 11s 172800K .......... .......... .......... .......... .......... 65% 10.0M 11s 172850K .......... .......... .......... .......... .......... 65% 22.4M 11s 172900K .......... .......... .......... .......... .......... 65% 12.3M 11s 172950K .......... .......... .......... .......... .......... 65% 9.61M 11s 173000K .......... .......... .......... .......... .......... 66% 10.4M 11s 173050K .......... .......... .......... .......... .......... 66% 11.7M 11s 173100K .......... .......... .......... .......... .......... 66% 7.00M 11s 173150K .......... .......... .......... .......... .......... 66% 12.2M 11s 173200K .......... .......... .......... .......... .......... 66% 10.6M 11s 173250K .......... .......... .......... .......... .......... 66% 11.6M 11s 173300K .......... .......... .......... .......... .......... 66% 15.1M 11s 173350K .......... .......... .......... .......... .......... 66% 8.76M 11s 173400K .......... .......... .......... .......... .......... 66% 15.8M 11s 173450K .......... .......... .......... .......... .......... 66% 11.3M 11s 173500K .......... .......... .......... .......... .......... 66% 12.2M 11s 173550K .......... .......... .......... .......... .......... 66% 12.0M 11s 173600K .......... .......... .......... .......... .......... 66% 21.8M 11s 173650K .......... .......... .......... .......... .......... 66% 12.0M 11s 173700K .......... .......... .......... .......... .......... 66% 13.4M 11s 173750K .......... .......... .......... .......... .......... 66% 14.8M 11s 173800K .......... .......... .......... .......... .......... 66% 11.9M 11s 173850K .......... .......... .......... .......... .......... 66% 8.97M 11s 173900K .......... .......... .......... .......... .......... 66% 7.53M 11s 173950K .......... .......... .......... .......... .......... 66% 6.79M 11s 174000K .......... .......... .......... .......... .......... 66% 8.03M 11s 174050K .......... .......... .......... .......... .......... 66% 6.36M 11s 174100K .......... .......... .......... .......... .......... 66% 6.43M 11s 174150K .......... .......... .......... .......... .......... 66% 5.63M 11s 174200K .......... .......... .......... .......... .......... 66% 3.93M 11s 174250K .......... .......... .......... .......... .......... 66% 4.66M 11s 174300K .......... .......... .......... .......... .......... 66% 4.26M 11s 174350K .......... .......... .......... .......... .......... 66% 3.32M 11s 174400K .......... .......... .......... .......... .......... 66% 4.23M 11s 174450K .......... .......... .......... .......... .......... 66% 4.87M 11s 174500K .......... .......... .......... .......... .......... 66% 16.6M 11s 174550K .......... .......... .......... .......... .......... 66% 14.9M 11s 174600K .......... .......... .......... .......... .......... 66% 10.4M 11s 174650K .......... .......... .......... .......... .......... 66% 9.24M 11s 174700K .......... .......... .......... .......... .......... 66% 7.05M 11s 174750K .......... .......... .......... .......... .......... 66% 7.45M 11s 174800K .......... .......... .......... .......... .......... 66% 8.37M 11s 174850K .......... .......... .......... .......... .......... 66% 5.74M 11s 174900K .......... .......... .......... .......... .......... 66% 8.15M 11s 174950K .......... .......... .......... .......... .......... 66% 4.96M 11s 175000K .......... .......... .......... .......... .......... 66% 6.81M 11s 175050K .......... .......... .......... .......... .......... 66% 7.10M 11s 175100K .......... .......... .......... .......... .......... 66% 3.37M 11s 175150K .......... .......... .......... .......... .......... 66% 2.51M 11s 175200K .......... .......... .......... .......... .......... 66% 1.73M 11s 175250K .......... .......... .......... .......... .......... 66% 6.44M 11s 175300K .......... .......... .......... .......... .......... 66% 9.51M 11s 175350K .......... .......... .......... .......... .......... 66% 8.58M 11s 175400K .......... .......... .......... .......... .......... 66% 9.29M 11s 175450K .......... .......... .......... .......... .......... 66% 9.93M 11s 175500K .......... .......... .......... .......... .......... 66% 9.46M 11s 175550K .......... .......... .......... .......... .......... 66% 6.18M 11s 175600K .......... .......... .......... .......... .......... 66% 4.51M 11s 175650K .......... .......... .......... .......... .......... 67% 6.96M 11s 175700K .......... .......... .......... .......... .......... 67% 4.48M 11s 175750K .......... .......... .......... .......... .......... 67% 5.13M 11s 175800K .......... .......... .......... .......... .......... 67% 3.70M 11s 175850K .......... .......... .......... .......... .......... 67% 2.75M 11s 175900K .......... .......... .......... .......... .......... 67% 4.81M 11s 175950K .......... .......... .......... .......... .......... 67% 7.86M 11s 176000K .......... .......... .......... .......... .......... 67% 9.70M 11s 176050K .......... .......... .......... .......... .......... 67% 10.0M 11s 176100K .......... .......... .......... .......... .......... 67% 7.67M 11s 176150K .......... .......... .......... .......... .......... 67% 9.17M 11s 176200K .......... .......... .......... .......... .......... 67% 6.81M 11s 176250K .......... .......... .......... .......... .......... 67% 7.64M 11s 176300K .......... .......... .......... .......... .......... 67% 8.25M 11s 176350K .......... .......... .......... .......... .......... 67% 6.65M 11s 176400K .......... .......... .......... .......... .......... 67% 9.26M 11s 176450K .......... .......... .......... .......... .......... 67% 7.08M 11s 176500K .......... .......... .......... .......... .......... 67% 8.19M 11s 176550K .......... .......... .......... .......... .......... 67% 6.14M 11s 176600K .......... .......... .......... .......... .......... 67% 4.76M 11s 176650K .......... .......... .......... .......... .......... 67% 5.89M 11s 176700K .......... .......... .......... .......... .......... 67% 5.39M 11s 176750K .......... .......... .......... .......... .......... 67% 5.48M 11s 176800K .......... .......... .......... .......... .......... 67% 5.94M 11s 176850K .......... .......... .......... .......... .......... 67% 3.80M 11s 176900K .......... .......... .......... .......... .......... 67% 5.99M 11s 176950K .......... .......... .......... .......... .......... 67% 4.98M 11s 177000K .......... .......... .......... .......... .......... 67% 7.01M 11s 177050K .......... .......... .......... .......... .......... 67% 8.49M 11s 177100K .......... .......... .......... .......... .......... 67% 7.83M 11s 177150K .......... .......... .......... .......... .......... 67% 25.4M 11s 177200K .......... .......... .......... .......... .......... 67% 13.6M 11s 177250K .......... .......... .......... .......... .......... 67% 14.9M 11s 177300K .......... .......... .......... .......... .......... 67% 13.8M 11s 177350K .......... .......... .......... .......... .......... 67% 12.4M 11s 177400K .......... .......... .......... .......... .......... 67% 17.2M 11s 177450K .......... .......... .......... .......... .......... 67% 16.0M 11s 177500K .......... .......... .......... .......... .......... 67% 14.7M 11s 177550K .......... .......... .......... .......... .......... 67% 14.8M 11s 177600K .......... .......... .......... .......... .......... 67% 13.7M 11s 177650K .......... .......... .......... .......... .......... 67% 15.2M 11s 177700K .......... .......... .......... .......... .......... 67% 13.5M 11s 177750K .......... .......... .......... .......... .......... 67% 11.0M 11s 177800K .......... .......... .......... .......... .......... 67% 29.8M 11s 177850K .......... .......... .......... .......... .......... 67% 18.3M 11s 177900K .......... .......... .......... .......... .......... 67% 21.1M 11s 177950K .......... .......... .......... .......... .......... 67% 17.2M 11s 178000K .......... .......... .......... .......... .......... 67% 18.5M 11s 178050K .......... .......... .......... .......... .......... 67% 12.5M 11s 178100K .......... .......... .......... .......... .......... 67% 29.3M 11s 178150K .......... .......... .......... .......... .......... 67% 11.0M 11s 178200K .......... .......... .......... .......... .......... 67% 7.96M 11s 178250K .......... .......... .......... .......... .......... 68% 5.78M 11s 178300K .......... .......... .......... .......... .......... 68% 6.08M 11s 178350K .......... .......... .......... .......... .......... 68% 4.93M 11s 178400K .......... .......... .......... .......... .......... 68% 4.92M 11s 178450K .......... .......... .......... .......... .......... 68% 3.59M 11s 178500K .......... .......... .......... .......... .......... 68% 5.80M 11s 178550K .......... .......... .......... .......... .......... 68% 4.15M 11s 178600K .......... .......... .......... .......... .......... 68% 3.43M 11s 178650K .......... .......... .......... .......... .......... 68% 5.20M 11s 178700K .......... .......... .......... .......... .......... 68% 2.71M 11s 178750K .......... .......... .......... .......... .......... 68% 2.59M 11s 178800K .......... .......... .......... .......... .......... 68% 3.45M 11s 178850K .......... .......... .......... .......... .......... 68% 12.6M 11s 178900K .......... .......... .......... .......... .......... 68% 18.2M 11s 178950K .......... .......... .......... .......... .......... 68% 15.7M 11s 179000K .......... .......... .......... .......... .......... 68% 17.2M 11s 179050K .......... .......... .......... .......... .......... 68% 16.7M 11s 179100K .......... .......... .......... .......... .......... 68% 16.3M 11s 179150K .......... .......... .......... .......... .......... 68% 14.5M 11s 179200K .......... .......... .......... .......... .......... 68% 6.99M 11s 179250K .......... .......... .......... .......... .......... 68% 5.84M 11s 179300K .......... .......... .......... .......... .......... 68% 4.01M 11s 179350K .......... .......... .......... .......... .......... 68% 2.82M 11s 179400K .......... .......... .......... .......... .......... 68% 4.07M 11s 179450K .......... .......... .......... .......... .......... 68% 8.48M 11s 179500K .......... .......... .......... .......... .......... 68% 6.62M 11s 179550K .......... .......... .......... .......... .......... 68% 14.8M 11s 179600K .......... .......... .......... .......... .......... 68% 10.3M 11s 179650K .......... .......... .......... .......... .......... 68% 11.1M 11s 179700K .......... .......... .......... .......... .......... 68% 10.7M 11s 179750K .......... .......... .......... .......... .......... 68% 8.85M 11s 179800K .......... .......... .......... .......... .......... 68% 14.8M 11s 179850K .......... .......... .......... .......... .......... 68% 11.3M 11s 179900K .......... .......... .......... .......... .......... 68% 15.1M 11s 179950K .......... .......... .......... .......... .......... 68% 12.3M 11s 180000K .......... .......... .......... .......... .......... 68% 14.7M 11s 180050K .......... .......... .......... .......... .......... 68% 12.1M 11s 180100K .......... .......... .......... .......... .......... 68% 11.6M 11s 180150K .......... .......... .......... .......... .......... 68% 12.6M 11s 180200K .......... .......... .......... .......... .......... 68% 11.3M 10s 180250K .......... .......... .......... .......... .......... 68% 16.5M 10s 180300K .......... .......... .......... .......... .......... 68% 13.7M 10s 180350K .......... .......... .......... .......... .......... 68% 12.9M 10s 180400K .......... .......... .......... .......... .......... 68% 13.7M 10s 180450K .......... .......... .......... .......... .......... 68% 8.84M 10s 180500K .......... .......... .......... .......... .......... 68% 10.1M 10s 180550K .......... .......... .......... .......... .......... 68% 7.84M 10s 180600K .......... .......... .......... .......... .......... 68% 13.9M 10s 180650K .......... .......... .......... .......... .......... 68% 15.8M 10s 180700K .......... .......... .......... .......... .......... 68% 12.2M 10s 180750K .......... .......... .......... .......... .......... 68% 19.4M 10s 180800K .......... .......... .......... .......... .......... 68% 12.8M 10s 180850K .......... .......... .......... .......... .......... 68% 7.77M 10s 180900K .......... .......... .......... .......... .......... 69% 12.1M 10s 180950K .......... .......... .......... .......... .......... 69% 26.5M 10s 181000K .......... .......... .......... .......... .......... 69% 19.0M 10s 181050K .......... .......... .......... .......... .......... 69% 22.8M 10s 181100K .......... .......... .......... .......... .......... 69% 14.5M 10s 181150K .......... .......... .......... .......... .......... 69% 10.4M 10s 181200K .......... .......... .......... .......... .......... 69% 10.6M 10s 181250K .......... .......... .......... .......... .......... 69% 9.36M 10s 181300K .......... .......... .......... .......... .......... 69% 9.90M 10s 181350K .......... .......... .......... .......... .......... 69% 8.52M 10s 181400K .......... .......... .......... .......... .......... 69% 8.61M 10s 181450K .......... .......... .......... .......... .......... 69% 6.41M 10s 181500K .......... .......... .......... .......... .......... 69% 1.81M 10s 181550K .......... .......... .......... .......... .......... 69% 14.1M 10s 181600K .......... .......... .......... .......... .......... 69% 24.8M 10s 181650K .......... .......... .......... .......... .......... 69% 23.0M 10s 181700K .......... .......... .......... .......... .......... 69% 14.9M 10s 181750K .......... .......... .......... .......... .......... 69% 18.4M 10s 181800K .......... .......... .......... .......... .......... 69% 15.7M 10s 181850K .......... .......... .......... .......... .......... 69% 9.02M 10s 181900K .......... .......... .......... .......... .......... 69% 6.60M 10s 181950K .......... .......... .......... .......... .......... 69% 5.55M 10s 182000K .......... .......... .......... .......... .......... 69% 8.64M 10s 182050K .......... .......... .......... .......... .......... 69% 8.69M 10s 182100K .......... .......... .......... .......... .......... 69% 7.58M 10s 182150K .......... .......... .......... .......... .......... 69% 761K 10s 182200K .......... .......... .......... .......... .......... 69% 1.96M 10s 182250K .......... .......... .......... .......... .......... 69% 3.03M 10s 182300K .......... .......... .......... .......... .......... 69% 3.76M 10s 182350K .......... .......... .......... .......... .......... 69% 3.45M 10s 182400K .......... .......... .......... .......... .......... 69% 15.5M 10s 182450K .......... .......... .......... .......... .......... 69% 25.2M 10s 182500K .......... .......... .......... .......... .......... 69% 19.2M 10s 182550K .......... .......... .......... .......... .......... 69% 23.8M 10s 182600K .......... .......... .......... .......... .......... 69% 26.7M 10s 182650K .......... .......... .......... .......... .......... 69% 26.6M 10s 182700K .......... .......... .......... .......... .......... 69% 19.0M 10s 182750K .......... .......... .......... .......... .......... 69% 15.8M 10s 182800K .......... .......... .......... .......... .......... 69% 31.7M 10s 182850K .......... .......... .......... .......... .......... 69% 20.4M 10s 182900K .......... .......... .......... .......... .......... 69% 11.5M 10s 182950K .......... .......... .......... .......... .......... 69% 21.9M 10s 183000K .......... .......... .......... .......... .......... 69% 14.6M 10s 183050K .......... .......... .......... .......... .......... 69% 8.72M 10s 183100K .......... .......... .......... .......... .......... 69% 9.75M 10s 183150K .......... .......... .......... .......... .......... 69% 10.6M 10s 183200K .......... .......... .......... .......... .......... 69% 9.92M 10s 183250K .......... .......... .......... .......... .......... 69% 11.9M 10s 183300K .......... .......... .......... .......... .......... 69% 7.80M 10s 183350K .......... .......... .......... .......... .......... 69% 6.30M 10s 183400K .......... .......... .......... .......... .......... 69% 6.93M 10s 183450K .......... .......... .......... .......... .......... 69% 5.76M 10s 183500K .......... .......... .......... .......... .......... 70% 7.78M 10s 183550K .......... .......... .......... .......... .......... 70% 7.58M 10s 183600K .......... .......... .......... .......... .......... 70% 5.67M 10s 183650K .......... .......... .......... .......... .......... 70% 10.3M 10s 183700K .......... .......... .......... .......... .......... 70% 12.7M 10s 183750K .......... .......... .......... .......... .......... 70% 15.4M 10s 183800K .......... .......... .......... .......... .......... 70% 14.6M 10s 183850K .......... .......... .......... .......... .......... 70% 10.4M 10s 183900K .......... .......... .......... .......... .......... 70% 11.6M 10s 183950K .......... .......... .......... .......... .......... 70% 9.97M 10s 184000K .......... .......... .......... .......... .......... 70% 14.1M 10s 184050K .......... .......... .......... .......... .......... 70% 16.3M 10s 184100K .......... .......... .......... .......... .......... 70% 10.8M 10s 184150K .......... .......... .......... .......... .......... 70% 8.86M 10s 184200K .......... .......... .......... .......... .......... 70% 8.91M 10s 184250K .......... .......... .......... .......... .......... 70% 13.8M 10s 184300K .......... .......... .......... .......... .......... 70% 13.1M 10s 184350K .......... .......... .......... .......... .......... 70% 7.45M 10s 184400K .......... .......... .......... .......... .......... 70% 9.70M 10s 184450K .......... .......... .......... .......... .......... 70% 8.26M 10s 184500K .......... .......... .......... .......... .......... 70% 4.62M 10s 184550K .......... .......... .......... .......... .......... 70% 4.73M 10s 184600K .......... .......... .......... .......... .......... 70% 4.82M 10s 184650K .......... .......... .......... .......... .......... 70% 3.87M 10s 184700K .......... .......... .......... .......... .......... 70% 3.51M 10s 184750K .......... .......... .......... .......... .......... 70% 4.15M 10s 184800K .......... .......... .......... .......... .......... 70% 7.19M 10s 184850K .......... .......... .......... .......... .......... 70% 9.24M 10s 184900K .......... .......... .......... .......... .......... 70% 10.0M 10s 184950K .......... .......... .......... .......... .......... 70% 7.92M 10s 185000K .......... .......... .......... .......... .......... 70% 5.95M 10s 185050K .......... .......... .......... .......... .......... 70% 6.14M 10s 185100K .......... .......... .......... .......... .......... 70% 4.40M 10s 185150K .......... .......... .......... .......... .......... 70% 5.59M 10s 185200K .......... .......... .......... .......... .......... 70% 6.57M 10s 185250K .......... .......... .......... .......... .......... 70% 7.89M 10s 185300K .......... .......... .......... .......... .......... 70% 9.21M 10s 185350K .......... .......... .......... .......... .......... 70% 7.96M 10s 185400K .......... .......... .......... .......... .......... 70% 8.10M 10s 185450K .......... .......... .......... .......... .......... 70% 6.51M 10s 185500K .......... .......... .......... .......... .......... 70% 5.62M 10s 185550K .......... .......... .......... .......... .......... 70% 22.1M 10s 185600K .......... .......... .......... .......... .......... 70% 6.60M 10s 185650K .......... .......... .......... .......... .......... 70% 10.1M 10s 185700K .......... .......... .......... .......... .......... 70% 7.96M 10s 185750K .......... .......... .......... .......... .......... 70% 11.6M 10s 185800K .......... .......... .......... .......... .......... 70% 8.85M 10s 185850K .......... .......... .......... .......... .......... 70% 8.86M 10s 185900K .......... .......... .......... .......... .......... 70% 12.2M 10s 185950K .......... .......... .......... .......... .......... 70% 9.30M 10s 186000K .......... .......... .......... .......... .......... 70% 13.9M 10s 186050K .......... .......... .......... .......... .......... 70% 29.1M 10s 186100K .......... .......... .......... .......... .......... 70% 23.6M 10s 186150K .......... .......... .......... .......... .......... 71% 50.4M 10s 186200K .......... .......... .......... .......... .......... 71% 25.6M 10s 186250K .......... .......... .......... .......... .......... 71% 35.1M 10s 186300K .......... .......... .......... .......... .......... 71% 27.6M 10s 186350K .......... .......... .......... .......... .......... 71% 16.0M 10s 186400K .......... .......... .......... .......... .......... 71% 52.1M 10s 186450K .......... .......... .......... .......... .......... 71% 35.3M 10s 186500K .......... .......... .......... .......... .......... 71% 13.7M 10s 186550K .......... .......... .......... .......... .......... 71% 56.8M 10s 186600K .......... .......... .......... .......... .......... 71% 11.0M 10s 186650K .......... .......... .......... .......... .......... 71% 22.1M 10s 186700K .......... .......... .......... .......... .......... 71% 10.3M 10s 186750K .......... .......... .......... .......... .......... 71% 9.81M 10s 186800K .......... .......... .......... .......... .......... 71% 9.28M 10s 186850K .......... .......... .......... .......... .......... 71% 8.23M 10s 186900K .......... .......... .......... .......... .......... 71% 9.28M 10s 186950K .......... .......... .......... .......... .......... 71% 9.11M 10s 187000K .......... .......... .......... .......... .......... 71% 9.40M 10s 187050K .......... .......... .......... .......... .......... 71% 7.49M 10s 187100K .......... .......... .......... .......... .......... 71% 6.96M 10s 187150K .......... .......... .......... .......... .......... 71% 5.90M 10s 187200K .......... .......... .......... .......... .......... 71% 5.93M 10s 187250K .......... .......... .......... .......... .......... 71% 6.16M 10s 187300K .......... .......... .......... .......... .......... 71% 10.8M 10s 187350K .......... .......... .......... .......... .......... 71% 7.09M 10s 187400K .......... .......... .......... .......... .......... 71% 5.70M 10s 187450K .......... .......... .......... .......... .......... 71% 4.10M 10s 187500K .......... .......... .......... .......... .......... 71% 4.72M 10s 187550K .......... .......... .......... .......... .......... 71% 4.53M 10s 187600K .......... .......... .......... .......... .......... 71% 4.12M 10s 187650K .......... .......... .......... .......... .......... 71% 5.02M 10s 187700K .......... .......... .......... .......... .......... 71% 5.80M 10s 187750K .......... .......... .......... .......... .......... 71% 6.85M 10s 187800K .......... .......... .......... .......... .......... 71% 3.43M 10s 187850K .......... .......... .......... .......... .......... 71% 4.19M 10s 187900K .......... .......... .......... .......... .......... 71% 3.05M 10s 187950K .......... .......... .......... .......... .......... 71% 1.28M 10s 188000K .......... .......... .......... .......... .......... 71% 2.52M 10s 188050K .......... .......... .......... .......... .......... 71% 5.27M 10s 188100K .......... .......... .......... .......... .......... 71% 5.66M 9s 188150K .......... .......... .......... .......... .......... 71% 5.58M 9s 188200K .......... .......... .......... .......... .......... 71% 5.70M 9s 188250K .......... .......... .......... .......... .......... 71% 5.06M 9s 188300K .......... .......... .......... .......... .......... 71% 5.75M 9s 188350K .......... .......... .......... .......... .......... 71% 234K 10s 188400K .......... .......... .......... .......... .......... 71% 3.87M 10s 188450K .......... .......... .......... .......... .......... 71% 7.93M 10s 188500K .......... .......... .......... .......... .......... 71% 8.48M 10s 188550K .......... .......... .......... .......... .......... 71% 8.32M 10s 188600K .......... .......... .......... .......... .......... 71% 5.16M 10s 188650K .......... .......... .......... .......... .......... 71% 6.01M 10s 188700K .......... .......... .......... .......... .......... 71% 3.69M 10s 188750K .......... .......... .......... .......... .......... 72% 3.30M 10s 188800K .......... .......... .......... .......... .......... 72% 4.59M 10s 188850K .......... .......... .......... .......... .......... 72% 5.09M 9s 188900K .......... .......... .......... .......... .......... 72% 4.40M 9s 188950K .......... .......... .......... .......... .......... 72% 2.76M 9s 189000K .......... .......... .......... .......... .......... 72% 3.80M 9s 189050K .......... .......... .......... .......... .......... 72% 10.8M 9s 189100K .......... .......... .......... .......... .......... 72% 13.5M 9s 189150K .......... .......... .......... .......... .......... 72% 15.6M 9s 189200K .......... .......... .......... .......... .......... 72% 11.0M 9s 189250K .......... .......... .......... .......... .......... 72% 16.5M 9s 189300K .......... .......... .......... .......... .......... 72% 11.2M 9s 189350K .......... .......... .......... .......... .......... 72% 10.8M 9s 189400K .......... .......... .......... .......... .......... 72% 12.4M 9s 189450K .......... .......... .......... .......... .......... 72% 7.23M 9s 189500K .......... .......... .......... .......... .......... 72% 5.51M 9s 189550K .......... .......... .......... .......... .......... 72% 4.09M 9s 189600K .......... .......... .......... .......... .......... 72% 5.42M 9s 189650K .......... .......... .......... .......... .......... 72% 6.12M 9s 189700K .......... .......... .......... .......... .......... 72% 6.51M 9s 189750K .......... .......... .......... .......... .......... 72% 5.14M 9s 189800K .......... .......... .......... .......... .......... 72% 5.73M 9s 189850K .......... .......... .......... .......... .......... 72% 4.63M 9s 189900K .......... .......... .......... .......... .......... 72% 5.38M 9s 189950K .......... .......... .......... .......... .......... 72% 4.32M 9s 190000K .......... .......... .......... .......... .......... 72% 6.02M 9s 190050K .......... .......... .......... .......... .......... 72% 15.2M 9s 190100K .......... .......... .......... .......... .......... 72% 9.83M 9s 190150K .......... .......... .......... .......... .......... 72% 20.6M 9s 190200K .......... .......... .......... .......... .......... 72% 6.73M 9s 190250K .......... .......... .......... .......... .......... 72% 7.12M 9s 190300K .......... .......... .......... .......... .......... 72% 6.69M 9s 190350K .......... .......... .......... .......... .......... 72% 3.66M 9s 190400K .......... .......... .......... .......... .......... 72% 4.87M 9s 190450K .......... .......... .......... .......... .......... 72% 3.11M 9s 190500K .......... .......... .......... .......... .......... 72% 12.3M 9s 190550K .......... .......... .......... .......... .......... 72% 23.9M 9s 190600K .......... .......... .......... .......... .......... 72% 34.4M 9s 190650K .......... .......... .......... .......... .......... 72% 42.8M 9s 190700K .......... .......... .......... .......... .......... 72% 40.8M 9s 190750K .......... .......... .......... .......... .......... 72% 20.9M 9s 190800K .......... .......... .......... .......... .......... 72% 30.7M 9s 190850K .......... .......... .......... .......... .......... 72% 8.78M 9s 190900K .......... .......... .......... .......... .......... 72% 37.3M 9s 190950K .......... .......... .......... .......... .......... 72% 12.6M 9s 191000K .......... .......... .......... .......... .......... 72% 8.17M 9s 191050K .......... .......... .......... .......... .......... 72% 28.1M 9s 191100K .......... .......... .......... .......... .......... 72% 12.0M 9s 191150K .......... .......... .......... .......... .......... 72% 8.29M 9s 191200K .......... .......... .......... .......... .......... 72% 9.38M 9s 191250K .......... .......... .......... .......... .......... 72% 11.0M 9s 191300K .......... .......... .......... .......... .......... 72% 11.3M 9s 191350K .......... .......... .......... .......... .......... 73% 8.50M 9s 191400K .......... .......... .......... .......... .......... 73% 9.09M 9s 191450K .......... .......... .......... .......... .......... 73% 6.75M 9s 191500K .......... .......... .......... .......... .......... 73% 8.24M 9s 191550K .......... .......... .......... .......... .......... 73% 6.91M 9s 191600K .......... .......... .......... .......... .......... 73% 6.66M 9s 191650K .......... .......... .......... .......... .......... 73% 8.63M 9s 191700K .......... .......... .......... .......... .......... 73% 9.65M 9s 191750K .......... .......... .......... .......... .......... 73% 14.0M 9s 191800K .......... .......... .......... .......... .......... 73% 19.2M 9s 191850K .......... .......... .......... .......... .......... 73% 15.6M 9s 191900K .......... .......... .......... .......... .......... 73% 11.0M 9s 191950K .......... .......... .......... .......... .......... 73% 15.2M 9s 192000K .......... .......... .......... .......... .......... 73% 10.1M 9s 192050K .......... .......... .......... .......... .......... 73% 11.4M 9s 192100K .......... .......... .......... .......... .......... 73% 6.31M 9s 192150K .......... .......... .......... .......... .......... 73% 6.74M 9s 192200K .......... .......... .......... .......... .......... 73% 4.73M 9s 192250K .......... .......... .......... .......... .......... 73% 4.10M 9s 192300K .......... .......... .......... .......... .......... 73% 3.85M 9s 192350K .......... .......... .......... .......... .......... 73% 5.36M 9s 192400K .......... .......... .......... .......... .......... 73% 14.1M 9s 192450K .......... .......... .......... .......... .......... 73% 11.1M 9s 192500K .......... .......... .......... .......... .......... 73% 11.1M 9s 192550K .......... .......... .......... .......... .......... 73% 12.7M 9s 192600K .......... .......... .......... .......... .......... 73% 9.00M 9s 192650K .......... .......... .......... .......... .......... 73% 9.42M 9s 192700K .......... .......... .......... .......... .......... 73% 7.75M 9s 192750K .......... .......... .......... .......... .......... 73% 11.0M 9s 192800K .......... .......... .......... .......... .......... 73% 9.40M 9s 192850K .......... .......... .......... .......... .......... 73% 9.61M 9s 192900K .......... .......... .......... .......... .......... 73% 11.2M 9s 192950K .......... .......... .......... .......... .......... 73% 9.01M 9s 193000K .......... .......... .......... .......... .......... 73% 10.6M 9s 193050K .......... .......... .......... .......... .......... 73% 11.7M 9s 193100K .......... .......... .......... .......... .......... 73% 6.42M 9s 193150K .......... .......... .......... .......... .......... 73% 6.15M 9s 193200K .......... .......... .......... .......... .......... 73% 5.12M 9s 193250K .......... .......... .......... .......... .......... 73% 4.21M 9s 193300K .......... .......... .......... .......... .......... 73% 4.20M 9s 193350K .......... .......... .......... .......... .......... 73% 4.07M 9s 193400K .......... .......... .......... .......... .......... 73% 14.4M 9s 193450K .......... .......... .......... .......... .......... 73% 12.9M 9s 193500K .......... .......... .......... .......... .......... 73% 11.8M 9s 193550K .......... .......... .......... .......... .......... 73% 10.7M 9s 193600K .......... .......... .......... .......... .......... 73% 12.2M 9s 193650K .......... .......... .......... .......... .......... 73% 8.20M 9s 193700K .......... .......... .......... .......... .......... 73% 7.90M 9s 193750K .......... .......... .......... .......... .......... 73% 7.32M 9s 193800K .......... .......... .......... .......... .......... 73% 231K 9s 193850K .......... .......... .......... .......... .......... 73% 5.89M 9s 193900K .......... .......... .......... .......... .......... 73% 7.59M 9s 193950K .......... .......... .......... .......... .......... 73% 6.32M 9s 194000K .......... .......... .......... .......... .......... 74% 6.66M 9s 194050K .......... .......... .......... .......... .......... 74% 5.87M 9s 194100K .......... .......... .......... .......... .......... 74% 6.28M 9s 194150K .......... .......... .......... .......... .......... 74% 9.59M 9s 194200K .......... .......... .......... .......... .......... 74% 12.9M 9s 194250K .......... .......... .......... .......... .......... 74% 10.6M 9s 194300K .......... .......... .......... .......... .......... 74% 8.09M 9s 194350K .......... .......... .......... .......... .......... 74% 13.9M 9s 194400K .......... .......... .......... .......... .......... 74% 12.8M 9s 194450K .......... .......... .......... .......... .......... 74% 10.2M 9s 194500K .......... .......... .......... .......... .......... 74% 13.6M 9s 194550K .......... .......... .......... .......... .......... 74% 10.5M 9s 194600K .......... .......... .......... .......... .......... 74% 10.0M 9s 194650K .......... .......... .......... .......... .......... 74% 9.35M 9s 194700K .......... .......... .......... .......... .......... 74% 13.5M 9s 194750K .......... .......... .......... .......... .......... 74% 14.3M 9s 194800K .......... .......... .......... .......... .......... 74% 14.6M 9s 194850K .......... .......... .......... .......... .......... 74% 12.8M 9s 194900K .......... .......... .......... .......... .......... 74% 16.8M 9s 194950K .......... .......... .......... .......... .......... 74% 12.1M 9s 195000K .......... .......... .......... .......... .......... 74% 17.1M 9s 195050K .......... .......... .......... .......... .......... 74% 10.9M 9s 195100K .......... .......... .......... .......... .......... 74% 7.52M 9s 195150K .......... .......... .......... .......... .......... 74% 9.04M 9s 195200K .......... .......... .......... .......... .......... 74% 7.52M 9s 195250K .......... .......... .......... .......... .......... 74% 5.89M 9s 195300K .......... .......... .......... .......... .......... 74% 7.50M 9s 195350K .......... .......... .......... .......... .......... 74% 6.99M 9s 195400K .......... .......... .......... .......... .......... 74% 7.05M 9s 195450K .......... .......... .......... .......... .......... 74% 5.32M 9s 195500K .......... .......... .......... .......... .......... 74% 14.3M 9s 195550K .......... .......... .......... .......... .......... 74% 20.3M 9s 195600K .......... .......... .......... .......... .......... 74% 22.7M 9s 195650K .......... .......... .......... .......... .......... 74% 12.9M 9s 195700K .......... .......... .......... .......... .......... 74% 11.3M 9s 195750K .......... .......... .......... .......... .......... 74% 17.8M 9s 195800K .......... .......... .......... .......... .......... 74% 14.8M 9s 195850K .......... .......... .......... .......... .......... 74% 10.8M 9s 195900K .......... .......... .......... .......... .......... 74% 10.9M 9s 195950K .......... .......... .......... .......... .......... 74% 8.83M 9s 196000K .......... .......... .......... .......... .......... 74% 9.56M 9s 196050K .......... .......... .......... .......... .......... 74% 8.23M 9s 196100K .......... .......... .......... .......... .......... 74% 10.3M 9s 196150K .......... .......... .......... .......... .......... 74% 7.66M 9s 196200K .......... .......... .......... .......... .......... 74% 7.98M 9s 196250K .......... .......... .......... .......... .......... 74% 8.30M 9s 196300K .......... .......... .......... .......... .......... 74% 7.88M 9s 196350K .......... .......... .......... .......... .......... 74% 8.16M 9s 196400K .......... .......... .......... .......... .......... 74% 6.91M 9s 196450K .......... .......... .......... .......... .......... 74% 5.59M 9s 196500K .......... .......... .......... .......... .......... 74% 7.16M 9s 196550K .......... .......... .......... .......... .......... 74% 7.36M 9s 196600K .......... .......... .......... .......... .......... 75% 8.37M 9s 196650K .......... .......... .......... .......... .......... 75% 8.58M 9s 196700K .......... .......... .......... .......... .......... 75% 5.93M 9s 196750K .......... .......... .......... .......... .......... 75% 6.88M 9s 196800K .......... .......... .......... .......... .......... 75% 8.29M 9s 196850K .......... .......... .......... .......... .......... 75% 6.15M 9s 196900K .......... .......... .......... .......... .......... 75% 8.10M 8s 196950K .......... .......... .......... .......... .......... 75% 17.3M 8s 197000K .......... .......... .......... .......... .......... 75% 14.2M 8s 197050K .......... .......... .......... .......... .......... 75% 26.5M 8s 197100K .......... .......... .......... .......... .......... 75% 9.52M 8s 197150K .......... .......... .......... .......... .......... 75% 13.5M 8s 197200K .......... .......... .......... .......... .......... 75% 12.1M 8s 197250K .......... .......... .......... .......... .......... 75% 8.14M 8s 197300K .......... .......... .......... .......... .......... 75% 16.0M 8s 197350K .......... .......... .......... .......... .......... 75% 8.67M 8s 197400K .......... .......... .......... .......... .......... 75% 8.94M 8s 197450K .......... .......... .......... .......... .......... 75% 8.41M 8s 197500K .......... .......... .......... .......... .......... 75% 8.48M 8s 197550K .......... .......... .......... .......... .......... 75% 9.40M 8s 197600K .......... .......... .......... .......... .......... 75% 9.67M 8s 197650K .......... .......... .......... .......... .......... 75% 14.9M 8s 197700K .......... .......... .......... .......... .......... 75% 12.6M 8s 197750K .......... .......... .......... .......... .......... 75% 13.2M 8s 197800K .......... .......... .......... .......... .......... 75% 29.2M 8s 197850K .......... .......... .......... .......... .......... 75% 7.38M 8s 197900K .......... .......... .......... .......... .......... 75% 14.0M 8s 197950K .......... .......... .......... .......... .......... 75% 9.09M 8s 198000K .......... .......... .......... .......... .......... 75% 9.15M 8s 198050K .......... .......... .......... .......... .......... 75% 8.81M 8s 198100K .......... .......... .......... .......... .......... 75% 8.66M 8s 198150K .......... .......... .......... .......... .......... 75% 8.53M 8s 198200K .......... .......... .......... .......... .......... 75% 9.70M 8s 198250K .......... .......... .......... .......... .......... 75% 10.2M 8s 198300K .......... .......... .......... .......... .......... 75% 14.6M 8s 198350K .......... .......... .......... .......... .......... 75% 10.4M 8s 198400K .......... .......... .......... .......... .......... 75% 16.5M 8s 198450K .......... .......... .......... .......... .......... 75% 7.11M 8s 198500K .......... .......... .......... .......... .......... 75% 12.7M 8s 198550K .......... .......... .......... .......... .......... 75% 10.1M 8s 198600K .......... .......... .......... .......... .......... 75% 9.50M 8s 198650K .......... .......... .......... .......... .......... 75% 11.2M 8s 198700K .......... .......... .......... .......... .......... 75% 4.02M 8s 198750K .......... .......... .......... .......... .......... 75% 3.72M 8s 198800K .......... .......... .......... .......... .......... 75% 4.51M 8s 198850K .......... .......... .......... .......... .......... 75% 3.00M 8s 198900K .......... .......... .......... .......... .......... 75% 2.72M 8s 198950K .......... .......... .......... .......... .......... 75% 3.31M 8s 199000K .......... .......... .......... .......... .......... 75% 16.3M 8s 199050K .......... .......... .......... .......... .......... 75% 20.2M 8s 199100K .......... .......... .......... .......... .......... 75% 16.4M 8s 199150K .......... .......... .......... .......... .......... 75% 32.8M 8s 199200K .......... .......... .......... .......... .......... 75% 15.1M 8s 199250K .......... .......... .......... .......... .......... 76% 20.4M 8s 199300K .......... .......... .......... .......... .......... 76% 21.4M 8s 199350K .......... .......... .......... .......... .......... 76% 17.1M 8s 199400K .......... .......... .......... .......... .......... 76% 16.5M 8s 199450K .......... .......... .......... .......... .......... 76% 10.3M 8s 199500K .......... .......... .......... .......... .......... 76% 17.9M 8s 199550K .......... .......... .......... .......... .......... 76% 13.1M 8s 199600K .......... .......... .......... .......... .......... 76% 6.41M 8s 199650K .......... .......... .......... .......... .......... 76% 10.8M 8s 199700K .......... .......... .......... .......... .......... 76% 6.83M 8s 199750K .......... .......... .......... .......... .......... 76% 8.94M 8s 199800K .......... .......... .......... .......... .......... 76% 8.17M 8s 199850K .......... .......... .......... .......... .......... 76% 4.48M 8s 199900K .......... .......... .......... .......... .......... 76% 3.88M 8s 199950K .......... .......... .......... .......... .......... 76% 3.90M 8s 200000K .......... .......... .......... .......... .......... 76% 3.00M 8s 200050K .......... .......... .......... .......... .......... 76% 3.42M 8s 200100K .......... .......... .......... .......... .......... 76% 3.67M 8s 200150K .......... .......... .......... .......... .......... 76% 18.8M 8s 200200K .......... .......... .......... .......... .......... 76% 14.3M 8s 200250K .......... .......... .......... .......... .......... 76% 16.8M 8s 200300K .......... .......... .......... .......... .......... 76% 16.6M 8s 200350K .......... .......... .......... .......... .......... 76% 11.0M 8s 200400K .......... .......... .......... .......... .......... 76% 16.0M 8s 200450K .......... .......... .......... .......... .......... 76% 14.8M 8s 200500K .......... .......... .......... .......... .......... 76% 9.18M 8s 200550K .......... .......... .......... .......... .......... 76% 7.91M 8s 200600K .......... .......... .......... .......... .......... 76% 5.95M 8s 200650K .......... .......... .......... .......... .......... 76% 6.90M 8s 200700K .......... .......... .......... .......... .......... 76% 6.14M 8s 200750K .......... .......... .......... .......... .......... 76% 9.59M 8s 200800K .......... .......... .......... .......... .......... 76% 10.5M 8s 200850K .......... .......... .......... .......... .......... 76% 17.5M 8s 200900K .......... .......... .......... .......... .......... 76% 11.6M 8s 200950K .......... .......... .......... .......... .......... 76% 12.7M 8s 201000K .......... .......... .......... .......... .......... 76% 15.3M 8s 201050K .......... .......... .......... .......... .......... 76% 10.6M 8s 201100K .......... .......... .......... .......... .......... 76% 14.4M 8s 201150K .......... .......... .......... .......... .......... 76% 15.2M 8s 201200K .......... .......... .......... .......... .......... 76% 5.99M 8s 201250K .......... .......... .......... .......... .......... 76% 10.8M 8s 201300K .......... .......... .......... .......... .......... 76% 11.3M 8s 201350K .......... .......... .......... .......... .......... 76% 12.1M 8s 201400K .......... .......... .......... .......... .......... 76% 11.9M 8s 201450K .......... .......... .......... .......... .......... 76% 9.96M 8s 201500K .......... .......... .......... .......... .......... 76% 10.5M 8s 201550K .......... .......... .......... .......... .......... 76% 11.4M 8s 201600K .......... .......... .......... .......... .......... 76% 8.48M 8s 201650K .......... .......... .......... .......... .......... 76% 10.4M 8s 201700K .......... .......... .......... .......... .......... 76% 8.24M 8s 201750K .......... .......... .......... .......... .......... 76% 10.4M 8s 201800K .......... .......... .......... .......... .......... 76% 8.52M 8s 201850K .......... .......... .......... .......... .......... 77% 5.98M 8s 201900K .......... .......... .......... .......... .......... 77% 7.24M 8s 201950K .......... .......... .......... .......... .......... 77% 7.23M 8s 202000K .......... .......... .......... .......... .......... 77% 9.10M 8s 202050K .......... .......... .......... .......... .......... 77% 7.47M 8s 202100K .......... .......... .......... .......... .......... 77% 6.46M 8s 202150K .......... .......... .......... .......... .......... 77% 5.79M 8s 202200K .......... .......... .......... .......... .......... 77% 7.33M 8s 202250K .......... .......... .......... .......... .......... 77% 10.6M 8s 202300K .......... .......... .......... .......... .......... 77% 10.9M 8s 202350K .......... .......... .......... .......... .......... 77% 9.87M 8s 202400K .......... .......... .......... .......... .......... 77% 13.0M 8s 202450K .......... .......... .......... .......... .......... 77% 11.4M 8s 202500K .......... .......... .......... .......... .......... 77% 10.5M 8s 202550K .......... .......... .......... .......... .......... 77% 13.1M 8s 202600K .......... .......... .......... .......... .......... 77% 9.16M 8s 202650K .......... .......... .......... .......... .......... 77% 8.74M 8s 202700K .......... .......... .......... .......... .......... 77% 8.74M 8s 202750K .......... .......... .......... .......... .......... 77% 10.0M 8s 202800K .......... .......... .......... .......... .......... 77% 8.21M 8s 202850K .......... .......... .......... .......... .......... 77% 10.0M 8s 202900K .......... .......... .......... .......... .......... 77% 11.5M 8s 202950K .......... .......... .......... .......... .......... 77% 14.4M 8s 203000K .......... .......... .......... .......... .......... 77% 19.9M 8s 203050K .......... .......... .......... .......... .......... 77% 17.1M 8s 203100K .......... .......... .......... .......... .......... 77% 13.6M 8s 203150K .......... .......... .......... .......... .......... 77% 17.0M 8s 203200K .......... .......... .......... .......... .......... 77% 13.7M 8s 203250K .......... .......... .......... .......... .......... 77% 24.5M 8s 203300K .......... .......... .......... .......... .......... 77% 21.3M 8s 203350K .......... .......... .......... .......... .......... 77% 17.2M 8s 203400K .......... .......... .......... .......... .......... 77% 20.8M 8s 203450K .......... .......... .......... .......... .......... 77% 22.1M 8s 203500K .......... .......... .......... .......... .......... 77% 14.3M 8s 203550K .......... .......... .......... .......... .......... 77% 9.59M 8s 203600K .......... .......... .......... .......... .......... 77% 7.13M 8s 203650K .......... .......... .......... .......... .......... 77% 5.96M 8s 203700K .......... .......... .......... .......... .......... 77% 9.17M 8s 203750K .......... .......... .......... .......... .......... 77% 8.80M 8s 203800K .......... .......... .......... .......... .......... 77% 8.58M 8s 203850K .......... .......... .......... .......... .......... 77% 6.74M 8s 203900K .......... .......... .......... .......... .......... 77% 8.42M 8s 203950K .......... .......... .......... .......... .......... 77% 9.18M 8s 204000K .......... .......... .......... .......... .......... 77% 6.78M 8s 204050K .......... .......... .......... .......... .......... 77% 21.1M 8s 204100K .......... .......... .......... .......... .......... 77% 32.7M 8s 204150K .......... .......... .......... .......... .......... 77% 22.4M 8s 204200K .......... .......... .......... .......... .......... 77% 66.5M 7s 204250K .......... .......... .......... .......... .......... 77% 43.0M 7s 204300K .......... .......... .......... .......... .......... 77% 33.0M 7s 204350K .......... .......... .......... .......... .......... 77% 25.1M 7s 204400K .......... .......... .......... .......... .......... 77% 28.9M 7s 204450K .......... .......... .......... .......... .......... 77% 15.7M 7s 204500K .......... .......... .......... .......... .......... 78% 29.2M 7s 204550K .......... .......... .......... .......... .......... 78% 26.5M 7s 204600K .......... .......... .......... .......... .......... 78% 19.3M 7s 204650K .......... .......... .......... .......... .......... 78% 21.1M 7s 204700K .......... .......... .......... .......... .......... 78% 13.3M 7s 204750K .......... .......... .......... .......... .......... 78% 14.2M 7s 204800K .......... .......... .......... .......... .......... 78% 11.2M 7s 204850K .......... .......... .......... .......... .......... 78% 7.66M 7s 204900K .......... .......... .......... .......... .......... 78% 10.9M 7s 204950K .......... .......... .......... .......... .......... 78% 8.35M 7s 205000K .......... .......... .......... .......... .......... 78% 9.91M 7s 205050K .......... .......... .......... .......... .......... 78% 5.77M 7s 205100K .......... .......... .......... .......... .......... 78% 6.25M 7s 205150K .......... .......... .......... .......... .......... 78% 10.6M 7s 205200K .......... .......... .......... .......... .......... 78% 8.17M 7s 205250K .......... .......... .......... .......... .......... 78% 10.4M 7s 205300K .......... .......... .......... .......... .......... 78% 12.0M 7s 205350K .......... .......... .......... .......... .......... 78% 7.20M 7s 205400K .......... .......... .......... .......... .......... 78% 10.2M 7s 205450K .......... .......... .......... .......... .......... 78% 9.96M 7s 205500K .......... .......... .......... .......... .......... 78% 15.3M 7s 205550K .......... .......... .......... .......... .......... 78% 12.7M 7s 205600K .......... .......... .......... .......... .......... 78% 10.2M 7s 205650K .......... .......... .......... .......... .......... 78% 10.1M 7s 205700K .......... .......... .......... .......... .......... 78% 11.5M 7s 205750K .......... .......... .......... .......... .......... 78% 8.97M 7s 205800K .......... .......... .......... .......... .......... 78% 9.61M 7s 205850K .......... .......... .......... .......... .......... 78% 8.03M 7s 205900K .......... .......... .......... .......... .......... 78% 9.45M 7s 205950K .......... .......... .......... .......... .......... 78% 6.19M 7s 206000K .......... .......... .......... .......... .......... 78% 9.80M 7s 206050K .......... .......... .......... .......... .......... 78% 12.2M 7s 206100K .......... .......... .......... .......... .......... 78% 11.9M 7s 206150K .......... .......... .......... .......... .......... 78% 12.2M 7s 206200K .......... .......... .......... .......... .......... 78% 13.4M 7s 206250K .......... .......... .......... .......... .......... 78% 9.19M 7s 206300K .......... .......... .......... .......... .......... 78% 7.44M 7s 206350K .......... .......... .......... .......... .......... 78% 7.48M 7s 206400K .......... .......... .......... .......... .......... 78% 4.97M 7s 206450K .......... .......... .......... .......... .......... 78% 3.57M 7s 206500K .......... .......... .......... .......... .......... 78% 5.01M 7s 206550K .......... .......... .......... .......... .......... 78% 13.6M 7s 206600K .......... .......... .......... .......... .......... 78% 14.2M 7s 206650K .......... .......... .......... .......... .......... 78% 15.8M 7s 206700K .......... .......... .......... .......... .......... 78% 9.45M 7s 206750K .......... .......... .......... .......... .......... 78% 8.16M 7s 206800K .......... .......... .......... .......... .......... 78% 10.3M 7s 206850K .......... .......... .......... .......... .......... 78% 7.03M 7s 206900K .......... .......... .......... .......... .......... 78% 7.78M 7s 206950K .......... .......... .......... .......... .......... 78% 4.49M 7s 207000K .......... .......... .......... .......... .......... 78% 7.15M 7s 207050K .......... .......... .......... .......... .......... 78% 6.73M 7s 207100K .......... .......... .......... .......... .......... 79% 5.28M 7s 207150K .......... .......... .......... .......... .......... 79% 8.72M 7s 207200K .......... .......... .......... .......... .......... 79% 8.30M 7s 207250K .......... .......... .......... .......... .......... 79% 8.68M 7s 207300K .......... .......... .......... .......... .......... 79% 14.0M 7s 207350K .......... .......... .......... .......... .......... 79% 17.9M 7s 207400K .......... .......... .......... .......... .......... 79% 16.2M 7s 207450K .......... .......... .......... .......... .......... 79% 13.1M 7s 207500K .......... .......... .......... .......... .......... 79% 16.5M 7s 207550K .......... .......... .......... .......... .......... 79% 24.8M 7s 207600K .......... .......... .......... .......... .......... 79% 12.0M 7s 207650K .......... .......... .......... .......... .......... 79% 16.0M 7s 207700K .......... .......... .......... .......... .......... 79% 13.0M 7s 207750K .......... .......... .......... .......... .......... 79% 17.3M 7s 207800K .......... .......... .......... .......... .......... 79% 18.9M 7s 207850K .......... .......... .......... .......... .......... 79% 9.68M 7s 207900K .......... .......... .......... .......... .......... 79% 19.7M 7s 207950K .......... .......... .......... .......... .......... 79% 11.8M 7s 208000K .......... .......... .......... .......... .......... 79% 12.2M 7s 208050K .......... .......... .......... .......... .......... 79% 17.1M 7s 208100K .......... .......... .......... .......... .......... 79% 14.2M 7s 208150K .......... .......... .......... .......... .......... 79% 12.4M 7s 208200K .......... .......... .......... .......... .......... 79% 14.0M 7s 208250K .......... .......... .......... .......... .......... 79% 8.86M 7s 208300K .......... .......... .......... .......... .......... 79% 7.41M 7s 208350K .......... .......... .......... .......... .......... 79% 10.6M 7s 208400K .......... .......... .......... .......... .......... 79% 19.7M 7s 208450K .......... .......... .......... .......... .......... 79% 14.4M 7s 208500K .......... .......... .......... .......... .......... 79% 15.8M 7s 208550K .......... .......... .......... .......... .......... 79% 14.0M 7s 208600K .......... .......... .......... .......... .......... 79% 12.8M 7s 208650K .......... .......... .......... .......... .......... 79% 12.1M 7s 208700K .......... .......... .......... .......... .......... 79% 9.93M 7s 208750K .......... .......... .......... .......... .......... 79% 18.0M 7s 208800K .......... .......... .......... .......... .......... 79% 20.8M 7s 208850K .......... .......... .......... .......... .......... 79% 12.0M 7s 208900K .......... .......... .......... .......... .......... 79% 7.75M 7s 208950K .......... .......... .......... .......... .......... 79% 26.8M 7s 209000K .......... .......... .......... .......... .......... 79% 75.5M 7s 209050K .......... .......... .......... .......... .......... 79% 15.0M 7s 209100K .......... .......... .......... .......... .......... 79% 38.1M 7s 209150K .......... .......... .......... .......... .......... 79% 88.0M 7s 209200K .......... .......... .......... .......... .......... 79% 39.0M 7s 209250K .......... .......... .......... .......... .......... 79% 13.4M 7s 209300K .......... .......... .......... .......... .......... 79% 9.12M 7s 209350K .......... .......... .......... .......... .......... 79% 10.4M 7s 209400K .......... .......... .......... .......... .......... 79% 12.5M 7s 209450K .......... .......... .......... .......... .......... 79% 10.8M 7s 209500K .......... .......... .......... .......... .......... 79% 12.8M 7s 209550K .......... .......... .......... .......... .......... 79% 14.1M 7s 209600K .......... .......... .......... .......... .......... 79% 10.3M 7s 209650K .......... .......... .......... .......... .......... 79% 11.0M 7s 209700K .......... .......... .......... .......... .......... 79% 7.82M 7s 209750K .......... .......... .......... .......... .......... 80% 10.6M 7s 209800K .......... .......... .......... .......... .......... 80% 10.8M 7s 209850K .......... .......... .......... .......... .......... 80% 8.09M 7s 209900K .......... .......... .......... .......... .......... 80% 8.51M 7s 209950K .......... .......... .......... .......... .......... 80% 8.54M 7s 210000K .......... .......... .......... .......... .......... 80% 9.18M 7s 210050K .......... .......... .......... .......... .......... 80% 9.69M 7s 210100K .......... .......... .......... .......... .......... 80% 8.38M 7s 210150K .......... .......... .......... .......... .......... 80% 9.96M 7s 210200K .......... .......... .......... .......... .......... 80% 10.3M 7s 210250K .......... .......... .......... .......... .......... 80% 14.7M 7s 210300K .......... .......... .......... .......... .......... 80% 23.7M 7s 210350K .......... .......... .......... .......... .......... 80% 12.6M 7s 210400K .......... .......... .......... .......... .......... 80% 32.0M 7s 210450K .......... .......... .......... .......... .......... 80% 10.5M 7s 210500K .......... .......... .......... .......... .......... 80% 3.48M 7s 210550K .......... .......... .......... .......... .......... 80% 186M 7s 210600K .......... .......... .......... .......... .......... 80% 10.1M 7s 210650K .......... .......... .......... .......... .......... 80% 10.4M 7s 210700K .......... .......... .......... .......... .......... 80% 9.66M 7s 210750K .......... .......... .......... .......... .......... 80% 12.4M 7s 210800K .......... .......... .......... .......... .......... 80% 14.6M 7s 210850K .......... .......... .......... .......... .......... 80% 18.6M 7s 210900K .......... .......... .......... .......... .......... 80% 19.0M 7s 210950K .......... .......... .......... .......... .......... 80% 8.18M 7s 211000K .......... .......... .......... .......... .......... 80% 26.4M 7s 211050K .......... .......... .......... .......... .......... 80% 10.3M 7s 211100K .......... .......... .......... .......... .......... 80% 9.48M 7s 211150K .......... .......... .......... .......... .......... 80% 10.4M 7s 211200K .......... .......... .......... .......... .......... 80% 7.53M 7s 211250K .......... .......... .......... .......... .......... 80% 9.64M 7s 211300K .......... .......... .......... .......... .......... 80% 11.0M 7s 211350K .......... .......... .......... .......... .......... 80% 9.65M 7s 211400K .......... .......... .......... .......... .......... 80% 17.5M 6s 211450K .......... .......... .......... .......... .......... 80% 12.9M 6s 211500K .......... .......... .......... .......... .......... 80% 21.0M 6s 211550K .......... .......... .......... .......... .......... 80% 13.7M 6s 211600K .......... .......... .......... .......... .......... 80% 17.4M 6s 211650K .......... .......... .......... .......... .......... 80% 14.7M 6s 211700K .......... .......... .......... .......... .......... 80% 8.84M 6s 211750K .......... .......... .......... .......... .......... 80% 20.1M 6s 211800K .......... .......... .......... .......... .......... 80% 9.93M 6s 211850K .......... .......... .......... .......... .......... 80% 23.7M 6s 211900K .......... .......... .......... .......... .......... 80% 18.4M 6s 211950K .......... .......... .......... .......... .......... 80% 16.7M 6s 212000K .......... .......... .......... .......... .......... 80% 13.2M 6s 212050K .......... .......... .......... .......... .......... 80% 13.7M 6s 212100K .......... .......... .......... .......... .......... 80% 9.79M 6s 212150K .......... .......... .......... .......... .......... 80% 8.28M 6s 212200K .......... .......... .......... .......... .......... 80% 6.90M 6s 212250K .......... .......... .......... .......... .......... 80% 8.27M 6s 212300K .......... .......... .......... .......... .......... 80% 10.9M 6s 212350K .......... .......... .......... .......... .......... 81% 6.14M 6s 212400K .......... .......... .......... .......... .......... 81% 7.85M 6s 212450K .......... .......... .......... .......... .......... 81% 1.93M 6s 212500K .......... .......... .......... .......... .......... 81% 5.10M 6s 212550K .......... .......... .......... .......... .......... 81% 5.48M 6s 212600K .......... .......... .......... .......... .......... 81% 4.40M 6s 212650K .......... .......... .......... .......... .......... 81% 15.4M 6s 212700K .......... .......... .......... .......... .......... 81% 33.9M 6s 212750K .......... .......... .......... .......... .......... 81% 30.0M 6s 212800K .......... .......... .......... .......... .......... 81% 57.8M 6s 212850K .......... .......... .......... .......... .......... 81% 61.7M 6s 212900K .......... .......... .......... .......... .......... 81% 38.0M 6s 212950K .......... .......... .......... .......... .......... 81% 44.2M 6s 213000K .......... .......... .......... .......... .......... 81% 31.9M 6s 213050K .......... .......... .......... .......... .......... 81% 34.0M 6s 213100K .......... .......... .......... .......... .......... 81% 82.2M 6s 213150K .......... .......... .......... .......... .......... 81% 62.5M 6s 213200K .......... .......... .......... .......... .......... 81% 25.4M 6s 213250K .......... .......... .......... .......... .......... 81% 50.5M 6s 213300K .......... .......... .......... .......... .......... 81% 80.4M 6s 213350K .......... .......... .......... .......... .......... 81% 20.9M 6s 213400K .......... .......... .......... .......... .......... 81% 135M 6s 213450K .......... .......... .......... .......... .......... 81% 28.0M 6s 213500K .......... .......... .......... .......... .......... 81% 12.7M 6s 213550K .......... .......... .......... .......... .......... 81% 134M 6s 213600K .......... .......... .......... .......... .......... 81% 21.2M 6s 213650K .......... .......... .......... .......... .......... 81% 19.3M 6s 213700K .......... .......... .......... .......... .......... 81% 12.3M 6s 213750K .......... .......... .......... .......... .......... 81% 12.0M 6s 213800K .......... .......... .......... .......... .......... 81% 12.1M 6s 213850K .......... .......... .......... .......... .......... 81% 10.7M 6s 213900K .......... .......... .......... .......... .......... 81% 10.5M 6s 213950K .......... .......... .......... .......... .......... 81% 12.9M 6s 214000K .......... .......... .......... .......... .......... 81% 14.0M 6s 214050K .......... .......... .......... .......... .......... 81% 8.85M 6s 214100K .......... .......... .......... .......... .......... 81% 11.2M 6s 214150K .......... .......... .......... .......... .......... 81% 11.8M 6s 214200K .......... .......... .......... .......... .......... 81% 8.12M 6s 214250K .......... .......... .......... .......... .......... 81% 11.6M 6s 214300K .......... .......... .......... .......... .......... 81% 10.1M 6s 214350K .......... .......... .......... .......... .......... 81% 8.82M 6s 214400K .......... .......... .......... .......... .......... 81% 13.2M 6s 214450K .......... .......... .......... .......... .......... 81% 10.5M 6s 214500K .......... .......... .......... .......... .......... 81% 9.67M 6s 214550K .......... .......... .......... .......... .......... 81% 10.9M 6s 214600K .......... .......... .......... .......... .......... 81% 5.98M 6s 214650K .......... .......... .......... .......... .......... 81% 7.78M 6s 214700K .......... .......... .......... .......... .......... 81% 6.93M 6s 214750K .......... .......... .......... .......... .......... 81% 6.59M 6s 214800K .......... .......... .......... .......... .......... 81% 6.26M 6s 214850K .......... .......... .......... .......... .......... 81% 8.17M 6s 214900K .......... .......... .......... .......... .......... 81% 11.6M 6s 214950K .......... .......... .......... .......... .......... 82% 9.07M 6s 215000K .......... .......... .......... .......... .......... 82% 7.24M 6s 215050K .......... .......... .......... .......... .......... 82% 9.92M 6s 215100K .......... .......... .......... .......... .......... 82% 7.83M 6s 215150K .......... .......... .......... .......... .......... 82% 6.30M 6s 215200K .......... .......... .......... .......... .......... 82% 6.19M 6s 215250K .......... .......... .......... .......... .......... 82% 6.81M 6s 215300K .......... .......... .......... .......... .......... 82% 5.67M 6s 215350K .......... .......... .......... .......... .......... 82% 6.40M 6s 215400K .......... .......... .......... .......... .......... 82% 13.9M 6s 215450K .......... .......... .......... .......... .......... 82% 25.8M 6s 215500K .......... .......... .......... .......... .......... 82% 16.5M 6s 215550K .......... .......... .......... .......... .......... 82% 18.6M 6s 215600K .......... .......... .......... .......... .......... 82% 13.0M 6s 215650K .......... .......... .......... .......... .......... 82% 11.9M 6s 215700K .......... .......... .......... .......... .......... 82% 10.6M 6s 215750K .......... .......... .......... .......... .......... 82% 12.5M 6s 215800K .......... .......... .......... .......... .......... 82% 11.5M 6s 215850K .......... .......... .......... .......... .......... 82% 7.27M 6s 215900K .......... .......... .......... .......... .......... 82% 9.65M 6s 215950K .......... .......... .......... .......... .......... 82% 6.58M 6s 216000K .......... .......... .......... .......... .......... 82% 7.75M 6s 216050K .......... .......... .......... .......... .......... 82% 7.14M 6s 216100K .......... .......... .......... .......... .......... 82% 6.08M 6s 216150K .......... .......... .......... .......... .......... 82% 5.91M 6s 216200K .......... .......... .......... .......... .......... 82% 4.81M 6s 216250K .......... .......... .......... .......... .......... 82% 3.24M 6s 216300K .......... .......... .......... .......... .......... 82% 1.63M 6s 216350K .......... .......... .......... .......... .......... 82% 2.88M 6s 216400K .......... .......... .......... .......... .......... 82% 17.2M 6s 216450K .......... .......... .......... .......... .......... 82% 25.8M 6s 216500K .......... .......... .......... .......... .......... 82% 30.9M 6s 216550K .......... .......... .......... .......... .......... 82% 13.2M 6s 216600K .......... .......... .......... .......... .......... 82% 8.91M 6s 216650K .......... .......... .......... .......... .......... 82% 28.9M 6s 216700K .......... .......... .......... .......... .......... 82% 9.20M 6s 216750K .......... .......... .......... .......... .......... 82% 10.6M 6s 216800K .......... .......... .......... .......... .......... 82% 10.3M 6s 216850K .......... .......... .......... .......... .......... 82% 8.07M 6s 216900K .......... .......... .......... .......... .......... 82% 11.6M 6s 216950K .......... .......... .......... .......... .......... 82% 9.21M 6s 217000K .......... .......... .......... .......... .......... 82% 11.8M 6s 217050K .......... .......... .......... .......... .......... 82% 9.38M 6s 217100K .......... .......... .......... .......... .......... 82% 12.3M 6s 217150K .......... .......... .......... .......... .......... 82% 7.43M 6s 217200K .......... .......... .......... .......... .......... 82% 9.98M 6s 217250K .......... .......... .......... .......... .......... 82% 11.1M 6s 217300K .......... .......... .......... .......... .......... 82% 7.37M 6s 217350K .......... .......... .......... .......... .......... 82% 9.58M 6s 217400K .......... .......... .......... .......... .......... 82% 9.72M 6s 217450K .......... .......... .......... .......... .......... 82% 8.37M 6s 217500K .......... .......... .......... .......... .......... 82% 8.38M 6s 217550K .......... .......... .......... .......... .......... 82% 4.61M 6s 217600K .......... .......... .......... .......... .......... 83% 6.47M 6s 217650K .......... .......... .......... .......... .......... 83% 5.51M 6s 217700K .......... .......... .......... .......... .......... 83% 4.39M 6s 217750K .......... .......... .......... .......... .......... 83% 5.56M 6s 217800K .......... .......... .......... .......... .......... 83% 4.45M 6s 217850K .......... .......... .......... .......... .......... 83% 4.48M 6s 217900K .......... .......... .......... .......... .......... 83% 5.44M 6s 217950K .......... .......... .......... .......... .......... 83% 4.21M 6s 218000K .......... .......... .......... .......... .......... 83% 4.81M 6s 218050K .......... .......... .......... .......... .......... 83% 5.81M 6s 218100K .......... .......... .......... .......... .......... 83% 13.4M 6s 218150K .......... .......... .......... .......... .......... 83% 13.2M 6s 218200K .......... .......... .......... .......... .......... 83% 10.5M 6s 218250K .......... .......... .......... .......... .......... 83% 10.4M 6s 218300K .......... .......... .......... .......... .......... 83% 8.47M 6s 218350K .......... .......... .......... .......... .......... 83% 9.74M 6s 218400K .......... .......... .......... .......... .......... 83% 9.29M 6s 218450K .......... .......... .......... .......... .......... 83% 6.96M 6s 218500K .......... .......... .......... .......... .......... 83% 4.67M 6s 218550K .......... .......... .......... .......... .......... 83% 6.85M 6s 218600K .......... .......... .......... .......... .......... 83% 5.20M 6s 218650K .......... .......... .......... .......... .......... 83% 4.36M 6s 218700K .......... .......... .......... .......... .......... 83% 2.81M 6s 218750K .......... .......... .......... .......... .......... 83% 5.28M 6s 218800K .......... .......... .......... .......... .......... 83% 882K 6s 218850K .......... .......... .......... .......... .......... 83% 3.09M 6s 218900K .......... .......... .......... .......... .......... 83% 3.51M 6s 218950K .......... .......... .......... .......... .......... 83% 2.83M 6s 219000K .......... .......... .......... .......... .......... 83% 3.58M 6s 219050K .......... .......... .......... .......... .......... 83% 7.80M 6s 219100K .......... .......... .......... .......... .......... 83% 3.71M 6s 219150K .......... .......... .......... .......... .......... 83% 5.27M 5s 219200K .......... .......... .......... .......... .......... 83% 3.51M 5s 219250K .......... .......... .......... .......... .......... 83% 2.86M 5s 219300K .......... .......... .......... .......... .......... 83% 5.20M 5s 219350K .......... .......... .......... .......... .......... 83% 4.42M 5s 219400K .......... .......... .......... .......... .......... 83% 4.94M 5s 219450K .......... .......... .......... .......... .......... 83% 1.97M 5s 219500K .......... .......... .......... .......... .......... 83% 3.01M 5s 219550K .......... .......... .......... .......... .......... 83% 8.66M 5s 219600K .......... .......... .......... .......... .......... 83% 10.2M 5s 219650K .......... .......... .......... .......... .......... 83% 11.3M 5s 219700K .......... .......... .......... .......... .......... 83% 8.68M 5s 219750K .......... .......... .......... .......... .......... 83% 9.98M 5s 219800K .......... .......... .......... .......... .......... 83% 9.93M 5s 219850K .......... .......... .......... .......... .......... 83% 8.63M 5s 219900K .......... .......... .......... .......... .......... 83% 5.73M 5s 219950K .......... .......... .......... .......... .......... 83% 11.8M 5s 220000K .......... .......... .......... .......... .......... 83% 6.72M 5s 220050K .......... .......... .......... .......... .......... 83% 8.37M 5s 220100K .......... .......... .......... .......... .......... 83% 7.71M 5s 220150K .......... .......... .......... .......... .......... 83% 6.46M 5s 220200K .......... .......... .......... .......... .......... 84% 4.47M 5s 220250K .......... .......... .......... .......... .......... 84% 6.74M 5s 220300K .......... .......... .......... .......... .......... 84% 7.56M 5s 220350K .......... .......... .......... .......... .......... 84% 16.5M 5s 220400K .......... .......... .......... .......... .......... 84% 8.46M 5s 220450K .......... .......... .......... .......... .......... 84% 6.70M 5s 220500K .......... .......... .......... .......... .......... 84% 9.63M 5s 220550K .......... .......... .......... .......... .......... 84% 8.27M 5s 220600K .......... .......... .......... .......... .......... 84% 8.46M 5s 220650K .......... .......... .......... .......... .......... 84% 6.49M 5s 220700K .......... .......... .......... .......... .......... 84% 7.65M 5s 220750K .......... .......... .......... .......... .......... 84% 8.00M 5s 220800K .......... .......... .......... .......... .......... 84% 10.5M 5s 220850K .......... .......... .......... .......... .......... 84% 4.56M 5s 220900K .......... .......... .......... .......... .......... 84% 12.1M 5s 220950K .......... .......... .......... .......... .......... 84% 5.53M 5s 221000K .......... .......... .......... .......... .......... 84% 6.46M 5s 221050K .......... .......... .......... .......... .......... 84% 7.22M 5s 221100K .......... .......... .......... .......... .......... 84% 12.6M 5s 221150K .......... .......... .......... .......... .......... 84% 14.0M 5s 221200K .......... .......... .......... .......... .......... 84% 10.2M 5s 221250K .......... .......... .......... .......... .......... 84% 8.21M 5s 221300K .......... .......... .......... .......... .......... 84% 6.69M 5s 221350K .......... .......... .......... .......... .......... 84% 6.25M 5s 221400K .......... .......... .......... .......... .......... 84% 7.30M 5s 221450K .......... .......... .......... .......... .......... 84% 5.41M 5s 221500K .......... .......... .......... .......... .......... 84% 4.17M 5s 221550K .......... .......... .......... .......... .......... 84% 6.49M 5s 221600K .......... .......... .......... .......... .......... 84% 4.08M 5s 221650K .......... .......... .......... .......... .......... 84% 3.93M 5s 221700K .......... .......... .......... .......... .......... 84% 6.45M 5s 221750K .......... .......... .......... .......... .......... 84% 11.7M 5s 221800K .......... .......... .......... .......... .......... 84% 9.22M 5s 221850K .......... .......... .......... .......... .......... 84% 6.95M 5s 221900K .......... .......... .......... .......... .......... 84% 7.80M 5s 221950K .......... .......... .......... .......... .......... 84% 6.79M 5s 222000K .......... .......... .......... .......... .......... 84% 6.88M 5s 222050K .......... .......... .......... .......... .......... 84% 5.82M 5s 222100K .......... .......... .......... .......... .......... 84% 4.56M 5s 222150K .......... .......... .......... .......... .......... 84% 4.30M 5s 222200K .......... .......... .......... .......... .......... 84% 2.99M 5s 222250K .......... .......... .......... .......... .......... 84% 2.69M 5s 222300K .......... .......... .......... .......... .......... 84% 3.37M 5s 222350K .......... .......... .......... .......... .......... 84% 4.09M 5s 222400K .......... .......... .......... .......... .......... 84% 3.83M 5s 222450K .......... .......... .......... .......... .......... 84% 5.06M 5s 222500K .......... .......... .......... .......... .......... 84% 8.36M 5s 222550K .......... .......... .......... .......... .......... 84% 7.55M 5s 222600K .......... .......... .......... .......... .......... 84% 4.92M 5s 222650K .......... .......... .......... .......... .......... 84% 7.14M 5s 222700K .......... .......... .......... .......... .......... 84% 13.4M 5s 222750K .......... .......... .......... .......... .......... 84% 16.5M 5s 222800K .......... .......... .......... .......... .......... 84% 13.6M 5s 222850K .......... .......... .......... .......... .......... 85% 12.6M 5s 222900K .......... .......... .......... .......... .......... 85% 23.9M 5s 222950K .......... .......... .......... .......... .......... 85% 13.5M 5s 223000K .......... .......... .......... .......... .......... 85% 15.1M 5s 223050K .......... .......... .......... .......... .......... 85% 17.1M 5s 223100K .......... .......... .......... .......... .......... 85% 10.3M 5s 223150K .......... .......... .......... .......... .......... 85% 15.4M 5s 223200K .......... .......... .......... .......... .......... 85% 14.6M 5s 223250K .......... .......... .......... .......... .......... 85% 14.8M 5s 223300K .......... .......... .......... .......... .......... 85% 14.9M 5s 223350K .......... .......... .......... .......... .......... 85% 8.77M 5s 223400K .......... .......... .......... .......... .......... 85% 12.3M 5s 223450K .......... .......... .......... .......... .......... 85% 12.4M 5s 223500K .......... .......... .......... .......... .......... 85% 12.5M 5s 223550K .......... .......... .......... .......... .......... 85% 19.7M 5s 223600K .......... .......... .......... .......... .......... 85% 23.7M 5s 223650K .......... .......... .......... .......... .......... 85% 21.5M 5s 223700K .......... .......... .......... .......... .......... 85% 21.8M 5s 223750K .......... .......... .......... .......... .......... 85% 21.2M 5s 223800K .......... .......... .......... .......... .......... 85% 25.1M 5s 223850K .......... .......... .......... .......... .......... 85% 21.5M 5s 223900K .......... .......... .......... .......... .......... 85% 23.8M 5s 223950K .......... .......... .......... .......... .......... 85% 20.6M 5s 224000K .......... .......... .......... .......... .......... 85% 22.7M 5s 224050K .......... .......... .......... .......... .......... 85% 23.0M 5s 224100K .......... .......... .......... .......... .......... 85% 11.3M 5s 224150K .......... .......... .......... .......... .......... 85% 31.2M 5s 224200K .......... .......... .......... .......... .......... 85% 14.0M 5s 224250K .......... .......... .......... .......... .......... 85% 11.8M 5s 224300K .......... .......... .......... .......... .......... 85% 17.3M 5s 224350K .......... .......... .......... .......... .......... 85% 11.5M 5s 224400K .......... .......... .......... .......... .......... 85% 10.7M 5s 224450K .......... .......... .......... .......... .......... 85% 8.05M 5s 224500K .......... .......... .......... .......... .......... 85% 5.49M 5s 224550K .......... .......... .......... .......... .......... 85% 6.01M 5s 224600K .......... .......... .......... .......... .......... 85% 5.77M 5s 224650K .......... .......... .......... .......... .......... 85% 6.47M 5s 224700K .......... .......... .......... .......... .......... 85% 7.33M 5s 224750K .......... .......... .......... .......... .......... 85% 13.9M 5s 224800K .......... .......... .......... .......... .......... 85% 15.4M 5s 224850K .......... .......... .......... .......... .......... 85% 13.5M 5s 224900K .......... .......... .......... .......... .......... 85% 7.76M 5s 224950K .......... .......... .......... .......... .......... 85% 11.3M 5s 225000K .......... .......... .......... .......... .......... 85% 145M 5s 225050K .......... .......... .......... .......... .......... 85% 16.8M 5s 225100K .......... .......... .......... .......... .......... 85% 6.68M 5s 225150K .......... .......... .......... .......... .......... 85% 120M 5s 225200K .......... .......... .......... .......... .......... 85% 8.83M 5s 225250K .......... .......... .......... .......... .......... 85% 10.5M 5s 225300K .......... .......... .......... .......... .......... 85% 7.60M 5s 225350K .......... .......... .......... .......... .......... 85% 6.80M 5s 225400K .......... .......... .......... .......... .......... 85% 11.0M 5s 225450K .......... .......... .......... .......... .......... 86% 3.94M 5s 225500K .......... .......... .......... .......... .......... 86% 4.90M 5s 225550K .......... .......... .......... .......... .......... 86% 4.50M 5s 225600K .......... .......... .......... .......... .......... 86% 4.37M 5s 225650K .......... .......... .......... .......... .......... 86% 10.7M 5s 225700K .......... .......... .......... .......... .......... 86% 8.50M 5s 225750K .......... .......... .......... .......... .......... 86% 8.10M 5s 225800K .......... .......... .......... .......... .......... 86% 13.0M 5s 225850K .......... .......... .......... .......... .......... 86% 6.20M 5s 225900K .......... .......... .......... .......... .......... 86% 5.91M 5s 225950K .......... .......... .......... .......... .......... 86% 4.92M 5s 226000K .......... .......... .......... .......... .......... 86% 6.80M 5s 226050K .......... .......... .......... .......... .......... 86% 6.49M 5s 226100K .......... .......... .......... .......... .......... 86% 6.34M 5s 226150K .......... .......... .......... .......... .......... 86% 6.92M 5s 226200K .......... .......... .......... .......... .......... 86% 4.59M 5s 226250K .......... .......... .......... .......... .......... 86% 4.47M 5s 226300K .......... .......... .......... .......... .......... 86% 4.57M 5s 226350K .......... .......... .......... .......... .......... 86% 3.32M 5s 226400K .......... .......... .......... .......... .......... 86% 3.24M 5s 226450K .......... .......... .......... .......... .......... 86% 2.88M 5s 226500K .......... .......... .......... .......... .......... 86% 8.02M 5s 226550K .......... .......... .......... .......... .......... 86% 11.0M 5s 226600K .......... .......... .......... .......... .......... 86% 8.46M 5s 226650K .......... .......... .......... .......... .......... 86% 8.88M 5s 226700K .......... .......... .......... .......... .......... 86% 4.53M 5s 226750K .......... .......... .......... .......... .......... 86% 5.46M 5s 226800K .......... .......... .......... .......... .......... 86% 6.45M 5s 226850K .......... .......... .......... .......... .......... 86% 5.87M 5s 226900K .......... .......... .......... .......... .......... 86% 6.47M 5s 226950K .......... .......... .......... .......... .......... 86% 5.26M 5s 227000K .......... .......... .......... .......... .......... 86% 5.70M 5s 227050K .......... .......... .......... .......... .......... 86% 3.17M 5s 227100K .......... .......... .......... .......... .......... 86% 8.45M 4s 227150K .......... .......... .......... .......... .......... 86% 19.8M 4s 227200K .......... .......... .......... .......... .......... 86% 20.6M 4s 227250K .......... .......... .......... .......... .......... 86% 12.5M 4s 227300K .......... .......... .......... .......... .......... 86% 20.6M 4s 227350K .......... .......... .......... .......... .......... 86% 36.7M 4s 227400K .......... .......... .......... .......... .......... 86% 18.4M 4s 227450K .......... .......... .......... .......... .......... 86% 16.3M 4s 227500K .......... .......... .......... .......... .......... 86% 14.4M 4s 227550K .......... .......... .......... .......... .......... 86% 22.4M 4s 227600K .......... .......... .......... .......... .......... 86% 14.7M 4s 227650K .......... .......... .......... .......... .......... 86% 23.3M 4s 227700K .......... .......... .......... .......... .......... 86% 13.3M 4s 227750K .......... .......... .......... .......... .......... 86% 16.4M 4s 227800K .......... .......... .......... .......... .......... 86% 15.3M 4s 227850K .......... .......... .......... .......... .......... 86% 9.70M 4s 227900K .......... .......... .......... .......... .......... 86% 7.90M 4s 227950K .......... .......... .......... .......... .......... 86% 14.1M 4s 228000K .......... .......... .......... .......... .......... 86% 10.8M 4s 228050K .......... .......... .......... .......... .......... 86% 8.77M 4s 228100K .......... .......... .......... .......... .......... 87% 9.54M 4s 228150K .......... .......... .......... .......... .......... 87% 16.5M 4s 228200K .......... .......... .......... .......... .......... 87% 10.3M 4s 228250K .......... .......... .......... .......... .......... 87% 10.3M 4s 228300K .......... .......... .......... .......... .......... 87% 11.2M 4s 228350K .......... .......... .......... .......... .......... 87% 9.94M 4s 228400K .......... .......... .......... .......... .......... 87% 8.70M 4s 228450K .......... .......... .......... .......... .......... 87% 6.57M 4s 228500K .......... .......... .......... .......... .......... 87% 5.57M 4s 228550K .......... .......... .......... .......... .......... 87% 3.72M 4s 228600K .......... .......... .......... .......... .......... 87% 4.80M 4s 228650K .......... .......... .......... .......... .......... 87% 5.35M 4s 228700K .......... .......... .......... .......... .......... 87% 4.96M 4s 228750K .......... .......... .......... .......... .......... 87% 5.95M 4s 228800K .......... .......... .......... .......... .......... 87% 6.29M 4s 228850K .......... .......... .......... .......... .......... 87% 3.63M 4s 228900K .......... .......... .......... .......... .......... 87% 3.82M 4s 228950K .......... .......... .......... .......... .......... 87% 5.15M 4s 229000K .......... .......... .......... .......... .......... 87% 6.10M 4s 229050K .......... .......... .......... .......... .......... 87% 3.55M 4s 229100K .......... .......... .......... .......... .......... 87% 3.49M 4s 229150K .......... .......... .......... .......... .......... 87% 4.82M 4s 229200K .......... .......... .......... .......... .......... 87% 9.07M 4s 229250K .......... .......... .......... .......... .......... 87% 36.3M 4s 229300K .......... .......... .......... .......... .......... 87% 17.2M 4s 229350K .......... .......... .......... .......... .......... 87% 16.9M 4s 229400K .......... .......... .......... .......... .......... 87% 20.9M 4s 229450K .......... .......... .......... .......... .......... 87% 17.4M 4s 229500K .......... .......... .......... .......... .......... 87% 12.4M 4s 229550K .......... .......... .......... .......... .......... 87% 15.0M 4s 229600K .......... .......... .......... .......... .......... 87% 10.3M 4s 229650K .......... .......... .......... .......... .......... 87% 6.61M 4s 229700K .......... .......... .......... .......... .......... 87% 5.48M 4s 229750K .......... .......... .......... .......... .......... 87% 6.67M 4s 229800K .......... .......... .......... .......... .......... 87% 6.48M 4s 229850K .......... .......... .......... .......... .......... 87% 12.1M 4s 229900K .......... .......... .......... .......... .......... 87% 12.6M 4s 229950K .......... .......... .......... .......... .......... 87% 11.4M 4s 230000K .......... .......... .......... .......... .......... 87% 14.6M 4s 230050K .......... .......... .......... .......... .......... 87% 13.9M 4s 230100K .......... .......... .......... .......... .......... 87% 10.1M 4s 230150K .......... .......... .......... .......... .......... 87% 12.3M 4s 230200K .......... .......... .......... .......... .......... 87% 7.75M 4s 230250K .......... .......... .......... .......... .......... 87% 9.65M 4s 230300K .......... .......... .......... .......... .......... 87% 10.1M 4s 230350K .......... .......... .......... .......... .......... 87% 5.26M 4s 230400K .......... .......... .......... .......... .......... 87% 6.34M 4s 230450K .......... .......... .......... .......... .......... 87% 10.3M 4s 230500K .......... .......... .......... .......... .......... 87% 13.0M 4s 230550K .......... .......... .......... .......... .......... 87% 12.5M 4s 230600K .......... .......... .......... .......... .......... 87% 11.6M 4s 230650K .......... .......... .......... .......... .......... 87% 9.29M 4s 230700K .......... .......... .......... .......... .......... 88% 5.89M 4s 230750K .......... .......... .......... .......... .......... 88% 9.08M 4s 230800K .......... .......... .......... .......... .......... 88% 8.93M 4s 230850K .......... .......... .......... .......... .......... 88% 8.01M 4s 230900K .......... .......... .......... .......... .......... 88% 5.27M 4s 230950K .......... .......... .......... .......... .......... 88% 5.08M 4s 231000K .......... .......... .......... .......... .......... 88% 4.05M 4s 231050K .......... .......... .......... .......... .......... 88% 3.35M 4s 231100K .......... .......... .......... .......... .......... 88% 3.44M 4s 231150K .......... .......... .......... .......... .......... 88% 4.46M 4s 231200K .......... .......... .......... .......... .......... 88% 5.22M 4s 231250K .......... .......... .......... .......... .......... 88% 9.62M 4s 231300K .......... .......... .......... .......... .......... 88% 9.89M 4s 231350K .......... .......... .......... .......... .......... 88% 4.76M 4s 231400K .......... .......... .......... .......... .......... 88% 8.92M 4s 231450K .......... .......... .......... .......... .......... 88% 5.58M 4s 231500K .......... .......... .......... .......... .......... 88% 5.86M 4s 231550K .......... .......... .......... .......... .......... 88% 8.02M 4s 231600K .......... .......... .......... .......... .......... 88% 7.74M 4s 231650K .......... .......... .......... .......... .......... 88% 7.09M 4s 231700K .......... .......... .......... .......... .......... 88% 6.71M 4s 231750K .......... .......... .......... .......... .......... 88% 9.55M 4s 231800K .......... .......... .......... .......... .......... 88% 10.2M 4s 231850K .......... .......... .......... .......... .......... 88% 14.4M 4s 231900K .......... .......... .......... .......... .......... 88% 8.60M 4s 231950K .......... .......... .......... .......... .......... 88% 13.8M 4s 232000K .......... .......... .......... .......... .......... 88% 9.41M 4s 232050K .......... .......... .......... .......... .......... 88% 8.46M 4s 232100K .......... .......... .......... .......... .......... 88% 8.91M 4s 232150K .......... .......... .......... .......... .......... 88% 9.41M 4s 232200K .......... .......... .......... .......... .......... 88% 8.88M 4s 232250K .......... .......... .......... .......... .......... 88% 10.2M 4s 232300K .......... .......... .......... .......... .......... 88% 25.6M 4s 232350K .......... .......... .......... .......... .......... 88% 18.6M 4s 232400K .......... .......... .......... .......... .......... 88% 20.6M 4s 232450K .......... .......... .......... .......... .......... 88% 20.6M 4s 232500K .......... .......... .......... .......... .......... 88% 26.4M 4s 232550K .......... .......... .......... .......... .......... 88% 21.6M 4s 232600K .......... .......... .......... .......... .......... 88% 18.2M 4s 232650K .......... .......... .......... .......... .......... 88% 37.0M 4s 232700K .......... .......... .......... .......... .......... 88% 21.7M 4s 232750K .......... .......... .......... .......... .......... 88% 28.3M 4s 232800K .......... .......... .......... .......... .......... 88% 15.4M 4s 232850K .......... .......... .......... .......... .......... 88% 19.2M 4s 232900K .......... .......... .......... .......... .......... 88% 23.7M 4s 232950K .......... .......... .......... .......... .......... 88% 20.1M 4s 233000K .......... .......... .......... .......... .......... 88% 20.9M 4s 233050K .......... .......... .......... .......... .......... 88% 22.7M 4s 233100K .......... .......... .......... .......... .......... 88% 23.6M 4s 233150K .......... .......... .......... .......... .......... 88% 16.5M 4s 233200K .......... .......... .......... .......... .......... 88% 18.3M 4s 233250K .......... .......... .......... .......... .......... 88% 10.3M 4s 233300K .......... .......... .......... .......... .......... 89% 21.5M 4s 233350K .......... .......... .......... .......... .......... 89% 11.8M 4s 233400K .......... .......... .......... .......... .......... 89% 11.1M 4s 233450K .......... .......... .......... .......... .......... 89% 11.0M 4s 233500K .......... .......... .......... .......... .......... 89% 5.80M 4s 233550K .......... .......... .......... .......... .......... 89% 21.9M 4s 233600K .......... .......... .......... .......... .......... 89% 6.84M 4s 233650K .......... .......... .......... .......... .......... 89% 7.30M 4s 233700K .......... .......... .......... .......... .......... 89% 5.25M 4s 233750K .......... .......... .......... .......... .......... 89% 8.18M 4s 233800K .......... .......... .......... .......... .......... 89% 7.25M 4s 233850K .......... .......... .......... .......... .......... 89% 4.85M 4s 233900K .......... .......... .......... .......... .......... 89% 6.78M 4s 233950K .......... .......... .......... .......... .......... 89% 4.33M 4s 234000K .......... .......... .......... .......... .......... 89% 4.02M 4s 234050K .......... .......... .......... .......... .......... 89% 5.28M 4s 234100K .......... .......... .......... .......... .......... 89% 4.73M 4s 234150K .......... .......... .......... .......... .......... 89% 6.47M 4s 234200K .......... .......... .......... .......... .......... 89% 6.16M 4s 234250K .......... .......... .......... .......... .......... 89% 11.9M 4s 234300K .......... .......... .......... .......... .......... 89% 16.3M 4s 234350K .......... .......... .......... .......... .......... 89% 10.2M 4s 234400K .......... .......... .......... .......... .......... 89% 16.8M 4s 234450K .......... .......... .......... .......... .......... 89% 13.8M 4s 234500K .......... .......... .......... .......... .......... 89% 16.2M 4s 234550K .......... .......... .......... .......... .......... 89% 19.2M 4s 234600K .......... .......... .......... .......... .......... 89% 9.64M 4s 234650K .......... .......... .......... .......... .......... 89% 9.35M 4s 234700K .......... .......... .......... .......... .......... 89% 9.30M 4s 234750K .......... .......... .......... .......... .......... 89% 9.10M 3s 234800K .......... .......... .......... .......... .......... 89% 10.7M 3s 234850K .......... .......... .......... .......... .......... 89% 6.57M 3s 234900K .......... .......... .......... .......... .......... 89% 5.91M 3s 234950K .......... .......... .......... .......... .......... 89% 4.00M 3s 235000K .......... .......... .......... .......... .......... 89% 5.49M 3s 235050K .......... .......... .......... .......... .......... 89% 5.78M 3s 235100K .......... .......... .......... .......... .......... 89% 4.26M 3s 235150K .......... .......... .......... .......... .......... 89% 4.43M 3s 235200K .......... .......... .......... .......... .......... 89% 4.39M 3s 235250K .......... .......... .......... .......... .......... 89% 4.41M 3s 235300K .......... .......... .......... .......... .......... 89% 14.6M 3s 235350K .......... .......... .......... .......... .......... 89% 21.0M 3s 235400K .......... .......... .......... .......... .......... 89% 9.40M 3s 235450K .......... .......... .......... .......... .......... 89% 50.7M 3s 235500K .......... .......... .......... .......... .......... 89% 12.0M 3s 235550K .......... .......... .......... .......... .......... 89% 13.7M 3s 235600K .......... .......... .......... .......... .......... 89% 10.3M 3s 235650K .......... .......... .......... .......... .......... 89% 11.6M 3s 235700K .......... .......... .......... .......... .......... 89% 12.5M 3s 235750K .......... .......... .......... .......... .......... 89% 16.5M 3s 235800K .......... .......... .......... .......... .......... 89% 15.6M 3s 235850K .......... .......... .......... .......... .......... 89% 15.6M 3s 235900K .......... .......... .......... .......... .......... 89% 13.7M 3s 235950K .......... .......... .......... .......... .......... 90% 14.1M 3s 236000K .......... .......... .......... .......... .......... 90% 9.42M 3s 236050K .......... .......... .......... .......... .......... 90% 11.4M 3s 236100K .......... .......... .......... .......... .......... 90% 6.26M 3s 236150K .......... .......... .......... .......... .......... 90% 7.55M 3s 236200K .......... .......... .......... .......... .......... 90% 2.97M 3s 236250K .......... .......... .......... .......... .......... 90% 3.39M 3s 236300K .......... .......... .......... .......... .......... 90% 4.22M 3s 236350K .......... .......... .......... .......... .......... 90% 25.5M 3s 236400K .......... .......... .......... .......... .......... 90% 18.6M 3s 236450K .......... .......... .......... .......... .......... 90% 13.7M 3s 236500K .......... .......... .......... .......... .......... 90% 13.1M 3s 236550K .......... .......... .......... .......... .......... 90% 13.0M 3s 236600K .......... .......... .......... .......... .......... 90% 9.48M 3s 236650K .......... .......... .......... .......... .......... 90% 15.5M 3s 236700K .......... .......... .......... .......... .......... 90% 11.9M 3s 236750K .......... .......... .......... .......... .......... 90% 9.28M 3s 236800K .......... .......... .......... .......... .......... 90% 15.9M 3s 236850K .......... .......... .......... .......... .......... 90% 12.1M 3s 236900K .......... .......... .......... .......... .......... 90% 10.8M 3s 236950K .......... .......... .......... .......... .......... 90% 8.63M 3s 237000K .......... .......... .......... .......... .......... 90% 8.70M 3s 237050K .......... .......... .......... .......... .......... 90% 11.8M 3s 237100K .......... .......... .......... .......... .......... 90% 7.90M 3s 237150K .......... .......... .......... .......... .......... 90% 11.5M 3s 237200K .......... .......... .......... .......... .......... 90% 5.47M 3s 237250K .......... .......... .......... .......... .......... 90% 6.37M 3s 237300K .......... .......... .......... .......... .......... 90% 7.43M 3s 237350K .......... .......... .......... .......... .......... 90% 8.22M 3s 237400K .......... .......... .......... .......... .......... 90% 13.9M 3s 237450K .......... .......... .......... .......... .......... 90% 7.76M 3s 237500K .......... .......... .......... .......... .......... 90% 15.3M 3s 237550K .......... .......... .......... .......... .......... 90% 13.1M 3s 237600K .......... .......... .......... .......... .......... 90% 9.59M 3s 237650K .......... .......... .......... .......... .......... 90% 16.8M 3s 237700K .......... .......... .......... .......... .......... 90% 12.8M 3s 237750K .......... .......... .......... .......... .......... 90% 10.3M 3s 237800K .......... .......... .......... .......... .......... 90% 11.8M 3s 237850K .......... .......... .......... .......... .......... 90% 9.08M 3s 237900K .......... .......... .......... .......... .......... 90% 10.3M 3s 237950K .......... .......... .......... .......... .......... 90% 7.86M 3s 238000K .......... .......... .......... .......... .......... 90% 11.5M 3s 238050K .......... .......... .......... .......... .......... 90% 11.8M 3s 238100K .......... .......... .......... .......... .......... 90% 8.64M 3s 238150K .......... .......... .......... .......... .......... 90% 8.77M 3s 238200K .......... .......... .......... .......... .......... 90% 7.12M 3s 238250K .......... .......... .......... .......... .......... 90% 10.0M 3s 238300K .......... .......... .......... .......... .......... 90% 7.57M 3s 238350K .......... .......... .......... .......... .......... 90% 6.52M 3s 238400K .......... .......... .......... .......... .......... 90% 7.07M 3s 238450K .......... .......... .......... .......... .......... 90% 4.84M 3s 238500K .......... .......... .......... .......... .......... 90% 2.70M 3s 238550K .......... .......... .......... .......... .......... 91% 3.55M 3s 238600K .......... .......... .......... .......... .......... 91% 9.79M 3s 238650K .......... .......... .......... .......... .......... 91% 24.7M 3s 238700K .......... .......... .......... .......... .......... 91% 14.4M 3s 238750K .......... .......... .......... .......... .......... 91% 17.7M 3s 238800K .......... .......... .......... .......... .......... 91% 14.6M 3s 238850K .......... .......... .......... .......... .......... 91% 13.5M 3s 238900K .......... .......... .......... .......... .......... 91% 10.5M 3s 238950K .......... .......... .......... .......... .......... 91% 8.13M 3s 239000K .......... .......... .......... .......... .......... 91% 13.0M 3s 239050K .......... .......... .......... .......... .......... 91% 14.0M 3s 239100K .......... .......... .......... .......... .......... 91% 13.7M 3s 239150K .......... .......... .......... .......... .......... 91% 16.4M 3s 239200K .......... .......... .......... .......... .......... 91% 11.8M 3s 239250K .......... .......... .......... .......... .......... 91% 19.9M 3s 239300K .......... .......... .......... .......... .......... 91% 16.7M 3s 239350K .......... .......... .......... .......... .......... 91% 9.19M 3s 239400K .......... .......... .......... .......... .......... 91% 10.8M 3s 239450K .......... .......... .......... .......... .......... 91% 9.70M 3s 239500K .......... .......... .......... .......... .......... 91% 8.16M 3s 239550K .......... .......... .......... .......... .......... 91% 14.0M 3s 239600K .......... .......... .......... .......... .......... 91% 9.32M 3s 239650K .......... .......... .......... .......... .......... 91% 8.87M 3s 239700K .......... .......... .......... .......... .......... 91% 5.60M 3s 239750K .......... .......... .......... .......... .......... 91% 5.73M 3s 239800K .......... .......... .......... .......... .......... 91% 6.95M 3s 239850K .......... .......... .......... .......... .......... 91% 5.72M 3s 239900K .......... .......... .......... .......... .......... 91% 5.08M 3s 239950K .......... .......... .......... .......... .......... 91% 4.63M 3s 240000K .......... .......... .......... .......... .......... 91% 7.85M 3s 240050K .......... .......... .......... .......... .......... 91% 21.7M 3s 240100K .......... .......... .......... .......... .......... 91% 10.5M 3s 240150K .......... .......... .......... .......... .......... 91% 11.9M 3s 240200K .......... .......... .......... .......... .......... 91% 11.4M 3s 240250K .......... .......... .......... .......... .......... 91% 10.8M 3s 240300K .......... .......... .......... .......... .......... 91% 11.0M 3s 240350K .......... .......... .......... .......... .......... 91% 10.7M 3s 240400K .......... .......... .......... .......... .......... 91% 12.0M 3s 240450K .......... .......... .......... .......... .......... 91% 11.6M 3s 240500K .......... .......... .......... .......... .......... 91% 13.3M 3s 240550K .......... .......... .......... .......... .......... 91% 12.4M 3s 240600K .......... .......... .......... .......... .......... 91% 12.6M 3s 240650K .......... .......... .......... .......... .......... 91% 13.7M 3s 240700K .......... .......... .......... .......... .......... 91% 15.0M 3s 240750K .......... .......... .......... .......... .......... 91% 23.1M 3s 240800K .......... .......... .......... .......... .......... 91% 16.8M 3s 240850K .......... .......... .......... .......... .......... 91% 15.2M 3s 240900K .......... .......... .......... .......... .......... 91% 17.1M 3s 240950K .......... .......... .......... .......... .......... 91% 26.1M 3s 241000K .......... .......... .......... .......... .......... 91% 16.3M 3s 241050K .......... .......... .......... .......... .......... 91% 17.5M 3s 241100K .......... .......... .......... .......... .......... 91% 30.2M 3s 241150K .......... .......... .......... .......... .......... 91% 17.1M 3s 241200K .......... .......... .......... .......... .......... 92% 15.0M 3s 241250K .......... .......... .......... .......... .......... 92% 11.2M 3s 241300K .......... .......... .......... .......... .......... 92% 14.6M 3s 241350K .......... .......... .......... .......... .......... 92% 13.5M 3s 241400K .......... .......... .......... .......... .......... 92% 9.36M 3s 241450K .......... .......... .......... .......... .......... 92% 13.3M 3s 241500K .......... .......... .......... .......... .......... 92% 10.4M 3s 241550K .......... .......... .......... .......... .......... 92% 10.5M 3s 241600K .......... .......... .......... .......... .......... 92% 8.13M 3s 241650K .......... .......... .......... .......... .......... 92% 10.5M 3s 241700K .......... .......... .......... .......... .......... 92% 8.82M 3s 241750K .......... .......... .......... .......... .......... 92% 8.79M 3s 241800K .......... .......... .......... .......... .......... 92% 6.97M 3s 241850K .......... .......... .......... .......... .......... 92% 6.60M 3s 241900K .......... .......... .......... .......... .......... 92% 7.93M 3s 241950K .......... .......... .......... .......... .......... 92% 5.88M 3s 242000K .......... .......... .......... .......... .......... 92% 7.39M 3s 242050K .......... .......... .......... .......... .......... 92% 12.5M 3s 242100K .......... .......... .......... .......... .......... 92% 8.50M 3s 242150K .......... .......... .......... .......... .......... 92% 13.5M 3s 242200K .......... .......... .......... .......... .......... 92% 9.88M 3s 242250K .......... .......... .......... .......... .......... 92% 12.2M 3s 242300K .......... .......... .......... .......... .......... 92% 12.6M 3s 242350K .......... .......... .......... .......... .......... 92% 11.9M 3s 242400K .......... .......... .......... .......... .......... 92% 16.0M 3s 242450K .......... .......... .......... .......... .......... 92% 7.39M 3s 242500K .......... .......... .......... .......... .......... 92% 18.1M 2s 242550K .......... .......... .......... .......... .......... 92% 8.35M 2s 242600K .......... .......... .......... .......... .......... 92% 7.43M 2s 242650K .......... .......... .......... .......... .......... 92% 9.55M 2s 242700K .......... .......... .......... .......... .......... 92% 8.58M 2s 242750K .......... .......... .......... .......... .......... 92% 6.48M 2s 242800K .......... .......... .......... .......... .......... 92% 9.79M 2s 242850K .......... .......... .......... .......... .......... 92% 6.94M 2s 242900K .......... .......... .......... .......... .......... 92% 9.52M 2s 242950K .......... .......... .......... .......... .......... 92% 7.69M 2s 243000K .......... .......... .......... .......... .......... 92% 6.68M 2s 243050K .......... .......... .......... .......... .......... 92% 5.74M 2s 243100K .......... .......... .......... .......... .......... 92% 6.52M 2s 243150K .......... .......... .......... .......... .......... 92% 5.24M 2s 243200K .......... .......... .......... .......... .......... 92% 3.75M 2s 243250K .......... .......... .......... .......... .......... 92% 4.54M 2s 243300K .......... .......... .......... .......... .......... 92% 4.24M 2s 243350K .......... .......... .......... .......... .......... 92% 4.07M 2s 243400K .......... .......... .......... .......... .......... 92% 8.16M 2s 243450K .......... .......... .......... .......... .......... 92% 6.10M 2s 243500K .......... .......... .......... .......... .......... 92% 8.00M 2s 243550K .......... .......... .......... .......... .......... 92% 8.57M 2s 243600K .......... .......... .......... .......... .......... 92% 8.58M 2s 243650K .......... .......... .......... .......... .......... 92% 8.79M 2s 243700K .......... .......... .......... .......... .......... 92% 6.03M 2s 243750K .......... .......... .......... .......... .......... 92% 7.74M 2s 243800K .......... .......... .......... .......... .......... 93% 6.01M 2s 243850K .......... .......... .......... .......... .......... 93% 5.55M 2s 243900K .......... .......... .......... .......... .......... 93% 7.05M 2s 243950K .......... .......... .......... .......... .......... 93% 9.31M 2s 244000K .......... .......... .......... .......... .......... 93% 9.77M 2s 244050K .......... .......... .......... .......... .......... 93% 9.49M 2s 244100K .......... .......... .......... .......... .......... 93% 9.23M 2s 244150K .......... .......... .......... .......... .......... 93% 8.22M 2s 244200K .......... .......... .......... .......... .......... 93% 7.05M 2s 244250K .......... .......... .......... .......... .......... 93% 11.6M 2s 244300K .......... .......... .......... .......... .......... 93% 8.41M 2s 244350K .......... .......... .......... .......... .......... 93% 15.8M 2s 244400K .......... .......... .......... .......... .......... 93% 11.5M 2s 244450K .......... .......... .......... .......... .......... 93% 9.65M 2s 244500K .......... .......... .......... .......... .......... 93% 9.08M 2s 244550K .......... .......... .......... .......... .......... 93% 8.37M 2s 244600K .......... .......... .......... .......... .......... 93% 7.08M 2s 244650K .......... .......... .......... .......... .......... 93% 7.81M 2s 244700K .......... .......... .......... .......... .......... 93% 6.87M 2s 244750K .......... .......... .......... .......... .......... 93% 5.62M 2s 244800K .......... .......... .......... .......... .......... 93% 2.15M 2s 244850K .......... .......... .......... .......... .......... 93% 5.29M 2s 244900K .......... .......... .......... .......... .......... 93% 6.60M 2s 244950K .......... .......... .......... .......... .......... 93% 3.20M 2s 245000K .......... .......... .......... .......... .......... 93% 11.3M 2s 245050K .......... .......... .......... .......... .......... 93% 22.0M 2s 245100K .......... .......... .......... .......... .......... 93% 26.5M 2s 245150K .......... .......... .......... .......... .......... 93% 37.3M 2s 245200K .......... .......... .......... .......... .......... 93% 14.2M 2s 245250K .......... .......... .......... .......... .......... 93% 41.9M 2s 245300K .......... .......... .......... .......... .......... 93% 19.2M 2s 245350K .......... .......... .......... .......... .......... 93% 13.6M 2s 245400K .......... .......... .......... .......... .......... 93% 11.6M 2s 245450K .......... .......... .......... .......... .......... 93% 13.2M 2s 245500K .......... .......... .......... .......... .......... 93% 14.7M 2s 245550K .......... .......... .......... .......... .......... 93% 10.4M 2s 245600K .......... .......... .......... .......... .......... 93% 10.6M 2s 245650K .......... .......... .......... .......... .......... 93% 11.6M 2s 245700K .......... .......... .......... .......... .......... 93% 8.50M 2s 245750K .......... .......... .......... .......... .......... 93% 20.6M 2s 245800K .......... .......... .......... .......... .......... 93% 14.9M 2s 245850K .......... .......... .......... .......... .......... 93% 13.1M 2s 245900K .......... .......... .......... .......... .......... 93% 18.7M 2s 245950K .......... .......... .......... .......... .......... 93% 13.0M 2s 246000K .......... .......... .......... .......... .......... 93% 15.3M 2s 246050K .......... .......... .......... .......... .......... 93% 13.7M 2s 246100K .......... .......... .......... .......... .......... 93% 9.66M 2s 246150K .......... .......... .......... .......... .......... 93% 6.61M 2s 246200K .......... .......... .......... .......... .......... 93% 16.9M 2s 246250K .......... .......... .......... .......... .......... 93% 3.89M 2s 246300K .......... .......... .......... .......... .......... 93% 41.3M 2s 246350K .......... .......... .......... .......... .......... 93% 26.3M 2s 246400K .......... .......... .......... .......... .......... 93% 7.15M 2s 246450K .......... .......... .......... .......... .......... 94% 10.0M 2s 246500K .......... .......... .......... .......... .......... 94% 11.0M 2s 246550K .......... .......... .......... .......... .......... 94% 11.6M 2s 246600K .......... .......... .......... .......... .......... 94% 8.00M 2s 246650K .......... .......... .......... .......... .......... 94% 6.64M 2s 246700K .......... .......... .......... .......... .......... 94% 11.1M 2s 246750K .......... .......... .......... .......... .......... 94% 8.87M 2s 246800K .......... .......... .......... .......... .......... 94% 6.74M 2s 246850K .......... .......... .......... .......... .......... 94% 2.69M 2s 246900K .......... .......... .......... .......... .......... 94% 4.73M 2s 246950K .......... .......... .......... .......... .......... 94% 7.99M 2s 247000K .......... .......... .......... .......... .......... 94% 31.3M 2s 247050K .......... .......... .......... .......... .......... 94% 31.3M 2s 247100K .......... .......... .......... .......... .......... 94% 46.8M 2s 247150K .......... .......... .......... .......... .......... 94% 22.0M 2s 247200K .......... .......... .......... .......... .......... 94% 36.2M 2s 247250K .......... .......... .......... .......... .......... 94% 90.1M 2s 247300K .......... .......... .......... .......... .......... 94% 79.4M 2s 247350K .......... .......... .......... .......... .......... 94% 108M 2s 247400K .......... .......... .......... .......... .......... 94% 52.3M 2s 247450K .......... .......... .......... .......... .......... 94% 33.5M 2s 247500K .......... .......... .......... .......... .......... 94% 38.0M 2s 247550K .......... .......... .......... .......... .......... 94% 24.6M 2s 247600K .......... .......... .......... .......... .......... 94% 26.6M 2s 247650K .......... .......... .......... .......... .......... 94% 38.1M 2s 247700K .......... .......... .......... .......... .......... 94% 52.6M 2s 247750K .......... .......... .......... .......... .......... 94% 66.7M 2s 247800K .......... .......... .......... .......... .......... 94% 26.7M 2s 247850K .......... .......... .......... .......... .......... 94% 21.1M 2s 247900K .......... .......... .......... .......... .......... 94% 19.7M 2s 247950K .......... .......... .......... .......... .......... 94% 29.9M 2s 248000K .......... .......... .......... .......... .......... 94% 6.37M 2s 248050K .......... .......... .......... .......... .......... 94% 74.1M 2s 248100K .......... .......... .......... .......... .......... 94% 17.1M 2s 248150K .......... .......... .......... .......... .......... 94% 5.54M 2s 248200K .......... .......... .......... .......... .......... 94% 22.8M 2s 248250K .......... .......... .......... .......... .......... 94% 9.41M 2s 248300K .......... .......... .......... .......... .......... 94% 11.7M 2s 248350K .......... .......... .......... .......... .......... 94% 6.36M 2s 248400K .......... .......... .......... .......... .......... 94% 5.24M 2s 248450K .......... .......... .......... .......... .......... 94% 4.41M 2s 248500K .......... .......... .......... .......... .......... 94% 3.76M 2s 248550K .......... .......... .......... .......... .......... 94% 4.22M 2s 248600K .......... .......... .......... .......... .......... 94% 7.97M 2s 248650K .......... .......... .......... .......... .......... 94% 9.60M 2s 248700K .......... .......... .......... .......... .......... 94% 9.86M 2s 248750K .......... .......... .......... .......... .......... 94% 9.49M 2s 248800K .......... .......... .......... .......... .......... 94% 10.7M 2s 248850K .......... .......... .......... .......... .......... 94% 6.77M 2s 248900K .......... .......... .......... .......... .......... 94% 8.83M 2s 248950K .......... .......... .......... .......... .......... 94% 7.46M 2s 249000K .......... .......... .......... .......... .......... 94% 8.48M 2s 249050K .......... .......... .......... .......... .......... 95% 9.08M 2s 249100K .......... .......... .......... .......... .......... 95% 7.88M 2s 249150K .......... .......... .......... .......... .......... 95% 4.67M 2s 249200K .......... .......... .......... .......... .......... 95% 6.22M 2s 249250K .......... .......... .......... .......... .......... 95% 8.03M 2s 249300K .......... .......... .......... .......... .......... 95% 6.93M 2s 249350K .......... .......... .......... .......... .......... 95% 7.33M 2s 249400K .......... .......... .......... .......... .......... 95% 9.88M 2s 249450K .......... .......... .......... .......... .......... 95% 20.0M 2s 249500K .......... .......... .......... .......... .......... 95% 18.1M 2s 249550K .......... .......... .......... .......... .......... 95% 22.4M 2s 249600K .......... .......... .......... .......... .......... 95% 19.9M 2s 249650K .......... .......... .......... .......... .......... 95% 24.1M 2s 249700K .......... .......... .......... .......... .......... 95% 23.8M 2s 249750K .......... .......... .......... .......... .......... 95% 20.2M 2s 249800K .......... .......... .......... .......... .......... 95% 25.2M 2s 249850K .......... .......... .......... .......... .......... 95% 23.0M 2s 249900K .......... .......... .......... .......... .......... 95% 18.8M 2s 249950K .......... .......... .......... .......... .......... 95% 28.1M 2s 250000K .......... .......... .......... .......... .......... 95% 13.6M 2s 250050K .......... .......... .......... .......... .......... 95% 12.0M 2s 250100K .......... .......... .......... .......... .......... 95% 10.2M 2s 250150K .......... .......... .......... .......... .......... 95% 10.6M 2s 250200K .......... .......... .......... .......... .......... 95% 10.1M 2s 250250K .......... .......... .......... .......... .......... 95% 10.9M 2s 250300K .......... .......... .......... .......... .......... 95% 10.1M 1s 250350K .......... .......... .......... .......... .......... 95% 8.05M 1s 250400K .......... .......... .......... .......... .......... 95% 11.4M 1s 250450K .......... .......... .......... .......... .......... 95% 23.0M 1s 250500K .......... .......... .......... .......... .......... 95% 21.4M 1s 250550K .......... .......... .......... .......... .......... 95% 19.8M 1s 250600K .......... .......... .......... .......... .......... 95% 13.8M 1s 250650K .......... .......... .......... .......... .......... 95% 134M 1s 250700K .......... .......... .......... .......... .......... 95% 19.1M 1s 250750K .......... .......... .......... .......... .......... 95% 18.6M 1s 250800K .......... .......... .......... .......... .......... 95% 21.4M 1s 250850K .......... .......... .......... .......... .......... 95% 30.2M 1s 250900K .......... .......... .......... .......... .......... 95% 22.1M 1s 250950K .......... .......... .......... .......... .......... 95% 23.2M 1s 251000K .......... .......... .......... .......... .......... 95% 19.2M 1s 251050K .......... .......... .......... .......... .......... 95% 13.9M 1s 251100K .......... .......... .......... .......... .......... 95% 12.9M 1s 251150K .......... .......... .......... .......... .......... 95% 14.4M 1s 251200K .......... .......... .......... .......... .......... 95% 11.0M 1s 251250K .......... .......... .......... .......... .......... 95% 11.1M 1s 251300K .......... .......... .......... .......... .......... 95% 12.1M 1s 251350K .......... .......... .......... .......... .......... 95% 7.05M 1s 251400K .......... .......... .......... .......... .......... 95% 9.13M 1s 251450K .......... .......... .......... .......... .......... 95% 7.35M 1s 251500K .......... .......... .......... .......... .......... 95% 7.21M 1s 251550K .......... .......... .......... .......... .......... 95% 5.56M 1s 251600K .......... .......... .......... .......... .......... 95% 4.10M 1s 251650K .......... .......... .......... .......... .......... 95% 5.77M 1s 251700K .......... .......... .......... .......... .......... 96% 2.83M 1s 251750K .......... .......... .......... .......... .......... 96% 5.79M 1s 251800K .......... .......... .......... .......... .......... 96% 3.91M 1s 251850K .......... .......... .......... .......... .......... 96% 2.59M 1s 251900K .......... .......... .......... .......... .......... 96% 1.61M 1s 251950K .......... .......... .......... .......... .......... 96% 2.28M 1s 252000K .......... .......... .......... .......... .......... 96% 3.02M 1s 252050K .......... .......... .......... .......... .......... 96% 3.54M 1s 252100K .......... .......... .......... .......... .......... 96% 3.82M 1s 252150K .......... .......... .......... .......... .......... 96% 10.4M 1s 252200K .......... .......... .......... .......... .......... 96% 12.4M 1s 252250K .......... .......... .......... .......... .......... 96% 13.2M 1s 252300K .......... .......... .......... .......... .......... 96% 11.9M 1s 252350K .......... .......... .......... .......... .......... 96% 15.1M 1s 252400K .......... .......... .......... .......... .......... 96% 8.08M 1s 252450K .......... .......... .......... .......... .......... 96% 5.22M 1s 252500K .......... .......... .......... .......... .......... 96% 7.60M 1s 252550K .......... .......... .......... .......... .......... 96% 8.48M 1s 252600K .......... .......... .......... .......... .......... 96% 5.95M 1s 252650K .......... .......... .......... .......... .......... 96% 9.41M 1s 252700K .......... .......... .......... .......... .......... 96% 10.6M 1s 252750K .......... .......... .......... .......... .......... 96% 7.65M 1s 252800K .......... .......... .......... .......... .......... 96% 7.57M 1s 252850K .......... .......... .......... .......... .......... 96% 3.85M 1s 252900K .......... .......... .......... .......... .......... 96% 4.00M 1s 252950K .......... .......... .......... .......... .......... 96% 3.39M 1s 253000K .......... .......... .......... .......... .......... 96% 3.57M 1s 253050K .......... .......... .......... .......... .......... 96% 3.02M 1s 253100K .......... .......... .......... .......... .......... 96% 81.3M 1s 253150K .......... .......... .......... .......... .......... 96% 116M 1s 253200K .......... .......... .......... .......... .......... 96% 8.43M 1s 253250K .......... .......... .......... .......... .......... 96% 19.8M 1s 253300K .......... .......... .......... .......... .......... 96% 16.1M 1s 253350K .......... .......... .......... .......... .......... 96% 10.7M 1s 253400K .......... .......... .......... .......... .......... 96% 12.6M 1s 253450K .......... .......... .......... .......... .......... 96% 12.5M 1s 253500K .......... .......... .......... .......... .......... 96% 9.74M 1s 253550K .......... .......... .......... .......... .......... 96% 15.8M 1s 253600K .......... .......... .......... .......... .......... 96% 8.03M 1s 253650K .......... .......... .......... .......... .......... 96% 3.32M 1s 253700K .......... .......... .......... .......... .......... 96% 56.5M 1s 253750K .......... .......... .......... .......... .......... 96% 8.37M 1s 253800K .......... .......... .......... .......... .......... 96% 11.0M 1s 253850K .......... .......... .......... .......... .......... 96% 10.3M 1s 253900K .......... .......... .......... .......... .......... 96% 12.1M 1s 253950K .......... .......... .......... .......... .......... 96% 8.05M 1s 254000K .......... .......... .......... .......... .......... 96% 11.1M 1s 254050K .......... .......... .......... .......... .......... 96% 1.59M 1s 254100K .......... .......... .......... .......... .......... 96% 89.1M 1s 254150K .......... .......... .......... .......... .......... 96% 23.9M 1s 254200K .......... .......... .......... .......... .......... 96% 22.8M 1s 254250K .......... .......... .......... .......... .......... 96% 24.2M 1s 254300K .......... .......... .......... .......... .......... 97% 21.0M 1s 254350K .......... .......... .......... .......... .......... 97% 12.4M 1s 254400K .......... .......... .......... .......... .......... 97% 14.9M 1s 254450K .......... .......... .......... .......... .......... 97% 15.1M 1s 254500K .......... .......... .......... .......... .......... 97% 9.27M 1s 254550K .......... .......... .......... .......... .......... 97% 13.6M 1s 254600K .......... .......... .......... .......... .......... 97% 10.3M 1s 254650K .......... .......... .......... .......... .......... 97% 9.32M 1s 254700K .......... .......... .......... .......... .......... 97% 8.94M 1s 254750K .......... .......... .......... .......... .......... 97% 11.9M 1s 254800K .......... .......... .......... .......... .......... 97% 12.6M 1s 254850K .......... .......... .......... .......... .......... 97% 10.6M 1s 254900K .......... .......... .......... .......... .......... 97% 10.4M 1s 254950K .......... .......... .......... .......... .......... 97% 7.22M 1s 255000K .......... .......... .......... .......... .......... 97% 219K 1s 255050K .......... .......... .......... .......... .......... 97% 5.95M 1s 255100K .......... .......... .......... .......... .......... 97% 5.79M 1s 255150K .......... .......... .......... .......... .......... 97% 9.58M 1s 255200K .......... .......... .......... .......... .......... 97% 8.79M 1s 255250K .......... .......... .......... .......... .......... 97% 9.29M 1s 255300K .......... .......... .......... .......... .......... 97% 11.0M 1s 255350K .......... .......... .......... .......... .......... 97% 14.6M 1s 255400K .......... .......... .......... .......... .......... 97% 19.4M 1s 255450K .......... .......... .......... .......... .......... 97% 13.9M 1s 255500K .......... .......... .......... .......... .......... 97% 18.3M 1s 255550K .......... .......... .......... .......... .......... 97% 18.0M 1s 255600K .......... .......... .......... .......... .......... 97% 17.8M 1s 255650K .......... .......... .......... .......... .......... 97% 13.3M 1s 255700K .......... .......... .......... .......... .......... 97% 15.7M 1s 255750K .......... .......... .......... .......... .......... 97% 11.0M 1s 255800K .......... .......... .......... .......... .......... 97% 12.7M 1s 255850K .......... .......... .......... .......... .......... 97% 11.4M 1s 255900K .......... .......... .......... .......... .......... 97% 10.5M 1s 255950K .......... .......... .......... .......... .......... 97% 12.0M 1s 256000K .......... .......... .......... .......... .......... 97% 23.6M 1s 256050K .......... .......... .......... .......... .......... 97% 26.4M 1s 256100K .......... .......... .......... .......... .......... 97% 14.7M 1s 256150K .......... .......... .......... .......... .......... 97% 22.0M 1s 256200K .......... .......... .......... .......... .......... 97% 18.7M 1s 256250K .......... .......... .......... .......... .......... 97% 28.9M 1s 256300K .......... .......... .......... .......... .......... 97% 25.6M 1s 256350K .......... .......... .......... .......... .......... 97% 21.7M 1s 256400K .......... .......... .......... .......... .......... 97% 23.3M 1s 256450K .......... .......... .......... .......... .......... 97% 16.7M 1s 256500K .......... .......... .......... .......... .......... 97% 23.6M 1s 256550K .......... .......... .......... .......... .......... 97% 21.0M 1s 256600K .......... .......... .......... .......... .......... 97% 15.7M 1s 256650K .......... .......... .......... .......... .......... 97% 17.3M 1s 256700K .......... .......... .......... .......... .......... 97% 13.3M 1s 256750K .......... .......... .......... .......... .......... 97% 12.4M 1s 256800K .......... .......... .......... .......... .......... 97% 11.4M 1s 256850K .......... .......... .......... .......... .......... 97% 8.96M 1s 256900K .......... .......... .......... .......... .......... 98% 10.4M 1s 256950K .......... .......... .......... .......... .......... 98% 11.0M 1s 257000K .......... .......... .......... .......... .......... 98% 13.3M 1s 257050K .......... .......... .......... .......... .......... 98% 8.27M 1s 257100K .......... .......... .......... .......... .......... 98% 6.74M 1s 257150K .......... .......... .......... .......... .......... 98% 8.53M 1s 257200K .......... .......... .......... .......... .......... 98% 8.23M 1s 257250K .......... .......... .......... .......... .......... 98% 10.0M 1s 257300K .......... .......... .......... .......... .......... 98% 7.24M 1s 257350K .......... .......... .......... .......... .......... 98% 7.12M 1s 257400K .......... .......... .......... .......... .......... 98% 10.2M 1s 257450K .......... .......... .......... .......... .......... 98% 9.68M 1s 257500K .......... .......... .......... .......... .......... 98% 11.6M 1s 257550K .......... .......... .......... .......... .......... 98% 11.5M 1s 257600K .......... .......... .......... .......... .......... 98% 8.16M 1s 257650K .......... .......... .......... .......... .......... 98% 13.7M 1s 257700K .......... .......... .......... .......... .......... 98% 12.1M 1s 257750K .......... .......... .......... .......... .......... 98% 12.4M 1s 257800K .......... .......... .......... .......... .......... 98% 9.25M 1s 257850K .......... .......... .......... .......... .......... 98% 8.94M 1s 257900K .......... .......... .......... .......... .......... 98% 11.0M 1s 257950K .......... .......... .......... .......... .......... 98% 8.06M 1s 258000K .......... .......... .......... .......... .......... 98% 8.42M 1s 258050K .......... .......... .......... .......... .......... 98% 8.04M 1s 258100K .......... .......... .......... .......... .......... 98% 7.36M 1s 258150K .......... .......... .......... .......... .......... 98% 6.31M 1s 258200K .......... .......... .......... .......... .......... 98% 2.85M 0s 258250K .......... .......... .......... .......... .......... 98% 9.04M 0s 258300K .......... .......... .......... .......... .......... 98% 10.2M 0s 258350K .......... .......... .......... .......... .......... 98% 9.78M 0s 258400K .......... .......... .......... .......... .......... 98% 10.7M 0s 258450K .......... .......... .......... .......... .......... 98% 7.98M 0s 258500K .......... .......... .......... .......... .......... 98% 11.4M 0s 258550K .......... .......... .......... .......... .......... 98% 14.8M 0s 258600K .......... .......... .......... .......... .......... 98% 16.0M 0s 258650K .......... .......... .......... .......... .......... 98% 16.3M 0s 258700K .......... .......... .......... .......... .......... 98% 8.80M 0s 258750K .......... .......... .......... .......... .......... 98% 13.4M 0s 258800K .......... .......... .......... .......... .......... 98% 14.8M 0s 258850K .......... .......... .......... .......... .......... 98% 11.7M 0s 258900K .......... .......... .......... .......... .......... 98% 12.4M 0s 258950K .......... .......... .......... .......... .......... 98% 6.45M 0s 259000K .......... .......... .......... .......... .......... 98% 5.89M 0s 259050K .......... .......... .......... .......... .......... 98% 8.44M 0s 259100K .......... .......... .......... .......... .......... 98% 9.56M 0s 259150K .......... .......... .......... .......... .......... 98% 10.8M 0s 259200K .......... .......... .......... .......... .......... 98% 7.53M 0s 259250K .......... .......... .......... .......... .......... 98% 16.3M 0s 259300K .......... .......... .......... .......... .......... 98% 11.5M 0s 259350K .......... .......... .......... .......... .......... 98% 9.61M 0s 259400K .......... .......... .......... .......... .......... 98% 11.6M 0s 259450K .......... .......... .......... .......... .......... 98% 6.33M 0s 259500K .......... .......... .......... .......... .......... 98% 7.35M 0s 259550K .......... .......... .......... .......... .......... 99% 8.47M 0s 259600K .......... .......... .......... .......... .......... 99% 7.96M 0s 259650K .......... .......... .......... .......... .......... 99% 10.9M 0s 259700K .......... .......... .......... .......... .......... 99% 15.6M 0s 259750K .......... .......... .......... .......... .......... 99% 21.0M 0s 259800K .......... .......... .......... .......... .......... 99% 19.5M 0s 259850K .......... .......... .......... .......... .......... 99% 13.2M 0s 259900K .......... .......... .......... .......... .......... 99% 18.7M 0s 259950K .......... .......... .......... .......... .......... 99% 9.97M 0s 260000K .......... .......... .......... .......... .......... 99% 11.6M 0s 260050K .......... .......... .......... .......... .......... 99% 16.7M 0s 260100K .......... .......... .......... .......... .......... 99% 16.4M 0s 260150K .......... .......... .......... .......... .......... 99% 19.7M 0s 260200K .......... .......... .......... .......... .......... 99% 14.8M 0s 260250K .......... .......... .......... .......... .......... 99% 16.4M 0s 260300K .......... .......... .......... .......... .......... 99% 16.7M 0s 260350K .......... .......... .......... .......... .......... 99% 12.7M 0s 260400K .......... .......... .......... .......... .......... 99% 16.0M 0s 260450K .......... .......... .......... .......... .......... 99% 12.7M 0s 260500K .......... .......... .......... .......... .......... 99% 14.1M 0s 260550K .......... .......... .......... .......... .......... 99% 12.6M 0s 260600K .......... .......... .......... .......... .......... 99% 5.35M 0s 260650K .......... .......... .......... .......... .......... 99% 5.17M 0s 260700K .......... .......... .......... .......... .......... 99% 3.83M 0s 260750K .......... .......... .......... .......... .......... 99% 5.55M 0s 260800K .......... .......... .......... .......... .......... 99% 11.7M 0s 260850K .......... .......... .......... .......... .......... 99% 9.92M 0s 260900K .......... .......... .......... .......... .......... 99% 10.3M 0s 260950K .......... .......... .......... .......... .......... 99% 11.0M 0s 261000K .......... .......... .......... .......... .......... 99% 10.5M 0s 261050K .......... .......... .......... .......... .......... 99% 14.3M 0s 261100K .......... .......... .......... .......... .......... 99% 11.0M 0s 261150K .......... .......... .......... .......... .......... 99% 12.0M 0s 261200K .......... .......... .......... .......... .......... 99% 18.7M 0s 261250K .......... .......... .......... .......... .......... 99% 24.2M 0s 261300K .......... .......... .......... .......... .......... 99% 8.95M 0s 261350K .......... .......... .......... .......... .......... 99% 45.7M 0s 261400K .......... .......... .......... .......... .......... 99% 20.5M 0s 261450K .......... .......... .......... .......... .......... 99% 11.9M 0s 261500K .......... .......... .......... .......... .......... 99% 12.3M 0s 261550K .......... .......... .......... .......... .......... 99% 12.4M 0s 261600K .......... .......... .......... .......... .......... 99% 11.6M 0s 261650K .......... .......... .......... .......... .......... 99% 14.6M 0s 261700K .......... .......... .......... .......... .......... 99% 9.31M 0s 261750K .......... .......... .......... .......... .......... 99% 12.7M 0s 261800K .......... .......... .......... .......... .......... 99% 9.63M 0s 261850K .......... .......... .......... .......... .......... 99% 10.2M 0s 261900K .......... .......... .......... .......... .......... 99% 8.45M 0s 261950K .......... .......... .......... .......... .......... 99% 8.46M 0s 262000K .......... .......... .......... .......... .......... 99% 10.8M 0s 262050K .......... .......... .......... .......... .......... 99% 12.1M 0s 262100K .......... .......... .......... .......... .......... 99% 11.1M 0s 262150K .......... .......... .......... .......... 100% 15.8M=33s 2024-04-28 10:17:33 (7.73 MB/s) - ‘ESPbeta.tgz’ saved [268483520/268483520] + tar -xf ESPbeta.tgz + rm -rf EngSketchPad/data/Slugs + python --version Python 3.11.9 + [[ '' == *\.\i\f\o\r\t ]] + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/config/ + ./makeEnv ESP runtime AutoConfigurator CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0 with contents: bin include lib share Info: Python exec /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python found! Info: Python header /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found! Info: Python library /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.so found! ESP_ARCH = LINUX64 ESP_ROOT = /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad EFCOMP = gfortran CARCH = LINUX64 CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0 CASARCH = . CASREV = 7.8 PYTHONINC= /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 + source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESPenv.sh ++ export ESP_ARCH=LINUX64 ++ ESP_ARCH=LINUX64 ++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad ++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad ++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASARCH=. ++ CASARCH=. ++ export CASREV=7.8 ++ CASREV=7.8 ++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 ++ PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 ++ export 'PYTHONLIB=-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11' ++ PYTHONLIB='-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11' ++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ export AFLR_ARCH=Linux-x86-64 ++ AFLR_ARCH=Linux-x86-64 ++ '[' -z /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ']' ++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph ++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph ++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0 ++ export 'SLUGS_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &' ++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &' ++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &' ++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &' ++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &' ++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &' + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src + make (cd EGADS/src; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src' touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64 rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64 cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64 touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD.h mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS.h mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/always_inline.h g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsGeom.cpp -o ./egadsGeom.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsHLevel.cpp -o ./egadsHLevel.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTopo.cpp -o ./egadsTopo.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsCopy.cpp -o ./egadsCopy.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSpline.cpp -o ./egadsSpline.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsIO.cpp -o ./egadsIO.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSplineFit.cpp -o ./egadsSplineFit.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSkinning.cpp -o ./egadsSkinning.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTessSens.cpp -o ./egadsTessSens.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsBase.c -o ./egadsBase.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o ./egadsMemory.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTess.c -o ./egadsTess.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTris.c -o ./egadsTris.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o ./egadsQuads.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsFit.c -o ./egadsFit.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o ./egadsRobust.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o ./egadsSBO.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmCfit.c -o ./prmCfit.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmGrid.c -o ./prmGrid.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmUV.c -o ./prmUV.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsExport.c -o ./egadsExport.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o ./egadsEffect.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o ./egadsSolids.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include ../util/emp.c \ -o ./emp.o g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/evaluate.c -o ./evaluate.o g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/rational.c -o ./rational.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \ ../util/regQuads.c -o ./regQuads.o g++ -g -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp ./SurrealD1 SurrealD1_test_suite Complete! g++ -g -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp ./SurrealD4 SurrealD4_test_suite Complete! g++ -g -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp ./SurrealS1 SurrealS1_test_suite Complete! g++ -g -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp ../util/SurrealS4_btest.cpp: In function ‘void multiply_deriv2()’: ../util/SurrealS4_btest.cpp:1265:23: note: variable tracking size limit exceeded with -fvar-tracking-assignments, retrying without BOOST_AUTO_TEST_CASE( multiply_deriv2 ) ^ ../util/SurrealS4_btest.cpp:19:42: note: in definition of macro ‘BOOST_AUTO_TEST_CASE’ #define BOOST_AUTO_TEST_CASE( fun ) void fun() ^~~ ./SurrealS4 SurrealS4_test_suite Complete! make -C ../util make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \ -o ./uvmap.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 egadsUVmap.c -Iuvmap \ -o ./egadsUVmap.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a (cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o uvmap_cpu_message.o uvmap_ibfibf.o uvmap_message.o uvmap_test.o uvmap_read.o uvmap_gen.o uvmap_gen_uv.o uvmap_inl_uv_bnd.o EG_uvmap_Read.o uvmap_chk_edge_ratio.o uvmap_idibe.o uvmap_ibeibe.o uvmap_iccin.o uvmap_malloc.o uvmap_to_egads.o EG_uvmap_Write.o uvmap_struct_tasks.o uvmap_iccibe.o EG_uvmapGen.o EG_uvmapTest.o uvmap_bnd_adj.o uvmap_ibfin.o uvmap_add.o uvmap_write.o EG_uvmapFindUV.o uvmap_version.o uvmap_chk_area_uv.o EG_uvmapStructFree.o uvmap_inibe.o uvmap_norm_uv.o uvmap_mben_disc.o uvmap_find_uv.o uvmap_solve.o uvmap_from_egads.o; ) ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a gcc -g -o ./uvmap.exe ./uvmap.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lrt -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util' touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so (cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so \ 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 \ -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm -lstdc++ -lrt ) touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a (cd .; \ ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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; ) gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsBase.c -o ./fgadsBase.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsMemory.c -o ./fgadsMemory.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsAttrs.c -o ./fgadsAttrs.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTess.c -o ./fgadsTess.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsHLevel.c -o ./fgadsHLevel.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsGeom.c -o ./fgadsGeom.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTopo.c -o ./fgadsTopo.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a (cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; ) ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a (cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a emp.o; ) ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a *** EGADS Build Complete! *** make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src' (cd EGADS/lite; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteBase.c -o ./liteBase.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteMemory.c -o ./liteMemory.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteGeom.c -o ./liteGeom.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteTopo.c -o ./liteTopo.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteAttrs.c -o ./liteAttrs.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteImport.c -o ./liteImport.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteString.c -o ./liteString.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o ./liteTess.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o ./liteTris.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src \ ../src/egadsQuads.c -o ./liteQuads.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o ./liteTessInp.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 ../src/egadsRobust.c \ -o ./egadsRobust.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLINUX64 -I../include ../util/emp.c \ -o ./emp.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o ./evaLite.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE ../util/rational.c \ -o ./ratLite.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I../util \ ../util/regQuads.c -o ./liteRegQuads.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o ./liteEffect.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o ./liteUVmap.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so (cd .; gcc -g -shared -Wl,-no-undefined \ -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so 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 \ -lpthread -lm ) touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a (cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite' (cd wvServer; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer' g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 map.cpp -o ./map.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include base64-decode.c -o ./base64-decode.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include handshake.c -o ./handshake.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include client-handshake.c -o ./client-handshake.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include md5.c -o ./md5.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include parsers.c -o ./parsers.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension.c -o ./extension.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include sha-1.c -o ./sha-1.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include server.c -o ./server.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include wv.c -o ./wv.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include browserMessage.c -o ./browserMessage.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a (cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -DSTANDALONE server.c \ -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -o ./servertest.o g++ -g -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a \ -lpthread -lz -lm touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so (cd .; g++ -g -shared -Wl,-no-undefined \ -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so 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 -lpthread) make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer' (cd EGADS/examples; make -f egads2cart.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cart.c \ -o ./egads2cart.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \ -lrt -lm make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' (cd EGADS/examples; make -f vCurvature.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' (cd EGADS/examples; make -f vGeom.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \ -lrt make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' (cd EGADS/examples; make -f vTess.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vTess.c -o ./vTess.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ../util/retessFaces.c \ -o ./retessFaces.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm \ -lpthread -lz -lrt -lm g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples' (cd OpenCSM; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udp.c -o ./udp.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o gcc -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lrt -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so ./udpWarp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o gfortran -g -c -O -fPIC -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J . touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h cp -p common.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM' (cd Slugs; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Fitter.c \ -o ./Fitter.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. RedBlackTree.c \ -o ./RedBlackTree.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Tessellate.c \ -o ./Tessellate.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \ ./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \ -lpthread -lz -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \ -lpthread -lz -lm make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs' (cd CAPS; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS' /bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libc3dio.a /bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libCart3D.a /bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/avl /bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pplot /bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pxplot /bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/xfoil /bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mastros.exe /bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.D01 /bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.IDX /bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mses /bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mset /bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr2AIM.so /bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr3AIM.so /bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr4AIM.so make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS' (cd CAPS/src; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src' touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \ -I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o ./aimTransferUtil.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \ aimMesh.c -o ./aimMesh.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \ ./aimTransferUtil.o ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsBase.c -o ./capsBase.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsBound.c -o ./capsBound.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsValue.c -o ./capsValue.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \ -I/usr/include/udunits2 printObject.c -o ./printObject.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so (cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so \ 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 -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \ -lrt -lm ) touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a (cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingAIM.c \ -o ./testingAIM.o rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so': No such file or directory Makefile:23: recipe for target '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so' failed make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored) gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingWriter.c \ -o ./testingWriter.o rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so rm: cannot remove '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so': No such file or directory Makefile:33: recipe for target '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so' failed make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored) gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -ldl -lrt -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include phaseUtil.c \ -o ./phaseUtil.o gcc -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src' (cd ../CAPSexamples; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples' (make -C cCAPS -f aeroelastic_SU2.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o gcc -g -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f avlTest.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o gcc -g -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f awaveTest.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o gcc -g -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f frictionTest.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o gcc -g -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f fun3d.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o gcc -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o gcc -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o gcc -g -o ./aeroelasticTest ./aeroelasticTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f hsm.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o gcc -g -o ./hsmTest ./hsmTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o gcc -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o gcc -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o gcc -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f interferenceTest.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceTest.c \ -o ./interferenceTest.o gcc -g -o ./interferenceTest ./interferenceTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f msesTest.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o gcc -g -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f mystran.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o gcc -g -o ./mystranTest ./mystranTest.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f pointwiseTest.make) make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o gcc -g -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \ -ludunits2 -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples' (cd CAPS/aim; make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim' make -C utils make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a (cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils' make -C friction make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \ -o ./frictionAIM.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm gfortran -g -c -O -fPIC -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o gfortran -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/friction ./friction.o -static-libgfortran -static-libgcc make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction' make -C tetgen make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen' g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tetgenAIM.cpp \ -o ./tetgenAIM.o g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I/home/jenkins/util/tetgen/tetgen1.6.0 -I../utils \ -DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DTETLIBRARY -w /home/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o g++ -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -O0 -w /home/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \ ./tetgen_Interface.o ./tetgen.o \ ./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -lrt -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen' make -C tacs make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \ -o ./tacsAIM.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs' make -C cbaero make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o gcc -g -shared -Wl,-no-undefined cbaeroAIM.o -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero' make -C pointwise make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils pointwiseAIM.c \ -o ./pointwiseAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hashElement.c \ -o ./hashElement.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -lrt -lm -lpthread make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise' make -C xfoil make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \ xfoilAIM.c -o ./xfoilAIM.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil' make -C aflr2 make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2' Not compiling aflr2AIM: AFLR must be set -- Please fix the environment.... make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2' make -C su2 make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \ -o ./su2AIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2Utils.c \ -o ./su2Utils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_4_Cardinal.c \ -o ./su2_4_Cardinal.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_5_Raven.c \ -o ./su2_5_Raven.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_6_Falcon.c \ -o ./su2_6_Falcon.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_7_Blackbird.c \ -o ./su2_7_Blackbird.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_801_Harrier.c \ -o ./su2_801_Harrier.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2' make -C skeleton make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \ -o ./skeletonAIM.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton' make -C cgt make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cgt.c \ -o ./egads2cgt.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aflr4egads.c \ -o ./aflr4egads.o g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt' make -C mses make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses' make -C egadsTess make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \ -o ./egadsTessAIM.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -lrt -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess' make -C sierraSD make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD' Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment.... make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD' make -C masstran make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran' g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \ -o ./masstranAIM.o g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran' make -C plato make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato' Not compiling platoAIM: SEACAS must be set -- Please fix the environment.... make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato' make -C refine make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \ -o ./refineAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 \ -I../meshWriter/libmeshbWriter/libMeshb/sources \ ../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -lrt -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine' make -C awave make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \ -o ./awaveAIM.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave' make -C tsfoil make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \ tsfoilAIM.c -o ./tsfoilAIM.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil' make -C fun3d make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \ -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \ fun3dUtils.c -o ./fun3dUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \ -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o Building FUN3D with Python gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \ ./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d' make -C delaundo make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \ -o ./delaundoAIM.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -lrt -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo' make -C abaqus make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \ abaqusAIM.c -o ./abaqusAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \ abaqusUtils.c -o ./abaqusUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \ -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o echo "Building Abaqus with Python" Building Abaqus with Python gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus' make -C aflr4 make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4' Not compiling aflr4AIM: AFLR must be set -- Please fix the environment.... make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4' make -C astros make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosAIM.c \ -o ./astrosAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosUtils.c \ -o ./astrosUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosCards.c \ -o ./astrosCards.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros' make -C interference make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceAIM.c \ -o ./interferenceAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. cloudFns.c \ -o ./cloudFns.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so \ ./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference' make -C meshWriter make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter' make -C libmeshbWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libmeshbWriter.c \ -o ./libmeshbWriter.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \ -o ./libmeshb7.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter' make -C fastWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fastWriter.c \ -o ./fastWriter.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter' make -C tecplotWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include tecplotWriter.c \ -o ./tecplotWriter.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter' make -C vtkWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vtkWriter.c \ -o ./vtkWriter.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter' make -C bstlWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bstlWriter.c \ -o ./bstlWriter.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter' make -C bvtkWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bvtkWriter.c \ -o ./bvtkWriter.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter' make -C su2Writer make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include su2Writer.c \ -o ./su2Writer.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer' make -C stlWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include stlWriter.c \ -o ./stlWriter.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter' make -C ugridWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ugridWriter.c \ -o ./ugridWriter.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter' make -C exodusWriter make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter' make[3]: Nothing to be done for 'default'. make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter' make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter' make -C nastran make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \ -o ./nastranAIM.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran' make -C sierraSM make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM' Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment.... make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM' make -C aflr3 make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3' Not compiling aflr3AIM: AFLR must be set -- Please fix the environment.... make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3' make -C hsm make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAIM.c \ -o src/hsmAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmUtils.c \ -o src/hsmUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAdj.c \ -o src/hsmAdj.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \ -o src/rcm.o g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \ -o src/genrcmi.o make -C src hsmbc.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src sbsolve.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmre1.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmdep.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmrfm.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmglr.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmrun.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmprj.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src atanc.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src ludcmp.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmbb2.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmabd.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src bmdump.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmren.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmeqn.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmsol.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmout.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src hsmgeo.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src cross.o make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' make -C src /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a make[3]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a (cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a make[3]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src' touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so \ src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \ src/rcm.o src/genrcmi.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -lstdc++ make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm' make -C avl make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_TOT.o ./avlRead_ELE.o ./avlRead_DERMATB.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_HINGE.o ./avlRead_DERMATS.o ./avlRead_STRP.o ./avlRead_VM.o ./avlRead_CPOML.o ./avlRead_DERMATM.o ./avlRead_SURF.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lstdc++ -lrt -lm make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl' make -C custom make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom' make[2]: Nothing to be done for 'default'. make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom' make -C cart3d make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d' make[2]: xml2-config: Command not found XML developer libarary missing. Not compiling cart3dAIM. make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d' make -C unitTest make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest' make[2]: Nothing to be done for 'all'. make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest' make -C mystran make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranAIM.c \ -o ./mystranAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \ -o ./mystranUtils.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \ -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran' make -C zaero make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero' make -C spinnaker make[2]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker' make[2]: Nothing to be done for 'default'. make[2]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker' make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim' (cd OpenCSM; make -f serveESP.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM' gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM' *** Build Completed! *** + export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data + CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin ++ uname -a + [[ Linux reynolds-ubuntu18 4.15.0-213-generic #224-Ubuntu SMP Mon Jun 19 13:30:12 UTC 2023 x86_64 x86_64 x86_64 GNU/Linux == *\D\a\r\w\i\n* ]] + sed -i 's/.*capsExamples.*/#&/' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh + bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh + expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:169]] ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)" ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:176]] ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)" ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:183]] iend must not be less than ibeg when evaluating "slice(e3,4,-1)" ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set) --> catching signal -258 (func_arg_out_of_bounds) ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:384]] index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:402]] index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:418]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:434]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:442]] row index must be between 1 and 2 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:450]] column index must be between 1 and 3 --> catching signal -262 (illegal_pmtr_index) ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:458]] column index must be between 1 and 3 --> catching signal -262 (illegal_pmtr_index) ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:1914]] signal 1 thrown by user --> catching signal 1 (UNKNOWN) ERROR:: (illegal_value) in Branch Brch_001813 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:1924]] vertex and base must be different --> catching signal -225 (illegal_value) ==> serveESP completed successfully with no verification data real 0m0.067s user 0m0.062s sys 0m0.004s + set +x ============================================= ESP verification case 01 passed (as expected) ============================================= + expectSuccess 02 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.309s user 0m0.312s sys 0m0.026s + set +x ============================================= ESP verification case 02 passed (as expected) ============================================= + expectSuccess 03 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m2.548s user 0m3.310s sys 0m0.104s + set +x ============================================= ESP verification case 03 passed (as expected) ============================================= + expectSuccess 04 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.609s user 0m0.737s sys 0m0.008s + set +x ============================================= ESP verification case 04 passed (as expected) ============================================= + expectSuccess 05 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.652s user 0m0.720s sys 0m0.017s + set +x ============================================= ESP verification case 05 passed (as expected) ============================================= + expectSuccess 06 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.612s user 0m0.719s sys 0m0.013s + set +x ============================================= ESP verification case 06 passed (as expected) ============================================= + expectSuccess 07 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m3.357s user 0m4.925s sys 0m0.080s + set +x ============================================= ESP verification case 07 passed (as expected) ============================================= + expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 0m29.272s user 0m42.447s sys 0m0.256s + set +x ============================================= ESP verification case 08 passed (as expected) ============================================= + expectSuccess 09 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.667s user 0m0.813s sys 0m0.020s + set +x ============================================= ESP verification case 09 passed (as expected) ============================================= + expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 0m36.807s user 1m0.620s sys 0m1.394s + set +x ============================================= ESP verification case 10 passed (as expected) ============================================= + expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 0m0.271s user 0m0.259s sys 0m0.020s + set +x ============================================= ESP verification case 11 passed (as expected) ============================================= + expectSuccess 12 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.667s user 0m0.741s sys 0m0.004s + set +x ============================================= ESP verification case 12 passed (as expected) ============================================= + expectSuccess 13 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped ==> serveESP completed successfully with no verification data real 0m0.124s user 0m0.152s sys 0m0.016s + set +x ============================================= ESP verification case 13 passed (as expected) ============================================= + expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3 + ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3 WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 0m0.332s user 0m0.445s sys 0m0.028s + set +x ============================================= ESP verification case 14 passed (as expected) ============================================= + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testEGADS + make test python --version Python 3.11.9 python -u -m unittest discover .................................................... PCurve Map: 48 (alloc 48)! Surface Map: 12 (alloc 24)! Curve Map: 28 (alloc 28)! Writing PCurves... Writing Curves... Writing Surfaces... Writing 16 Nodes... Writing 28 Edges... Writing 12 Loops... Writing 12 Faces... Writing 1 Shells... EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close! ................... ---------------------------------------------------------------------- Ran 71 tests in 2.138s OK + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testOCSM + source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/test_pyOCSM.sh ++ set -x ++ python -u test_pyOCSM.py -skipHelp real 0m6.017s user 0m9.538s sys 0m0.237s ++ set +x ================================================= test_pyOCSM.py passed (as expected) ================================================= + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testCAPS + make test python --version Python 3.11.9 python -u -m unittest discover ..Mapping Csys attributes ................ Number of unique Csys attributes = 2 Name = leftWingSkin, index = 1 Name = riteWingSkin, index = 2 Getting FEA coordinate systems....... Number of coordinate systems - 2 Coordinate system name - leftWingSkin Coordinate system name - riteWingSkin Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Upper_Left, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing1, index = 1 Name = Wing2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 143 Number of elements = 282 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 282 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 140 Number of elements = 276 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 276 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 283 Combined Number of elements = 558 Combined Elemental Nodes = 0 Combined Elemental Rods = 0 Combined Elemental Tria3 = 558 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 12.577s 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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/ + make test python --version Python 3.11.9 python -u -m unittest discover --verbose Please set the environment variable ASTROS_ROOT 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 Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM 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 = 0.031 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 = 0.098 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.008 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 = 0.038 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 = 0.117 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 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 = 0.031 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 = 0.098 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.008 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 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 = 0.039 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 = 0.104 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 23187 44150 AFLR2 : CPU Time = 0.023 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 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 = 0.042 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 = 0.111 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 29897 57550 AFLR2 : CPU Time = 0.008 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 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 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 = 0.008 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 4705 9066 AFLR2 : CPU Time = 0.001 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4705 Number of elements = 9410 Number of tris = 9066 Number of quad = 0 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing Binary VTK file .... Finished writing Binary VTK 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 libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates! 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 = 0.001 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 = 0.012 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 = 0.007 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 Writing ASCII STL file .... Finished writing ASCII STL file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing Binary VTK file .... Finished writing Binary VTK 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 libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!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 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 = 0.013 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 = 0.007 seconds AFLR2 : DONE Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 4055 Number of elements = 4420 Number of tris = 386 Number of quad = 3690 Writing Tecplot file .... Finished writing Tecplot file ok test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM 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 Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR4 : Compile Date 04/23/24 @ 12:17PM 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 = 6092 Number of elements = 33723 Number of triangles = 4434 Number of quadrilatarals = 0 Number of tetrahedrals = 29289 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 = 13578 Number of elements = 76165 Number of triangles = 8144 Number of quadrilatarals = 0 Number of tetrahedrals = 68021 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 = 42341 Number of elements = 240656 Number of triangles = 19890 Number of quadrilatarals = 0 Number of tetrahedrals = 220766 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 = 4356 Number of elements = 24173 Number of triangles = 3018 Number of quadrilatarals = 0 Number of tetrahedrals = 21155 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 = 10984 Number of elements = 60667 Number of triangles = 8628 Number of quadrilatarals = 0 Number of tetrahedrals = 52039 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 = 10678 Number of elements = 59894 Number of triangles = 6366 Number of quadrilatarals = 0 Number of tetrahedrals = 53528 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 = 89218 Number of elements = 501527 Number of triangles = 51812 Number of quadrilatarals = 0 Number of tetrahedrals = 449715 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Getting volume mesh EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 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 = 16488 Number of elements = 93795 Number of triangles = 7926 Number of quadrilatarals = 0 Number of tetrahedrals = 85869 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 = 3649 Number of elements = 19777 Number of triangles = 3394 Number of quadrilatarals = 0 Number of tetrahedrals = 16383 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 = 5514 Number of elements = 30658 Number of triangles = 3656 Number of quadrilatarals = 0 Number of tetrahedrals = 27002 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 = 5092 Number of elements = 27888 Number of triangles = 4070 Number of quadrilatarals = 0 Number of tetrahedrals = 23818 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 = 5238 Number of elements = 28440 Number of triangles = 4622 Number of quadrilatarals = 0 Number of tetrahedrals = 23818 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 = 4902 Number of elements = 26933 Number of triangles = 4038 Number of quadrilatarals = 0 Number of tetrahedrals = 22895 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Getting volume mesh for body 2 (of 2) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- Volume mesh for body 2 (of 2): Number of nodes = 336 Number of elements = 1507 Number of triangles = 584 Number of quadrilatarals = 0 Number of tetrahedrals = 923 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 = 33106 Number of elements = 191761 Number of triangles = 8496 Number of quadrilatarals = 0 Number of tetrahedrals = 183265 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 = 36447 Number of elements = 205093 Number of triangles = 21828 Number of quadrilatarals = 0 Number of tetrahedrals = 183265 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 = 28882 Number of elements = 164134 Number of triangles = 15162 Number of quadrilatarals = 0 Number of tetrahedrals = 148972 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 = 1415 Number of elements = 7515 Number of triangles = 1456 Number of quadrilatarals = 0 Number of tetrahedrals = 6059 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 = 4186 Number of elements = 23181 Number of triangles = 2942 Number of quadrilatarals = 0 Number of tetrahedrals = 20239 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 = 1253 Number of elements = 6578 Number of triangles = 1424 Number of quadrilatarals = 0 Number of tetrahedrals = 5154 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 = 16786 Number of elements = 95215 Number of triangles = 8798 Number of quadrilatarals = 0 Number of tetrahedrals = 86417 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 = 18710 Number of elements = 102591 Number of triangles = 16174 Number of quadrilatarals = 0 Number of tetrahedrals = 86417 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 = 12124 Number of elements = 68112 Number of triangles = 7138 Number of quadrilatarals = 0 Number of tetrahedrals = 60974 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 = 6586 Number of elements = 34479 Number of triangles = 9036 Number of quadrilatarals = 0 Number of tetrahedrals = 25443 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 = 2940 Number of elements = 12771 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7319 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 = 2497 Number of elements = 10947 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6395 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 = 2940 Number of elements = 12771 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7319 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 = 2497 Number of elements = 10947 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6395 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 = 2940 Number of elements = 12771 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7319 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 = 2497 Number of elements = 10947 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6395 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 = 2940 Number of elements = 12771 Number of triangles = 5452 Number of quadrilatarals = 0 Number of tetrahedrals = 7319 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 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 = 2497 Number of elements = 10947 Number of triangles = 4552 Number of quadrilatarals = 0 Number of tetrahedrals = 6395 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 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 = 5047 Number of elements = 27987 Number of triangles = 3464 Number of quadrilatarals = 0 Number of tetrahedrals = 24523 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 = 6342 Number of elements = 35410 Number of triangles = 4052 Number of quadrilatarals = 0 Number of tetrahedrals = 31358 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 = 60311 Number of elements = 351913 Number of triangles = 12928 Number of quadrilatarals = 0 Number of tetrahedrals = 338985 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 = 59175 Number of elements = 344623 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 332195 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 = 60311 Number of elements = 351413 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 338985 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file ok test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 4 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Wake, index = 3 Name = Farfield, index = 4 AFLR4 : Proximity BG Surface Grid Generation Skipped AFLR4 : No Modifications Required ok test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - trailingEdge Done getting mesh sizing parameters ok test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wall, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example2.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example3.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example4.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example6.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example7.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example8.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/example9.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/multi_prim.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing Tecplot file .... Finished writing Tecplot file Writing Tecplot file .... Finished writing Tecplot file ok test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ok test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 ok test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 file Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 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) ... skipped 'No astros.exe executable' test_Plate (test_astros.TestAstros.test_Plate) ... skipped 'No astros.exe executable' 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 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 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 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_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:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 9 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = nodeBody, index = 8 Name = farfield, index = 9 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 7F4AD42FC740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7F4AD42FC740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7F4AB2883700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7F4AB2883700 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 7F4AD42FC740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7F4AD42FC740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7F4AB3885700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7F4AB3885700 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 7F4AB3885700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7F4AD42FC740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7F4AB3885700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7F4AD42FC740 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 7F4AD42FC740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7F4AD42FC740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7F4AB2883700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7F4AB2883700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! ok test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 ok test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) ok test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = nodeBody, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 ok test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting mesh sizing parameters Mesh sizing name - box Done getting mesh sizing parameters ok test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 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 Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk surface file .... capsGroups found: 1: Farfield 2: Wing1 Finished writing vtk file Writing ugrid file .... Finished writing ugrid file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 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 = 7766 Number of elements = 15528 Number of triangle elements = 15528 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5870 Number of elements = 11736 Number of triangle elements = 11736 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14124 Total number of elements = 28236 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 - 14124, elements - 28236 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.14858 Creating surface mesh ... Surface mesh seconds: 0.031856 Recovering boundaries... Boundary recovery seconds: 0.119687 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.056128 Recovering Delaunayness... Delaunay recovery seconds: 0.066321 Refining mesh... 18827 insertions, added 13420 points, 721721 tetrahedra in queue. 6269 insertions, added 2485 points, 625204 tetrahedra in queue. 8356 insertions, added 2101 points, 168215 tetrahedra in queue. Refinement seconds: 2.75304 Smoothing vertices... Mesh smoothing seconds: 2.30656 Improving mesh... Mesh improvement seconds: 0.055508 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.013815 Total running seconds: 5.552 Statistics: Input points: 14124 Input facets: 28236 Input segments: 42354 Input holes: 2 Input regions: 0 Mesh points: 33059 Mesh tetrahedra: 159851 Mesh faces: 333820 Mesh faces on exterior boundary: 28236 Mesh faces on input facets: 28236 Mesh edges on input segments: 42354 Steiner points inside domain: 18935 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 = 7766 Number of elements = 15528 Number of triangle elements = 15528 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5870 Number of elements = 11736 Number of triangle elements = 11736 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 488 Number of elements = 972 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14124 Total number of elements = 28236 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 - 14124, elements - 28236 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.146967 Creating surface mesh ... Surface mesh seconds: 0.031192 Recovering boundaries... Boundary recovery seconds: 0.121326 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.057837 Recovering Delaunayness... Delaunay recovery seconds: 0.067387 Refining mesh... 18827 insertions, added 13420 points, 721721 tetrahedra in queue. 6269 insertions, added 2485 points, 625204 tetrahedra in queue. 8356 insertions, added 2101 points, 168215 tetrahedra in queue. Refinement seconds: 2.67886 Smoothing vertices... Mesh smoothing seconds: 2.32736 Improving mesh... Mesh improvement seconds: 0.057229 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.013516 Total running seconds: 5.50224 Statistics: Input points: 14124 Input facets: 28236 Input segments: 42354 Input holes: 2 Input regions: 0 Mesh points: 33059 Mesh tetrahedra: 159851 Mesh faces: 333820 Mesh faces on exterior boundary: 28236 Mesh faces on input facets: 28236 Mesh edges on input segments: 42354 Steiner points inside domain: 18935 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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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) /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 - 5043, elements - 10074 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 - 5043, elements - 10074 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 - 14124, elements - 28236 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) ... skipped "No 'ref' executable" test_all (test_refine.TestREFINE.test_all) ... skipped "No 'ref' executable" test_box_volume (test_refine.TestREFINE.test_box_volume) ... skipped "No 'ref' executable" test_boxhole (test_refine.TestREFINE.test_boxhole) ... skipped "No 'ref' executable" test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... skipped "No 'ref' executable" test_fun3d (test_refine.TestREFINE.test_fun3d) ... skipped "No 'ref' executable" test_inputs (test_refine.TestREFINE.test_inputs) ... skipped "No 'ref' executable" test_phase (test_refine.TestREFINE.test_phase) ... skipped "No 'ref' executable" test_sphere (test_refine.TestREFINE.test_sphere) ... skipped "No 'ref' executable" EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! 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 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 Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR3 : Compile Date 03/08/24 @ 01:03AM 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 = 0.017 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 43475 AFLR3 IG : Nodes, Elements = 6227 43439 AFLR3 IG : Nodes, Elements = 6220 26110 AFLR3 IG : Nodes, Elements = 6220 26133 AFLR3 IG : Nodes, Elements = 6220 21488 AFLR3 IG : Nodes, Elements = 6220 19195 AFLR3 : CPU Time = 0.187 seconds AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION AFLR3 GG : Nodes, Elements = 6220 19195 AFLR3 GG : Nodes, Elements = 9104 28052 AFLR3 GG : Nodes, Elements = 9104 39102 AFLR3 GG : Nodes, Elements = 9104 36335 AFLR3 GG : Nodes, Elements = 9104 34880 AFLR3 GG : Nodes, Elements = 11662 42890 AFLR3 GG : Nodes, Elements = 11662 54004 AFLR3 GG : Nodes, Elements = 11662 50843 AFLR3 GG : Nodes, Elements = 11662 49925 AFLR3 GG : Nodes, Elements = 14498 58736 AFLR3 GG : Nodes, Elements = 14498 71038 AFLR3 GG : Nodes, Elements = 14498 67638 AFLR3 GG : Nodes, Elements = 14498 66762 AFLR3 GG : Nodes, Elements = 17480 75922 AFLR3 GG : Nodes, Elements = 17480 88720 AFLR3 GG : Nodes, Elements = 17480 85188 AFLR3 GG : Nodes, Elements = 17480 84349 AFLR3 GG : Nodes, Elements = 20711 94213 AFLR3 GG : Nodes, Elements = 20711 107855 AFLR3 GG : Nodes, Elements = 20711 104214 AFLR3 GG : Nodes, Elements = 20711 103375 AFLR3 GG : Nodes, Elements = 24093 113678 AFLR3 GG : Nodes, Elements = 24093 128254 AFLR3 GG : Nodes, Elements = 24093 124257 AFLR3 GG : Nodes, Elements = 24093 123406 AFLR3 GG : Nodes, Elements = 27618 134141 AFLR3 GG : Nodes, Elements = 27618 149080 AFLR3 GG : Nodes, Elements = 27618 145168 AFLR3 GG : Nodes, Elements = 27618 144374 AFLR3 GG : Nodes, Elements = 31189 155227 AFLR3 GG : Nodes, Elements = 31189 170286 AFLR3 GG : Nodes, Elements = 31189 166309 AFLR3 GG : Nodes, Elements = 31189 165453 AFLR3 GG : Nodes, Elements = 34751 176284 AFLR3 GG : Nodes, Elements = 34751 191463 AFLR3 GG : Nodes, Elements = 34751 187411 AFLR3 GG : Nodes, Elements = 34751 186588 AFLR3 GG : Nodes, Elements = 38283 197293 AFLR3 GG : Nodes, Elements = 38283 212453 AFLR3 GG : Nodes, Elements = 38283 208438 AFLR3 GG : Nodes, Elements = 38283 207716 AFLR3 GG : Nodes, Elements = 41833 218438 AFLR3 GG : Nodes, Elements = 41833 233399 AFLR3 GG : Nodes, Elements = 41833 229556 AFLR3 GG : Nodes, Elements = 41833 228802 AFLR3 GG : Nodes, Elements = 45233 239061 AFLR3 GG : Nodes, Elements = 45233 253453 AFLR3 GG : Nodes, Elements = 45233 249686 AFLR3 GG : Nodes, Elements = 45233 248980 AFLR3 GG : Nodes, Elements = 48547 258960 AFLR3 GG : Nodes, Elements = 48547 273037 AFLR3 GG : Nodes, Elements = 48547 269340 AFLR3 GG : Nodes, Elements = 48547 268660 AFLR3 GG : Nodes, Elements = 51788 278411 AFLR3 GG : Nodes, Elements = 51788 292195 AFLR3 GG : Nodes, Elements = 51788 288655 AFLR3 GG : Nodes, Elements = 51788 288020 AFLR3 GG : Nodes, Elements = 54897 297367 AFLR3 GG : Nodes, Elements = 54897 310536 AFLR3 GG : Nodes, Elements = 54897 307175 AFLR3 GG : Nodes, Elements = 54897 306599 AFLR3 GG : Nodes, Elements = 57861 315502 AFLR3 GG : Nodes, Elements = 57861 327967 AFLR3 GG : Nodes, Elements = 57861 324838 AFLR3 GG : Nodes, Elements = 57861 324290 AFLR3 GG : Nodes, Elements = 60791 333083 AFLR3 GG : Nodes, Elements = 60791 345364 AFLR3 GG : Nodes, Elements = 60791 342206 AFLR3 GG : Nodes, Elements = 60791 341750 AFLR3 GG : Nodes, Elements = 63489 349850 AFLR3 GG : Nodes, Elements = 63489 361174 AFLR3 GG : Nodes, Elements = 63489 358324 AFLR3 GG : Nodes, Elements = 63489 357881 AFLR3 GG : Nodes, Elements = 65986 365375 AFLR3 GG : Nodes, Elements = 65986 375877 AFLR3 GG : Nodes, Elements = 65986 373150 AFLR3 GG : Nodes, Elements = 65986 372801 AFLR3 GG : Nodes, Elements = 68262 379634 AFLR3 GG : Nodes, Elements = 68262 389039 AFLR3 GG : Nodes, Elements = 68262 386682 AFLR3 GG : Nodes, Elements = 68262 386428 AFLR3 GG : Nodes, Elements = 70242 392370 AFLR3 GG : Nodes, Elements = 70242 400574 AFLR3 GG : Nodes, Elements = 70242 398524 AFLR3 GG : Nodes, Elements = 70242 398290 AFLR3 GG : Nodes, Elements = 71834 403067 AFLR3 GG : Nodes, Elements = 71834 409901 AFLR3 GG : Nodes, Elements = 71834 408035 AFLR3 GG : Nodes, Elements = 71834 407840 AFLR3 GG : Nodes, Elements = 73096 411631 AFLR3 GG : Nodes, Elements = 73096 416942 AFLR3 GG : Nodes, Elements = 73096 415543 AFLR3 GG : Nodes, Elements = 73096 415387 AFLR3 GG : Nodes, Elements = 74042 418225 AFLR3 GG : Nodes, Elements = 74042 422196 AFLR3 GG : Nodes, Elements = 74042 421120 AFLR3 GG : Nodes, Elements = 74042 421030 AFLR3 GG : Nodes, Elements = 74697 422995 AFLR3 GG : Nodes, Elements = 74697 425691 AFLR3 GG : Nodes, Elements = 74697 424979 AFLR3 GG : Nodes, Elements = 74697 424921 AFLR3 GG : Nodes, Elements = 75147 426271 AFLR3 GG : Nodes, Elements = 75147 428179 AFLR3 GG : Nodes, Elements = 75147 427658 AFLR3 GG : Nodes, Elements = 75147 427613 AFLR3 GG : Nodes, Elements = 75442 428499 AFLR3 GG : Nodes, Elements = 75442 429739 AFLR3 GG : Nodes, Elements = 75442 429380 AFLR3 GG : Nodes, Elements = 75442 429354 AFLR3 GG : Nodes, Elements = 75634 429930 AFLR3 GG : Nodes, Elements = 75634 430753 AFLR3 GG : Nodes, Elements = 75634 430521 AFLR3 GG : Nodes, Elements = 75634 430497 AFLR3 GG : Nodes, Elements = 75743 430824 AFLR3 GG : Nodes, Elements = 75743 431284 AFLR3 GG : Nodes, Elements = 75743 431147 AFLR3 GG : Nodes, Elements = 75743 431140 AFLR3 GG : Nodes, Elements = 75813 431351 AFLR3 GG : Nodes, Elements = 75813 431632 AFLR3 GG : Nodes, Elements = 75813 431554 AFLR3 GG : Nodes, Elements = 75813 431549 AFLR3 GG : Nodes, Elements = 75854 431672 AFLR3 GG : Nodes, Elements = 75854 431830 AFLR3 GG : Nodes, Elements = 75854 431793 AFLR3 GG : Nodes, Elements = 75854 431785 AFLR3 GG : Nodes, Elements = 75878 431857 AFLR3 GG : Nodes, Elements = 75878 431960 AFLR3 GG : Nodes, Elements = 75878 431923 AFLR3 GG : Nodes, Elements = 75878 431919 AFLR3 GG : Nodes, Elements = 75896 431973 AFLR3 GG : Nodes, Elements = 75896 432050 AFLR3 GG : Nodes, Elements = 75896 432029 AFLR3 GG : Nodes, Elements = 75896 432027 AFLR3 GG : Nodes, Elements = 75911 432072 AFLR3 GG : Nodes, Elements = 75911 432140 AFLR3 GG : Nodes, Elements = 75911 432115 AFLR3 GG : Nodes, Elements = 75911 432113 AFLR3 GG : Nodes, Elements = 75917 432131 AFLR3 GG : Nodes, Elements = 75917 432161 AFLR3 GG : Nodes, Elements = 75917 432148 AFLR3 GG : Nodes, Elements = 75917 432146 AFLR3 GG : Nodes, Elements = 75922 432161 AFLR3 GG : Nodes, Elements = 75922 432186 AFLR3 GG : Nodes, Elements = 75922 432175 AFLR3 GG : Nodes, Elements = 75925 432184 AFLR3 GG : Nodes, Elements = 75925 432192 AFLR3 GG : Nodes, Elements = 75925 432191 AFLR3 GG : Nodes, Elements = 75927 432197 AFLR3 GG : Nodes, Elements = 75927 432207 AFLR3 GG : Nodes, Elements = 75927 432204 AFLR3 GG : Nodes, Elements = 75929 432210 AFLR3 GG : Nodes, Elements = 75929 432216 AFLR3 GG : Nodes, Elements = 75929 432215 AFLR3 GG : Nodes, Elements = 75932 432224 AFLR3 GG : Nodes, Elements = 75932 432240 AFLR3 GG : Nodes, Elements = 75932 432234 AFLR3 GG : Nodes, Elements = 75932 432233 AFLR3 GG : Nodes, Elements = 75933 432236 AFLR3 GG : Nodes, Elements = 75933 432244 AFLR3 GG : Nodes, Elements = 75933 432241 AFLR3 GG : Nodes, Elements = 75933 432240 AFLR3 GG : Nodes, Elements = 75962 432327 AFLR3 GG : Nodes, Elements = 75962 432440 AFLR3 GG : Nodes, Elements = 75962 432401 AFLR3 GG : Nodes, Elements = 75962 432400 AFLR3 GG : Nodes, Elements = 75964 432406 AFLR3 GG : Nodes, Elements = 75964 432411 AFLR3 GG : Nodes, Elements = 75964 432408 AFLR3 : CPU Time = 6.705 seconds AFLR3 QI : QUALITY IMPROVEMENT AFLR3 QI : Nodes, Elements = 75964 432408 AFLR3 QI : Nodes, Elements = 74464 423905 AFLR3 QI : Nodes, Elements = 74236 422620 AFLR3 QI : Nodes, Elements = 74218 422515 AFLR3 QI : Nodes, Elements = 74218 426676 AFLR3 QI : Nodes, Elements = 74218 422354 AFLR3 QI : Nodes, Elements = 74218 421937 AFLR3 QI : Nodes, Elements = 74218 422317 AFLR3 QI : Nodes, Elements = 74218 421673 AFLR3 QI : Nodes, Elements = 74218 421449 AFLR3 QI : Nodes, Elements = 74218 421720 AFLR3 QI : Nodes, Elements = 74218 421413 AFLR3 QI : Nodes, Elements = 74218 421313 AFLR3 QI : Nodes, Elements = 74218 421535 AFLR3 QI : Nodes, Elements = 74218 421304 AFLR3 QI : Nodes, Elements = 74218 421266 AFLR3 QI : Nodes, Elements = 74218 421471 AFLR3 QI : Nodes, Elements = 74218 421263 AFLR3 QI : Nodes, Elements = 74218 421232 AFLR3 QI : Nodes, Elements = 74223 421255 AFLR3 QI : Nodes, Elements = 74223 421470 AFLR3 QI : Nodes, Elements = 74223 421272 AFLR3 QI : Nodes, Elements = 74223 421260 AFLR3 QI : Nodes, Elements = 74223 421451 AFLR3 QI : Nodes, Elements = 74223 421266 AFLR3 QI : Nodes, Elements = 74223 421234 AFLR3 : CPU Time = 1.968 seconds AFLR3 QRG: QUALITY GRID RE-GENERATION AFLR3 QRG: Nodes, Elements = 74223 421234 AFLR3 QRG: Nodes, Elements = 74223 421233 AFLR3 QRG: Nodes, Elements = 74223 421232 AFLR3 QRG: Nodes, Elements = 74225 421243 AFLR3 QRG: Nodes, Elements = 74230 421269 AFLR3 QRG: Nodes, Elements = 74239 421316 AFLR3 : CPU Time = 0.114 seconds AFLR3 : DONE UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 421316 UG3 : Min, Max Ang = 1.064 171.4 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 62 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 421316 UG3 : Min Vol = 6.77e-10 UG3 : Average Vol = 5.04 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 = 421316 UG3 : Min, Max Q = 0.0787 1 UG3 : Average Q = 0.894 UG3 : No. Q< 0.1 = 24 UG3 : No. Q< 0.01 = 0 OVERALL : CPU Time = 9.363 seconds UG3 : DIHEDRAL ANGLE CHECK UG3 : No. Tet Elems = 421316 UG3 : Min, Max Ang = 1.064 171.4 UG3 : Average Angle = 70.2 UG3 : No. Angle>160.0 = 62 UG3 : No. Angle>179.9 = 0 UG3 : VOL CHECK UG3 : Total-Volume = 2.12e+06 UG3 : No. Tet Elems = 421316 UG3 : Min Vol = 6.77e-10 UG3 : Average Vol = 5.04 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 = 421316 UG3 : Min, Max Q = 0.188 1 UG3 : Average Q = 0.854 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 = 74239 Number of elements = 433744 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 421316 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 = 74239 Number of elements = 433744 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 421316 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 = 74239 Number of elements = 433744 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 421316 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 = 74239 Number of elements = 433744 Number of triangles = 12428 Number of quadrilatarals = 0 Number of tetrahedrals = 421316 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:61955) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 7F4AB3885700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7F4AD42FC740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7F4AB3885700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7F4AD42FC740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 296 Number of elements = 588 Number of triangle elements = 588 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 487 Number of elements = 970 Number of triangle elements = 970 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 = 4193 Total number of elements = 8366 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 - 296, elements - 588 Body 3 number of surface: nodes - 487, elements - 970 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 - 296, elements - 588 Body 3 number of surface: nodes - 487, elements - 970 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 - 4193, elements - 8366 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 = 1352 Number of elements = 2684 Number of triangle elements = 2684 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 288 Number of elements = 572 Number of triangle elements = 572 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 173 Number of elements = 342 Number of triangle elements = 342 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 26 Number of elements = 48 Number of triangle elements = 48 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 482 Number of elements = 960 Number of triangle elements = 960 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 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 - 1352, elements - 2684 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 173, elements - 342 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 1352, elements - 2684 Body 2 number of surface: nodes - 288, elements - 572 Body 3 number of surface: nodes - 173, elements - 342 Body 4 number of surface: nodes - 26, elements - 48 Body 5 number of surface: nodes - 482, elements - 960 Getting volume mesh for body 1 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 2 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 3 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 4 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Getting volume mesh for body 5 (of 5) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! ../csmData/MultiDomain/cyl_seam.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 440 Number of elements = 876 Number of triangle elements = 876 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 = 962 Total number of elements = 1920 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = dummy_att, index = 1 Body 1 number of surface: nodes - 440, elements - 876 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 - 440, elements - 876 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 - 9626, elements - 19244 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 - 9626, elements - 19244 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 - 9626, elements - 19244 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 - 9626, elements - 19244 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 - 9626, elements - 19244 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 - 7130, elements - 14252 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 = 9626 Number of elements = 19244 Number of triangle elements = 19244 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9626 Total number of elements = 19244 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file Writing ASCII STL file .... Finished writing ASCII STL file Writing FAST file .... Finished writing FAST file Writing Binary STL file .... Finished writing Binary STL file Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing Binary VTK file .... Finished writing Binary VTK file Writing SU2 file .... Finished writing SU2 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, 69822.813292, 6179.981375, 19723.152207, 370546.335524] ok ---------------------------------------------------------------------- Ran 143 tests in 513.839s OK (skipped=26) + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/ + make test TYPE=MINIMAL (make -C cCAPS -f aeroelastic_SU2.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f avlTest.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'avlTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f awaveTest.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'awaveTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f frictionTest.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'frictionTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f fun3d.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: Nothing to be done for 'fun3d'. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f hsm.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'hsm' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f interferenceTest.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'interferenceTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f msesTest.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'msesTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f mystran.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'mystranTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (make -C cCAPS -f pointwiseTest.make) make[1]: Entering directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' make[1]: 'pointwiseTest' is up to date. make[1]: Leaving directory '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS' (cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL) Running.... MINIMAL c-Tests All tests pass! (cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL) ================================================= Using python : /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python ================================================= Running.... MINIMAL PyTests ================================================= + echo 'avl_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 0.0006119078685746836 CYtot -6.288067668554914e-15 CZtot -0.3012861394886091 Cltot -4.782099331324466e-14 Cmtot -0.1945055953450467 Cntot -2.339543963831951e-15 Cl'tot -4.785454061647156e-14 Cn'tot -1.504596228417061e-15 CLtot 0.3012509314150772 CDtot 0.004646353488232841 CDvis 0.0 CLff 0.3009503023520527 CYff -7.718708857566269e-15 CDind 0.004646353488232841 CDff 0.004968969500908292 e 0.9669902146157957 StripForces Wing cl = [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408] Wing cd = [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545] real 0m0.739s user 0m0.489s sys 0m0.345s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'xfoil_PyTest.py test;' xfoil_PyTest.py test; + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u xfoil_PyTest.py -outLevel=0 -noPlotData Cl = [1.05475230552567, 1.36488869373635, 1.56607214272105, 2.03059709344862, 1.97271083121169, 1.87307153172386, 1.76050475760117] Cd = [0.0131991208675727, 0.0166540240605751, 0.0200551482562831, 0.0458671341969345, 0.0754256009394856, 0.0994469174477522, 0.127479430989037] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.4960441144043, 0.461377732041502, 0.44237656820185, 0.361251636355465, 0.276104140853559, 0.214381239321467, 0.132988264746661] real 0m4.780s user 0m4.718s sys 0m0.268s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= ================================================= + echo 'mses_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Cl = 0.37837910855492407 Cd = 0.007775858417210143 Cm = 0.005262636995811319 real 0m5.049s user 0m4.885s sys 0m0.219s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected) ================================================= ================================================= + echo 'friction_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Loading AIM Setting Mach & Altitude Values Lifting Surface: Body = 1, units m XLE: 1.571946 -3.872983 0.249728 XTE: 2.536563 -3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 2, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.614012 0.000000 0.002015 Chord: 1.614013 Arc: 3.308635 T/C: 0.127839 Type: Wing Lifting Surface: Body = 3, units m XLE: 1.571946 3.872983 0.249728 XTE: 2.536563 3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 4, units m XLE: 5.484123 0.000000 1.468246 XTE: 6.210307 0.000915 1.468246 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: VTail Lifting Surface: Body = 5, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.210307 0.001525 0.500000 Chord: 1.210308 Arc: 2.471195 T/C: 0.120035 Type: VTail Lifting Surface: Body = 6, units m XLE: 5.484123 -0.968246 0.500000 XTE: 6.210307 -0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Lifting Surface: Body = 7, units m XLE: 5.484123 0.968246 0.500000 XTE: 6.210307 0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Body of Revolution: Body = 8, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 9, units m Arc: 3.714180 Diameter: 1.020621 Type: Fuse Body of Revolution: Body = 10, units m Arc: 2.771209 Diameter: 0.645497 Type: Fuse Body of Revolution: Body = 11, units m Arc: 1.013945 Diameter: 0.322749 Type: Fuse Body of Revolution: Body = 12, units m Arc: 0.101394 Diameter: 0.032275 Type: Fuse Number of sections 4, number of revolution sections 1 Number of Mach-Altitude cases = 2 Total drag = [0.0132, 0.01226] Form drag = [0.0033, 0.00307] Friction drag = [0.0099, 0.00919] real 0m0.463s user 0m0.363s sys 0m0.217s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tsfoil_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Getting results PAUSE Press the ENTER key to exit To resume execution, type go. Other input will terminate the job. Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Cl = 0.933329 Cd = 0.000283 Cd Wave = 0.0 Cm = -0.203433 Cp _Critcal = -1.303869 real 0m0.652s user 0m0.556s sys 0m0.272s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo 'delaundo_PyTest.py test;' delaundo_PyTest.py test; + python -u delaundo_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Name = AirfoilTE, index = 6 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 6 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Name = AirfoilTE, index = 6 Getting mesh sizing parameters Mesh sizing name - Airfoil Mesh sizing name - AirfoilTE Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting edge discretization for body 1 Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping! Swapping z and y coordinates! Writing delaundo control file - delaundo.ctr Writing out *.pts file Reading delaundo mesh file - delaundo_CAPS.mesh Swapping y and z coordinates! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file Writing ugrid file .... Finished writing ugrid file real 0m0.647s user 0m0.563s sys 0m0.247s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected) ================================================= ================================================= + echo 'egadsTess_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt egadsTess_PyTest.py test; + python -u egadsTess_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 0m8.565s user 0m12.613s sys 0m0.562s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr2_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr2_PyTest.py test; + python -u aflr2_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 5 Name = 2DSlice, index = 1 Name = TunnelWall, index = 2 Name = OutFlow, index = 3 Name = InFlow, index = 4 Name = Airfoil, index = 5 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = TunnelWall, index = 1 Name = OutFlow, index = 2 Name = InFlow, index = 3 Name = Airfoil, index = 4 Getting mesh sizing parameters Mesh sizing name - 2DSlice Mesh sizing name - Airfoil Mesh sizing name - InFlow Mesh sizing name - OutFlow Mesh sizing name - TunnelWall Done getting mesh sizing parameters Getting 2D mesh for body 1 (of 1) AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR2 IC : INPUT DATA CHECK AFLR2 IC : Nodes, Faces = 344 0 AFLR2 : CPU Time = 0.000 seconds AFLR2 EG : EDGE GRID RE-GENERATION AFLR2 EG : Nodes, Edges = 344 344 AFLR2 : CPU Time = 0.000 seconds AFLR2 IG : INITIAL GRID GENERATION AFLR2 IG : Nodes, Faces = 0 2 AFLR2 IG : Nodes, Faces = 70 142 AFLR2 IG : Nodes, Faces = 140 282 AFLR2 IG : Nodes, Faces = 210 422 AFLR2 IG : Nodes, Faces = 280 562 AFLR2 IG : Nodes, Faces = 316 634 AFLR2 IG : Nodes, Faces = 344 690 AFLR2 IG : Nodes, Faces = 348 690 AFLR2 IG : Nodes, Faces = 344 344 AFLR2 : CPU Time = 0.001 seconds AFLR2 GG : FIELD GRID GENERATION AFLR2 GGp: Nodes, Faces = 344 344 AFLR2 GGp: Nodes, Faces = 681 1018 AFLR2 GGp: Nodes, Faces = 1013 1682 AFLR2 GGp: Nodes, Faces = 1339 2334 AFLR2 GGp: Nodes, Faces = 1652 2960 AFLR2 GGp: Nodes, Faces = 1957 3570 AFLR2 GGp: Nodes, Faces = 2252 4160 AFLR2 GGp: Nodes, Faces = 2526 4708 AFLR2 GGp: Nodes, Faces = 2809 5274 AFLR2 GGp: Nodes, Faces = 3083 5822 AFLR2 GGp: Nodes, Faces = 3327 6310 AFLR2 GGp: Nodes, Faces = 3564 6784 AFLR2 GGp: Nodes, Faces = 3788 7232 AFLR2 GGp: Nodes, Faces = 3995 7646 AFLR2 GGp: Nodes, Faces = 4194 8044 AFLR2 GGp: Nodes, Faces = 4394 8444 AFLR2 GGp: Nodes, Faces = 4585 8826 AFLR2 GGp: Nodes, Faces = 4772 9200 AFLR2 GGp: Nodes, Faces = 4943 9542 AFLR2 GGp: Nodes, Faces = 5129 9914 AFLR2 GGp: Nodes, Faces = 5293 10242 AFLR2 GGp: Nodes, Faces = 5447 10550 AFLR2 GGp: Nodes, Faces = 5594 10844 AFLR2 GGp: Nodes, Faces = 5716 11088 AFLR2 GGp: Nodes, Faces = 5830 11316 AFLR2 GGp: Nodes, Faces = 5909 11474 AFLR2 GGp: Nodes, Faces = 5964 11584 AFLR2 GGp: Nodes, Faces = 6006 11668 AFLR2 GGp: Nodes, Faces = 6025 11706 AFLR2 GGp: Nodes, Faces = 6034 11724 AFLR2 : CPU Time = 0.030 seconds AFLR2 QI : QUALITY IMPROVEMENT AFLR2 QI : Nodes, Faces = 6034 11724 AFLR2 QI : Nodes, Faces = 6033 454 AFLR2 QI : Nodes, Faces = 6033 5634 AFLR2 QI : Nodes, Faces = 6033 11722 AFLR2 QI : Nodes, Faces = 6032 462 AFLR2 QI : Nodes, Faces = 6032 5629 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 456 AFLR2 QI : Nodes, Faces = 6032 5632 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6032 474 AFLR2 QI : Nodes, Faces = 6032 5623 AFLR2 QI : Nodes, Faces = 6032 11720 AFLR2 QI : Nodes, Faces = 6031 486 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 QI : Nodes, Faces = 6031 488 AFLR2 QI : Nodes, Faces = 6031 5616 AFLR2 : CPU Time = 0.010 seconds AFLR2 : DONE EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing AFLR3 file .... Finished writing AFLR3 file Number of nodes = 6031 Number of elements = 6448 Number of tris = 488 Number of quad = 5616 EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)! EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)! EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)! EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)! Writing Tecplot file .... Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh! Swapping z and y coordinates! Finished writing Tecplot file real 0m0.635s user 0m0.633s sys 0m0.301s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'aflr4_and_aflr3_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt aflr4_and_aflr3_PyTest.py test; + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM 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 Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR4 : Compile Date 04/23/24 @ 12:17PM 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 = 151604 Number of elements = 458324 Number of triangles = 14380 Number of quadrilatarals = 0 Number of tetrahedrals = 222892 Number of pyramids = 425 Number of prisms = 220627 Number of hexahedrals = 0 Writing Tecplot file .... Finished writing Tecplot file real 0m16.514s user 0m16.176s sys 0m0.442s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected) ================================================= ================================================= + echo 'tetgen_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt tetgen_PyTest.py test; + python -u tetgen_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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: 0.024089 Creating surface mesh ... Surface mesh seconds: 0.005679 Recovering boundaries... Boundary recovery seconds: 0.056391 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.008012 Suppressing Steiner points ... Steiner suppression seconds: 3.8e-05 Recovering Delaunayness... Delaunay recovery seconds: 0.010635 Refining mesh... 4190 insertions, added 2180 points, 134280 tetrahedra in queue. 1395 insertions, added 459 points, 138994 tetrahedra in queue. 1859 insertions, added 487 points, 137112 tetrahedra in queue. 2478 insertions, added 498 points, 120303 tetrahedra in queue. 3304 insertions, added 499 points, 74342 tetrahedra in queue. 4404 insertions, added 474 points, 460 tetrahedra in queue. Refinement seconds: 0.690902 Smoothing vertices... Mesh smoothing seconds: 0.438769 Improving mesh... Mesh improvement seconds: 0.01414 Jettisoning redundant points. Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002577 Total running seconds: 1.25144 Statistics: Input points: 3139 Input facets: 6266 Input segments: 9399 Input holes: 2 Input regions: 0 Mesh points: 8309 Mesh tetrahedra: 41161 Mesh faces: 85455 Mesh faces on exterior boundary: 6266 Mesh faces on input facets: 6266 Mesh edges on input segments: 9399 Steiner points inside domain: 5170 Done meshing using TetGen! Writing Tecplot file .... Finished writing Tecplot file real 0m2.622s user 0m2.678s sys 0m0.339s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected) ================================================= ================================================= + echo 'su2_and_AFLR2_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt su2_and_AFLR2_PyTest.py test; + python -u su2_and_AFLR2_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 Linux 3.10.0-1160.88.1.el7.x86_64 x86_64 AFLR2 : Compile Date 04/23/24 @ 12:17PM 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 = 0.050 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| 1.0250e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267| | 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0053e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028| | 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.8944e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910| | 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.7784e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695| | 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.6967e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976| | 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.6786e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542| | 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.6636e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759| | 0| 0| 7| 0.0000e+00| 0.0000e+00| 9.6125e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332| | 0| 0| 8| 0.0000e+00| 0.0000e+00| 9.5659e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216| | 0| 0| 9| 0.0000e+00| 0.0000e+00| 9.5390e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653| ----------------------------- Solver Exit ------------------------------- Maximum number of iterations reached (ITER = 10) before convergence. +-----------------------------------------------------------------------+ | Convergence Field | Value | Criterion | Converged | +-----------------------------------------------------------------------+ | rms[Rho]| -1.22124| < -14| No| +-----------------------------------------------------------------------+ ------------------------------------------------------------------------- +-----------------------------------------------------------------------+ | File Writing Summary | Filename | +-----------------------------------------------------------------------+ |SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |CSV file |surface_flow_pyCAPS_su2_aflr2.csv | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary |flow_pyCAPS_su2_aflr2.szplt | Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). |Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt| Error in tecFileWriterClose: Not all node map values for zone 1 have been written. Currently need 994 more values.0: Error finishing Tecplot file output. Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat). +-----------------------------------------------------------------------+ --------------------------- Finalizing Solver --------------------------- Deleted CNumerics container. Deleted CIntegration container. Deleted CSolver container. Deleted CIteration container. Deleted CInterface container. Deleted CGeometry container. Deleted CFreeFormDefBox class. Deleted CSurfaceMovement class. Deleted CVolumetricMovement class. Deleted CConfig container. Deleted nInst container. Deleted COutput class. ------------------------------------------------------------------------- ------------------------- Exit Success (SU2_CFD) ------------------------ Total Force - Pressure + Viscous Cl = 0.072253 Cd = -0.01151 Cmz = 0.070975 Cx = -0.01151 Cy = 0.072253 Pressure Contribution Cl_p = 0.072253 Cd_p = -0.01151 Cmz_p = 0.070975 Cx_p = -0.01151 Cy_p = 0.072253 Viscous Contribution Cl_v = 0.0 Cd_v = 0.0 Cmz_v = 0.0 Cx_v = 0.0 Cy_v = 0.0 real 0m2.198s user 0m2.077s sys 0m0.393s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected) ================================================= ================================================= + echo 'masstran_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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, -4.234505810751e-11] CG [1.222256036874, 0.1634981473778, -4.234637807833e-11] Ixx 22133.97306033 Iyy 23448.30046709 Izz 1389.213122582 Ixy 164.2055275657 Ixz -7.45484669011e-06 Iyz 1.707686795832e-06 I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06] II [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]] real 0m4.507s user 0m6.177s sys 0m0.878s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected) ================================================= ================================================= + echo 'hsm_SingleLoadCase_PyTest.py test;' + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + python -u hsm_SingleLoadCase_PyTest.py -outLevel=0 + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 81 Number of elements = 96 Elemental Tria3 = 0 Elemental Quad4 = 64 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 32 ->HSMSOL Matrix Non-zero Entries = 5741 Converging HSM equation system ... iter dr dd dp rlx max 1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00) 1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00) 2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00) 2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00) 4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00) 5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00) 6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00) 7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00) Converging n vectors ... it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 ) it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 ) Converging e1,e2 vectors ... it = 1 de = 0.691E-03 rlx = 1.000 ( 45 ) it = 2 de = 0.404E-04 rlx = 1.000 ( 9 ) it = 3 de = 0.142E-07 rlx = 1.000 ( 46 ) it = 4 de = 0.521E-11 rlx = 1.000 ( 62 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat real 0m0.934s user 0m0.844s sys 0m0.195s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + echo '../corsairlite/qp.py test;' ../corsairlite/qp.py test; + tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt + python -u ../corsairlite/qp.py -outLevel=0 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 0m2.202s user 0m2.226s sys 0m0.400s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: abaqus awave Cart3D Astros Mystran ================================================= All tests pass! + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64 + mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs + cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs + find /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs -name 'plugs0*.csm' find: ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs’: No such file or directory + sort -f + awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsFailure.txt + cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsIgnore.txt . + set +x Testing CSM files: total 28M -rw-rw-r-- 1 jenkins jenkins 1.3M Apr 28 10:21 ASTRO.D01 -rw-rw-r-- 1 jenkins jenkins 316K Apr 28 10:21 ASTRO.IDX -rwxrwxr-x 1 jenkins jenkins 1.1M Apr 28 10:21 avl -rwxrwxr-x 1 jenkins jenkins 33K Apr 28 10:19 egads2cart -rwxrwxr-x 1 jenkins jenkins 137K Apr 28 10:21 egads2cgt -rwxrwxr-x 1 jenkins jenkins 317K Apr 28 10:21 friction -rwxrwxr-x 1 jenkins jenkins 8.2M Apr 28 10:21 mastros.exe -rwxrwxr-x 1 jenkins jenkins 727K Apr 28 10:21 mses -rwxrwxr-x 1 jenkins jenkins 536K Apr 28 10:21 mset -rwxrwxr-x 1 jenkins jenkins 52K Apr 28 10:21 phaseUtil -rw-rw-r-- 1 jenkins jenkins 1.6K Apr 28 10:23 pod.egads -rw-rw-r-- 1 jenkins jenkins 0 Apr 28 10:23 port7681.jrnl -rwxrwxr-x 1 jenkins jenkins 451K Apr 28 10:21 pplot -rwxrwxr-x 1 jenkins jenkins 405K Apr 28 10:21 pxplot -rwxrwxr-x 1 jenkins jenkins 147K Apr 28 10:20 sensCSM -rwxrwxr-x 1 jenkins jenkins 685K Apr 28 10:20 serveCSM -rwxrwxr-x 1 jenkins jenkins 599K Apr 28 10:20 serveESP -rwxrwxr-x 1 jenkins jenkins 711K Apr 28 10:21 Slugs -rwxrwxr-x 1 jenkins jenkins 187K Apr 28 10:21 TestFit -rwxrwxr-x 1 jenkins jenkins 71K Apr 28 10:19 vCurvature -rwxrwxr-x 1 jenkins jenkins 45K Apr 28 10:19 vGeom -rwxrwxr-x 1 jenkins jenkins 71K Apr 28 10:19 vTess -rwxrwxr-x 1 jenkins jenkins 11M Apr 28 10:19 vTesstatic -rw-rw-r-- 1 jenkins jenkins 195K Apr 28 10:23 wingMultiModel.bdf -rwxrwxr-x 1 jenkins jenkins 1.1M Apr 28 10:21 xfoil [Execution node] check if [reynolds-ubuntu18] is in [[viggen]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [reynolds-ubuntu18] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64') [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: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64') [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: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64') [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: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64') [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=LINUX64,buildnode=reynolds-ubuntu18 #711'. [Checks API] No suitable checks publisher found. [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Deferred wipeout is used... [WS-CLEANUP] done Finished: SUCCESS