Started by upstream project "ESP_Beta" build number 716
originally caused by:
Started by user galbramc
Running as galbramc
[EnvInject] - Loading node environment variables.
Building remotely on macys_VM in workspace /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-16T19:53:04.016 -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 2495
Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-16T19:53:04.016 -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 861
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [macys_VM] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[DARWIN64] $ /bin/bash -ex /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jenkins17525082069956409802.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Beta.sh
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ macys_VM == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]]
+++ . /usr/local/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ macys_VM == \m\a\c\y\s* ]]
++ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/intercept-*'
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ ln -s /usr/local/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python
++ ln -s /usr/local/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python-config
++ ln -s /usr/local/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/virtualenv
+++ python-config --includes
++ export 'PYTHONINC=. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11'
++ PYTHONINC='. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11'
+++ python-config --help
++ [[ Usage: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB=-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation'
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.5
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/data
+ virtualenv /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv
created virtual environment CPython3.11.5.final.0-64 in 2209ms
creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv)
added seed packages: pip==24.0, setuptools==69.5.1, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/activate
++ '[' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv
++ '[' darwin20 = cygwin ']'
++ '[' darwin20 = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl.metadata (61 kB)
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl (20.6 MB)
Installing collected packages: numpy
Successfully installed numpy-1.26.4
+ pip_install openmdao
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.32.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Requirement already satisfied: numpy<2 in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4)
Collecting packaging (from openmdao)
Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB)
Collecting requests (from openmdao)
Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB)
Collecting scipy (from openmdao)
Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached packaging-24.0-py3-none-any.whl (53 kB)
Using cached requests-2.31.0-py3-none-any.whl (62 kB)
Using cached scipy-1.13.0-cp311-cp311-macosx_10_9_x86_64.whl (39.3 MB)
Using cached certifi-2024.2.2-py3-none-any.whl (163 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl (121 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.1-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao
Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.32.0 packaging-24.0 requests-2.31.0 scipy-1.13.0 urllib3-2.2.1
+ [[ macys_VM == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl (13.8 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install matplotlib
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.9.0-cp311-cp311-macosx_10_12_x86_64.whl.metadata (11 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (159 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.23 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.0)
Collecting pillow>=8 (from matplotlib)
Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.9.0-cp311-cp311-macosx_10_12_x86_64.whl (7.9 MB)
Using cached contourpy-1.2.1-cp311-cp311-macosx_10_9_x86_64.whl (262 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_x86_64.whl (2.3 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl (68 kB)
Using cached pillow-10.3.0-cp311-cp311-macosx_10_10_x86_64.whl (3.5 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.0)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-05-16 19:55:03-- https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 272107101 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
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5100K .......... .......... .......... .......... .......... 1% 38.8M 20s
5150K .......... .......... .......... .......... .......... 1% 89.1M 20s
5200K .......... .......... .......... .......... .......... 1% 113M 20s
5250K .......... .......... .......... .......... .......... 1% 1.56M 21s
5300K .......... .......... .......... .......... .......... 2% 59.8M 21s
5350K .......... .......... .......... .......... .......... 2% 5.44M 21s
5400K .......... .......... .......... .......... .......... 2% 48.4M 21s
5450K .......... .......... .......... .......... .......... 2% 72.2M 21s
5500K .......... .......... .......... .......... .......... 2% 79.8M 21s
5550K .......... .......... .......... .......... .......... 2% 84.6M 21s
5600K .......... .......... .......... .......... .......... 2% 108M 20s
5650K .......... .......... .......... .......... .......... 2% 141M 20s
5700K .......... .......... .......... .......... .......... 2% 115M 20s
5750K .......... .......... .......... .......... .......... 2% 131M 20s
5800K .......... .......... .......... .......... .......... 2% 70.1M 20s
5850K .......... .......... .......... .......... .......... 2% 99.2M 20s
5900K .......... .......... .......... .......... .......... 2% 4.70M 20s
5950K .......... .......... .......... .......... .......... 2% 48.7M 20s
6000K .......... .......... .......... .......... .......... 2% 134M 20s
6050K .......... .......... .......... .......... .......... 2% 39.3M 20s
6100K .......... .......... .......... .......... .......... 2% 110M 19s
6150K .......... .......... .......... .......... .......... 2% 107M 19s
6200K .......... .......... .......... .......... .......... 2% 68.5M 19s
6250K .......... .......... .......... .......... .......... 2% 122M 19s
6300K .......... .......... .......... .......... .......... 2% 157M 19s
6350K .......... .......... .......... .......... .......... 2% 129M 19s
6400K .......... .......... .......... .......... .......... 2% 149M 19s
6450K .......... .......... .......... .......... .......... 2% 133M 18s
6500K .......... .......... .......... .......... .......... 2% 153M 18s
6550K .......... .......... .......... .......... .......... 2% 154M 18s
6600K .......... .......... .......... .......... .......... 2% 132M 18s
6650K .......... .......... .......... .......... .......... 2% 159M 18s
6700K .......... .......... .......... .......... .......... 2% 136M 18s
6750K .......... .......... .......... .......... .......... 2% 159M 18s
6800K .......... .......... .......... .......... .......... 2% 160M 18s
6850K .......... .......... .......... .......... .......... 2% 132M 17s
6900K .......... .......... .......... .......... .......... 2% 151M 17s
6950K .......... .......... .......... .......... .......... 2% 135M 17s
7000K .......... .......... .......... .......... .......... 2% 74.5M 17s
7050K .......... .......... .......... .......... .......... 2% 112M 17s
7100K .......... .......... .......... .......... .......... 2% 72.2M 17s
7150K .......... .......... .......... .......... .......... 2% 126M 17s
7200K .......... .......... .......... .......... .......... 2% 32.4M 17s
7250K .......... .......... .......... .......... .......... 2% 117M 17s
7300K .......... .......... .......... .......... .......... 2% 135M 17s
7350K .......... .......... .......... .......... .......... 2% 109M 16s
7400K .......... .......... .......... .......... .......... 2% 124M 16s
7450K .......... .......... .......... .......... .......... 2% 119M 16s
7500K .......... .......... .......... .......... .......... 2% 124M 16s
7550K .......... .......... .......... .......... .......... 2% 126M 16s
7600K .......... .......... .......... .......... .......... 2% 109M 16s
7650K .......... .......... .......... .......... .......... 2% 130M 16s
7700K .......... .......... .......... .......... .......... 2% 109M 16s
7750K .......... .......... .......... .......... .......... 2% 123M 16s
7800K .......... .......... .......... .......... .......... 2% 129M 16s
7850K .......... .......... .......... .......... .......... 2% 108M 16s
7900K .......... .......... .......... .......... .......... 2% 132M 15s
7950K .......... .......... .......... .......... .......... 3% 120M 15s
8000K .......... .......... .......... .......... .......... 3% 133M 15s
8050K .......... .......... .......... .......... .......... 3% 132M 15s
8100K .......... .......... .......... .......... .......... 3% 118M 15s
8150K .......... .......... .......... .......... .......... 3% 3.61M 15s
8200K .......... .......... .......... .......... .......... 3% 1.15M 17s
8250K .......... .......... .......... .......... .......... 3% 19.0M 17s
8300K .......... .......... .......... .......... .......... 3% 136M 17s
8350K .......... .......... .......... .......... .......... 3% 114M 16s
8400K .......... .......... .......... .......... .......... 3% 93.0M 16s
8450K .......... .......... .......... .......... .......... 3% 4.63M 17s
8500K .......... .......... .......... .......... .......... 3% 142M 16s
8550K .......... .......... .......... .......... .......... 3% 142M 16s
8600K .......... .......... .......... .......... .......... 3% 24.5M 16s
8650K .......... .......... .......... .......... .......... 3% 53.5M 16s
8700K .......... .......... .......... .......... .......... 3% 3.25M 17s
8750K .......... .......... .......... .......... .......... 3% 25.1M 17s
8800K .......... .......... .......... .......... .......... 3% 23.3M 17s
8850K .......... .......... .......... .......... .......... 3% 25.4M 17s
8900K .......... .......... .......... .......... .......... 3% 13.9M 17s
8950K .......... .......... .......... .......... .......... 3% 28.5M 16s
9000K .......... .......... .......... .......... .......... 3% 20.6M 16s
9050K .......... .......... .......... .......... .......... 3% 17.3M 16s
9100K .......... .......... .......... .......... .......... 3% 27.5M 16s
9150K .......... .......... .......... .......... .......... 3% 32.3M 16s
9200K .......... .......... .......... .......... .......... 3% 9.84M 16s
9250K .......... .......... .......... .......... .......... 3% 13.0M 16s
9300K .......... .......... .......... .......... .......... 3% 21.4M 16s
9350K .......... .......... .......... .......... .......... 3% 13.8M 16s
9400K .......... .......... .......... .......... .......... 3% 1006K 18s
9450K .......... .......... .......... .......... .......... 3% 38.9M 18s
9500K .......... .......... .......... .......... .......... 3% 24.7M 18s
9550K .......... .......... .......... .......... .......... 3% 14.9M 18s
9600K .......... .......... .......... .......... .......... 3% 9.83M 18s
9650K .......... .......... .......... .......... .......... 3% 11.0M 18s
9700K .......... .......... .......... .......... .......... 3% 8.68M 18s
9750K .......... .......... .......... .......... .......... 3% 10.3M 18s
9800K .......... .......... .......... .......... .......... 3% 18.3M 18s
9850K .......... .......... .......... .......... .......... 3% 31.6M 18s
9900K .......... .......... .......... .......... .......... 3% 81.1M 18s
9950K .......... .......... .......... .......... .......... 3% 70.6M 17s
10000K .......... .......... .......... .......... .......... 3% 89.8M 17s
10050K .......... .......... .......... .......... .......... 3% 75.4M 17s
10100K .......... .......... .......... .......... .......... 3% 78.6M 17s
10150K .......... .......... .......... .......... .......... 3% 111M 17s
10200K .......... .......... .......... .......... .......... 3% 5.62M 17s
10250K .......... .......... .......... .......... .......... 3% 50.8M 17s
10300K .......... .......... .......... .......... .......... 3% 53.0M 17s
10350K .......... .......... .......... .......... .......... 3% 52.4M 17s
10400K .......... .......... .......... .......... .......... 3% 85.8M 17s
10450K .......... .......... .......... .......... .......... 3% 111M 17s
10500K .......... .......... .......... .......... .......... 3% 128M 17s
10550K .......... .......... .......... .......... .......... 3% 65.7M 17s
10600K .......... .......... .......... .......... .......... 4% 84.5M 17s
10650K .......... .......... .......... .......... .......... 4% 139M 17s
10700K .......... .......... .......... .......... .......... 4% 122M 17s
10750K .......... .......... .......... .......... .......... 4% 81.1M 17s
10800K .......... .......... .......... .......... .......... 4% 146M 16s
10850K .......... .......... .......... .......... .......... 4% 123M 16s
10900K .......... .......... .......... .......... .......... 4% 142M 16s
10950K .......... .......... .......... .......... .......... 4% 130M 16s
11000K .......... .......... .......... .......... .......... 4% 144M 16s
11050K .......... .......... .......... .......... .......... 4% 108M 16s
11100K .......... .......... .......... .......... .......... 4% 12.2M 16s
11150K .......... .......... .......... .......... .......... 4% 147M 16s
11200K .......... .......... .......... .......... .......... 4% 127M 16s
11250K .......... .......... .......... .......... .......... 4% 7.56M 16s
11300K .......... .......... .......... .......... .......... 4% 151M 16s
11350K .......... .......... .......... .......... .......... 4% 125M 16s
11400K .......... .......... .......... .......... .......... 4% 84.6M 16s
11450K .......... .......... .......... .......... .......... 4% 71.6M 16s
11500K .......... .......... .......... .......... .......... 4% 69.1M 16s
11550K .......... .......... .......... .......... .......... 4% 126M 16s
11600K .......... .......... .......... .......... .......... 4% 48.2M 16s
11650K .......... .......... .......... .......... .......... 4% 65.9M 16s
11700K .......... .......... .......... .......... .......... 4% 33.5M 16s
11750K .......... .......... .......... .......... .......... 4% 51.1M 16s
11800K .......... .......... .......... .......... .......... 4% 81.7M 15s
11850K .......... .......... .......... .......... .......... 4% 83.0M 15s
11900K .......... .......... .......... .......... .......... 4% 41.0M 15s
11950K .......... .......... .......... .......... .......... 4% 84.0M 15s
12000K .......... .......... .......... .......... .......... 4% 64.9M 15s
12050K .......... .......... .......... .......... .......... 4% 66.8M 15s
12100K .......... .......... .......... .......... .......... 4% 84.5M 15s
12150K .......... .......... .......... .......... .......... 4% 64.7M 15s
12200K .......... .......... .......... .......... .......... 4% 64.4M 15s
12250K .......... .......... .......... .......... .......... 4% 11.5M 15s
12300K .......... .......... .......... .......... .......... 4% 105M 15s
12350K .......... .......... .......... .......... .......... 4% 110M 15s
12400K .......... .......... .......... .......... .......... 4% 28.0M 15s
12450K .......... .......... .......... .......... .......... 4% 106M 15s
12500K .......... .......... .......... .......... .......... 4% 118M 15s
12550K .......... .......... .......... .......... .......... 4% 140M 15s
12600K .......... .......... .......... .......... .......... 4% 121M 15s
12650K .......... .......... .......... .......... .......... 4% 152M 15s
12700K .......... .......... .......... .......... .......... 4% 135M 15s
12750K .......... .......... .......... .......... .......... 4% 133M 15s
12800K .......... .......... .......... .......... .......... 4% 148M 15s
12850K .......... .......... .......... .......... .......... 4% 125M 14s
12900K .......... .......... .......... .......... .......... 4% 151M 14s
12950K .......... .......... .......... .......... .......... 4% 133M 14s
13000K .......... .......... .......... .......... .......... 4% 152M 14s
13050K .......... .......... .......... .......... .......... 4% 132M 14s
13100K .......... .......... .......... .......... .......... 4% 129M 14s
13150K .......... .......... .......... .......... .......... 4% 127M 14s
13200K .......... .......... .......... .......... .......... 4% 103M 14s
13250K .......... .......... .......... .......... .......... 5% 124M 14s
13300K .......... .......... .......... .......... .......... 5% 3.22M 14s
13350K .......... .......... .......... .......... .......... 5% 57.6M 14s
13400K .......... .......... .......... .......... .......... 5% 99.6M 14s
13450K .......... .......... .......... .......... .......... 5% 113M 14s
13500K .......... .......... .......... .......... .......... 5% 134M 14s
13550K .......... .......... .......... .......... .......... 5% 63.2M 14s
13600K .......... .......... .......... .......... .......... 5% 84.2M 14s
13650K .......... .......... .......... .......... .......... 5% 98.2M 14s
13700K .......... .......... .......... .......... .......... 5% 74.3M 14s
13750K .......... .......... .......... .......... .......... 5% 98.8M 14s
13800K .......... .......... .......... .......... .......... 5% 114M 14s
13850K .......... .......... .......... .......... .......... 5% 54.3M 14s
13900K .......... .......... .......... .......... .......... 5% 80.7M 14s
13950K .......... .......... .......... .......... .......... 5% 71.1M 14s
14000K .......... .......... .......... .......... .......... 5% 74.4M 14s
14050K .......... .......... .......... .......... .......... 5% 72.0M 14s
14100K .......... .......... .......... .......... .......... 5% 73.9M 14s
14150K .......... .......... .......... .......... .......... 5% 115M 14s
14200K .......... .......... .......... .......... .......... 5% 67.4M 14s
14250K .......... .......... .......... .......... .......... 5% 107M 13s
14300K .......... .......... .......... .......... .......... 5% 695K 15s
14350K .......... .......... .......... .......... .......... 5% 53.8M 15s
14400K .......... .......... .......... .......... .......... 5% 107M 15s
14450K .......... .......... .......... .......... .......... 5% 108M 15s
14500K .......... .......... .......... .......... .......... 5% 135M 15s
14550K .......... .......... .......... .......... .......... 5% 121M 14s
14600K .......... .......... .......... .......... .......... 5% 43.7M 14s
14650K .......... .......... .......... .......... .......... 5% 62.8M 14s
14700K .......... .......... .......... .......... .......... 5% 77.9M 14s
14750K .......... .......... .......... .......... .......... 5% 141M 14s
14800K .......... .......... .......... .......... .......... 5% 132M 14s
14850K .......... .......... .......... .......... .......... 5% 112M 14s
14900K .......... .......... .......... .......... .......... 5% 57.4M 14s
14950K .......... .......... .......... .......... .......... 5% 113M 14s
15000K .......... .......... .......... .......... .......... 5% 136M 14s
15050K .......... .......... .......... .......... .......... 5% 131M 14s
15100K .......... .......... .......... .......... .......... 5% 88.9M 14s
15150K .......... .......... .......... .......... .......... 5% 117M 14s
15200K .......... .......... .......... .......... .......... 5% 83.3M 14s
15250K .......... .......... .......... .......... .......... 5% 131M 14s
15300K .......... .......... .......... .......... .......... 5% 114M 14s
15350K .......... .......... .......... .......... .......... 5% 77.1M 14s
15400K .......... .......... .......... .......... .......... 5% 142M 14s
15450K .......... .......... .......... .......... .......... 5% 131M 14s
15500K .......... .......... .......... .......... .......... 5% 148M 14s
15550K .......... .......... .......... .......... .......... 5% 149M 14s
15600K .......... .......... .......... .......... .......... 5% 128M 14s
15650K .......... .......... .......... .......... .......... 5% 148M 14s
15700K .......... .......... .......... .......... .......... 5% 127M 14s
15750K .......... .......... .......... .......... .......... 5% 122M 13s
15800K .......... .......... .......... .......... .......... 5% 139M 13s
15850K .......... .......... .......... .......... .......... 5% 124M 13s
15900K .......... .......... .......... .......... .......... 6% 135M 13s
15950K .......... .......... .......... .......... .......... 6% 122M 13s
16000K .......... .......... .......... .......... .......... 6% 133M 13s
16050K .......... .......... .......... .......... .......... 6% 133M 13s
16100K .......... .......... .......... .......... .......... 6% 72.6M 13s
16150K .......... .......... .......... .......... .......... 6% 52.4M 13s
16200K .......... .......... .......... .......... .......... 6% 118M 13s
16250K .......... .......... .......... .......... .......... 6% 97.9M 13s
16300K .......... .......... .......... .......... .......... 6% 52.7M 13s
16350K .......... .......... .......... .......... .......... 6% 52.9M 13s
16400K .......... .......... .......... .......... .......... 6% 133M 13s
16450K .......... .......... .......... .......... .......... 6% 116M 13s
16500K .......... .......... .......... .......... .......... 6% 88.3M 13s
16550K .......... .......... .......... .......... .......... 6% 118M 13s
16600K .......... .......... .......... .......... .......... 6% 104M 13s
16650K .......... .......... .......... .......... .......... 6% 123M 13s
16700K .......... .......... .......... .......... .......... 6% 105M 13s
16750K .......... .......... .......... .......... .......... 6% 122M 13s
16800K .......... .......... .......... .......... .......... 6% 124M 13s
16850K .......... .......... .......... .......... .......... 6% 105M 13s
16900K .......... .......... .......... .......... .......... 6% 120M 13s
16950K .......... .......... .......... .......... .......... 6% 3.55M 13s
17000K .......... .......... .......... .......... .......... 6% 100M 13s
17050K .......... .......... .......... .......... .......... 6% 75.0M 13s
17100K .......... .......... .......... .......... .......... 6% 103M 13s
17150K .......... .......... .......... .......... .......... 6% 129M 13s
17200K .......... .......... .......... .......... .......... 6% 122M 13s
17250K .......... .......... .......... .......... .......... 6% 145M 13s
17300K .......... .......... .......... .......... .......... 6% 135M 13s
17350K .......... .......... .......... .......... .......... 6% 121M 13s
17400K .......... .......... .......... .......... .......... 6% 7.36M 13s
17450K .......... .......... .......... .......... .......... 6% 63.0M 13s
17500K .......... .......... .......... .......... .......... 6% 126M 13s
17550K .......... .......... .......... .......... .......... 6% 30.5M 13s
17600K .......... .......... .......... .......... .......... 6% 64.8M 13s
17650K .......... .......... .......... .......... .......... 6% 80.3M 13s
17700K .......... .......... .......... .......... .......... 6% 76.1M 12s
17750K .......... .......... .......... .......... .......... 6% 80.7M 12s
17800K .......... .......... .......... .......... .......... 6% 72.3M 12s
17850K .......... .......... .......... .......... .......... 6% 74.2M 12s
17900K .......... .......... .......... .......... .......... 6% 112M 12s
17950K .......... .......... .......... .......... .......... 6% 93.7M 12s
18000K .......... .......... .......... .......... .......... 6% 110M 12s
18050K .......... .......... .......... .......... .......... 6% 79.4M 12s
18100K .......... .......... .......... .......... .......... 6% 122M 12s
18150K .......... .......... .......... .......... .......... 6% 130M 12s
18200K .......... .......... .......... .......... .......... 6% 70.0M 12s
18250K .......... .......... .......... .......... .......... 6% 79.5M 12s
18300K .......... .......... .......... .......... .......... 6% 66.6M 12s
18350K .......... .......... .......... .......... .......... 6% 2.45M 12s
18400K .......... .......... .......... .......... .......... 6% 9.05M 12s
18450K .......... .......... .......... .......... .......... 6% 40.4M 12s
18500K .......... .......... .......... .......... .......... 6% 66.9M 12s
18550K .......... .......... .......... .......... .......... 6% 116M 12s
18600K .......... .......... .......... .......... .......... 7% 117M 12s
18650K .......... .......... .......... .......... .......... 7% 138M 12s
18700K .......... .......... .......... .......... .......... 7% 121M 12s
18750K .......... .......... .......... .......... .......... 7% 139M 12s
18800K .......... .......... .......... .......... .......... 7% 144M 12s
18850K .......... .......... .......... .......... .......... 7% 121M 12s
18900K .......... .......... .......... .......... .......... 7% 131M 12s
18950K .......... .......... .......... .......... .......... 7% 117M 12s
19000K .......... .......... .......... .......... .......... 7% 127M 12s
19050K .......... .......... .......... .......... .......... 7% 127M 12s
19100K .......... .......... .......... .......... .......... 7% 120M 12s
19150K .......... .......... .......... .......... .......... 7% 140M 12s
19200K .......... .......... .......... .......... .......... 7% 126M 12s
19250K .......... .......... .......... .......... .......... 7% 145M 12s
19300K .......... .......... .......... .......... .......... 7% 149M 12s
19350K .......... .......... .......... .......... .......... 7% 3.17M 12s
19400K .......... .......... .......... .......... .......... 7% 139M 12s
19450K .......... .......... .......... .......... .......... 7% 47.0M 12s
19500K .......... .......... .......... .......... .......... 7% 80.7M 12s
19550K .......... .......... .......... .......... .......... 7% 144M 12s
19600K .......... .......... .......... .......... .......... 7% 51.9M 12s
19650K .......... .......... .......... .......... .......... 7% 15.2M 12s
19700K .......... .......... .......... .......... .......... 7% 123M 12s
19750K .......... .......... .......... .......... .......... 7% 133M 12s
19800K .......... .......... .......... .......... .......... 7% 148M 12s
19850K .......... .......... .......... .......... .......... 7% 123M 12s
19900K .......... .......... .......... .......... .......... 7% 128M 12s
19950K .......... .......... .......... .......... .......... 7% 121M 12s
20000K .......... .......... .......... .......... .......... 7% 137M 12s
20050K .......... .......... .......... .......... .......... 7% 124M 12s
20100K .......... .......... .......... .......... .......... 7% 96.7M 12s
20150K .......... .......... .......... .......... .......... 7% 136M 12s
20200K .......... .......... .......... .......... .......... 7% 112M 12s
20250K .......... .......... .......... .......... .......... 7% 126M 12s
20300K .......... .......... .......... .......... .......... 7% 151M 12s
20350K .......... .......... .......... .......... .......... 7% 104M 12s
20400K .......... .......... .......... .......... .......... 7% 126M 12s
20450K .......... .......... .......... .......... .......... 7% 547K 13s
20500K .......... .......... .......... .......... .......... 7% 195M 13s
20550K .......... .......... .......... .......... .......... 7% 225M 13s
20600K .......... .......... .......... .......... .......... 7% 183M 12s
20650K .......... .......... .......... .......... .......... 7% 220M 12s
20700K .......... .......... .......... .......... .......... 7% 198M 12s
20750K .......... .......... .......... .......... .......... 7% 197M 12s
20800K .......... .......... .......... .......... .......... 7% 203M 12s
20850K .......... .......... .......... .......... .......... 7% 186M 12s
20900K .......... .......... .......... .......... .......... 7% 174M 12s
20950K .......... .......... .......... .......... .......... 7% 179M 12s
21000K .......... .......... .......... .......... .......... 7% 214M 12s
21050K .......... .......... .......... .......... .......... 7% 204M 12s
21100K .......... .......... .......... .......... .......... 7% 174M 12s
21150K .......... .......... .......... .......... .......... 7% 98.4M 12s
21200K .......... .......... .......... .......... .......... 7% 124M 12s
21250K .......... .......... .......... .......... .......... 8% 103M 12s
21300K .......... .......... .......... .......... .......... 8% 165M 12s
21350K .......... .......... .......... .......... .......... 8% 54.4M 12s
21400K .......... .......... .......... .......... .......... 8% 220M 12s
21450K .......... .......... .......... .......... .......... 8% 180M 12s
21500K .......... .......... .......... .......... .......... 8% 4.89M 12s
21550K .......... .......... .......... .......... .......... 8% 77.6M 12s
21600K .......... .......... .......... .......... .......... 8% 116M 12s
21650K .......... .......... .......... .......... .......... 8% 176M 12s
21700K .......... .......... .......... .......... .......... 8% 132M 12s
21750K .......... .......... .......... .......... .......... 8% 150M 12s
21800K .......... .......... .......... .......... .......... 8% 148M 12s
21850K .......... .......... .......... .......... .......... 8% 128M 12s
21900K .......... .......... .......... .......... .......... 8% 160M 12s
21950K .......... .......... .......... .......... .......... 8% 144M 12s
22000K .......... .......... .......... .......... .......... 8% 179M 12s
22050K .......... .......... .......... .......... .......... 8% 213M 12s
22100K .......... .......... .......... .......... .......... 8% 189M 12s
22150K .......... .......... .......... .......... .......... 8% 217M 12s
22200K .......... .......... .......... .......... .......... 8% 191M 12s
22250K .......... .......... .......... .......... .......... 8% 139M 12s
22300K .......... .......... .......... .......... .......... 8% 129M 12s
22350K .......... .......... .......... .......... .......... 8% 110M 12s
22400K .......... .......... .......... .......... .......... 8% 136M 12s
22450K .......... .......... .......... .......... .......... 8% 135M 12s
22500K .......... .......... .......... .......... .......... 8% 2.52M 12s
22550K .......... .......... .......... .......... .......... 8% 35.0M 12s
22600K .......... .......... .......... .......... .......... 8% 103M 12s
22650K .......... .......... .......... .......... .......... 8% 164M 12s
22700K .......... .......... .......... .......... .......... 8% 12.3M 12s
22750K .......... .......... .......... .......... .......... 8% 128M 12s
22800K .......... .......... .......... .......... .......... 8% 126M 12s
22850K .......... .......... .......... .......... .......... 8% 37.2M 12s
22900K .......... .......... .......... .......... .......... 8% 16.3M 12s
22950K .......... .......... .......... .......... .......... 8% 9.64M 12s
23000K .......... .......... .......... .......... .......... 8% 13.6M 12s
23050K .......... .......... .......... .......... .......... 8% 15.0M 12s
23100K .......... .......... .......... .......... .......... 8% 2.22M 12s
23150K .......... .......... .......... .......... .......... 8% 132M 12s
23200K .......... .......... .......... .......... .......... 8% 20.6M 12s
23250K .......... .......... .......... .......... .......... 8% 43.5M 12s
23300K .......... .......... .......... .......... .......... 8% 203M 12s
23350K .......... .......... .......... .......... .......... 8% 197M 12s
23400K .......... .......... .......... .......... .......... 8% 212M 12s
23450K .......... .......... .......... .......... .......... 8% 182M 12s
23500K .......... .......... .......... .......... .......... 8% 101M 12s
23550K .......... .......... .......... .......... .......... 8% 18.6M 12s
23600K .......... .......... .......... .......... .......... 8% 7.85M 12s
23650K .......... .......... .......... .......... .......... 8% 12.3M 12s
23700K .......... .......... .......... .......... .......... 8% 10.8M 12s
23750K .......... .......... .......... .......... .......... 8% 9.34M 12s
23800K .......... .......... .......... .......... .......... 8% 21.5M 12s
23850K .......... .......... .......... .......... .......... 8% 159M 12s
23900K .......... .......... .......... .......... .......... 9% 61.0M 12s
23950K .......... .......... .......... .......... .......... 9% 124M 12s
24000K .......... .......... .......... .......... .......... 9% 138M 12s
24050K .......... .......... .......... .......... .......... 9% 163M 12s
24100K .......... .......... .......... .......... .......... 9% 97.1M 12s
24150K .......... .......... .......... .......... .......... 9% 2.61M 12s
24200K .......... .......... .......... .......... .......... 9% 6.52M 12s
24250K .......... .......... .......... .......... .......... 9% 10.7M 12s
24300K .......... .......... .......... .......... .......... 9% 66.3M 12s
24350K .......... .......... .......... .......... .......... 9% 104M 12s
24400K .......... .......... .......... .......... .......... 9% 64.3M 12s
24450K .......... .......... .......... .......... .......... 9% 29.1M 12s
24500K .......... .......... .......... .......... .......... 9% 16.0M 12s
24550K .......... .......... .......... .......... .......... 9% 12.5M 12s
24600K .......... .......... .......... .......... .......... 9% 115M 12s
24650K .......... .......... .......... .......... .......... 9% 45.9M 12s
24700K .......... .......... .......... .......... .......... 9% 34.8M 12s
24750K .......... .......... .......... .......... .......... 9% 22.4M 12s
24800K .......... .......... .......... .......... .......... 9% 111M 12s
24850K .......... .......... .......... .......... .......... 9% 29.0M 12s
24900K .......... .......... .......... .......... .......... 9% 173M 12s
24950K .......... .......... .......... .......... .......... 9% 130M 12s
25000K .......... .......... .......... .......... .......... 9% 148M 12s
25050K .......... .......... .......... .......... .......... 9% 146M 12s
25100K .......... .......... .......... .......... .......... 9% 93.0M 12s
25150K .......... .......... .......... .......... .......... 9% 216M 12s
25200K .......... .......... .......... .......... .......... 9% 204M 12s
25250K .......... .......... .......... .......... .......... 9% 234M 12s
25300K .......... .......... .......... .......... .......... 9% 234M 12s
25350K .......... .......... .......... .......... .......... 9% 204M 12s
25400K .......... .......... .......... .......... .......... 9% 236M 12s
25450K .......... .......... .......... .......... .......... 9% 207M 12s
25500K .......... .......... .......... .......... .......... 9% 236M 12s
25550K .......... .......... .......... .......... .......... 9% 233M 11s
25600K .......... .......... .......... .......... .......... 9% 24.3M 11s
25650K .......... .......... .......... .......... .......... 9% 167M 11s
25700K .......... .......... .......... .......... .......... 9% 96.9M 11s
25750K .......... .......... .......... .......... .......... 9% 198M 11s
25800K .......... .......... .......... .......... .......... 9% 205M 11s
25850K .......... .......... .......... .......... .......... 9% 113M 11s
25900K .......... .......... .......... .......... .......... 9% 208M 11s
25950K .......... .......... .......... .......... .......... 9% 185M 11s
26000K .......... .......... .......... .......... .......... 9% 213M 11s
26050K .......... .......... .......... .......... .......... 9% 203M 11s
26100K .......... .......... .......... .......... .......... 9% 184M 11s
26150K .......... .......... .......... .......... .......... 9% 214M 11s
26200K .......... .......... .......... .......... .......... 9% 186M 11s
26250K .......... .......... .......... .......... .......... 9% 219M 11s
26300K .......... .......... .......... .......... .......... 9% 208M 11s
26350K .......... .......... .......... .......... .......... 9% 180M 11s
26400K .......... .......... .......... .......... .......... 9% 230M 11s
26450K .......... .......... .......... .......... .......... 9% 198M 11s
26500K .......... .......... .......... .......... .......... 9% 227M 11s
26550K .......... .......... .......... .......... .......... 10% 223M 11s
26600K .......... .......... .......... .......... .......... 10% 2.53M 11s
26650K .......... .......... .......... .......... .......... 10% 74.0M 11s
26700K .......... .......... .......... .......... .......... 10% 99.6M 11s
26750K .......... .......... .......... .......... .......... 10% 186M 11s
26800K .......... .......... .......... .......... .......... 10% 186M 11s
26850K .......... .......... .......... .......... .......... 10% 164M 11s
26900K .......... .......... .......... .......... .......... 10% 191M 11s
26950K .......... .......... .......... .......... .......... 10% 166M 11s
27000K .......... .......... .......... .......... .......... 10% 142M 11s
27050K .......... .......... .......... .......... .......... 10% 166M 11s
27100K .......... .......... .......... .......... .......... 10% 150M 11s
27150K .......... .......... .......... .......... .......... 10% 236M 11s
27200K .......... .......... .......... .......... .......... 10% 116M 11s
27250K .......... .......... .......... .......... .......... 10% 193M 11s
27300K .......... .......... .......... .......... .......... 10% 153M 11s
27350K .......... .......... .......... .......... .......... 10% 120M 11s
27400K .......... .......... .......... .......... .......... 10% 195M 11s
27450K .......... .......... .......... .......... .......... 10% 140M 11s
27500K .......... .......... .......... .......... .......... 10% 158M 11s
27550K .......... .......... .......... .......... .......... 10% 21.0M 11s
27600K .......... .......... .......... .......... .......... 10% 1.47M 11s
27650K .......... .......... .......... .......... .......... 10% 159M 11s
27700K .......... .......... .......... .......... .......... 10% 184M 11s
27750K .......... .......... .......... .......... .......... 10% 208M 11s
27800K .......... .......... .......... .......... .......... 10% 206M 11s
27850K .......... .......... .......... .......... .......... 10% 183M 11s
27900K .......... .......... .......... .......... .......... 10% 228M 11s
27950K .......... .......... .......... .......... .......... 10% 205M 11s
28000K .......... .......... .......... .......... .......... 10% 238M 11s
28050K .......... .......... .......... .......... .......... 10% 233M 11s
28100K .......... .......... .......... .......... .......... 10% 199M 11s
28150K .......... .......... .......... .......... .......... 10% 233M 11s
28200K .......... .......... .......... .......... .......... 10% 203M 11s
28250K .......... .......... .......... .......... .......... 10% 222M 11s
28300K .......... .......... .......... .......... .......... 10% 233M 11s
28350K .......... .......... .......... .......... .......... 10% 203M 11s
28400K .......... .......... .......... .......... .......... 10% 253M 11s
28450K .......... .......... .......... .......... .......... 10% 218M 11s
28500K .......... .......... .......... .......... .......... 10% 254M 11s
28550K .......... .......... .......... .......... .......... 10% 247M 11s
28600K .......... .......... .......... .......... .......... 10% 51.2M 11s
28650K .......... .......... .......... .......... .......... 10% 1.36M 11s
28700K .......... .......... .......... .......... .......... 10% 191M 11s
28750K .......... .......... .......... .......... .......... 10% 146M 11s
28800K .......... .......... .......... .......... .......... 10% 27.3M 11s
28850K .......... .......... .......... .......... .......... 10% 24.7M 11s
28900K .......... .......... .......... .......... .......... 10% 91.3M 11s
28950K .......... .......... .......... .......... .......... 10% 162M 11s
29000K .......... .......... .......... .......... .......... 10% 213M 11s
29050K .......... .......... .......... .......... .......... 10% 214M 11s
29100K .......... .......... .......... .......... .......... 10% 157M 11s
29150K .......... .......... .......... .......... .......... 10% 222M 11s
29200K .......... .......... .......... .......... .......... 11% 175M 11s
29250K .......... .......... .......... .......... .......... 11% 185M 11s
29300K .......... .......... .......... .......... .......... 11% 182M 11s
29350K .......... .......... .......... .......... .......... 11% 187M 11s
29400K .......... .......... .......... .......... .......... 11% 181M 11s
29450K .......... .......... .......... .......... .......... 11% 189M 11s
29500K .......... .......... .......... .......... .......... 11% 229M 11s
29550K .......... .......... .......... .......... .......... 11% 223M 11s
29600K .......... .......... .......... .......... .......... 11% 194M 11s
29650K .......... .......... .......... .......... .......... 11% 228M 11s
29700K .......... .......... .......... .......... .......... 11% 5.19M 11s
29750K .......... .......... .......... .......... .......... 11% 203M 11s
29800K .......... .......... .......... .......... .......... 11% 171M 11s
29850K .......... .......... .......... .......... .......... 11% 156M 11s
29900K .......... .......... .......... .......... .......... 11% 174M 11s
29950K .......... .......... .......... .......... .......... 11% 135M 11s
30000K .......... .......... .......... .......... .......... 11% 199M 11s
30050K .......... .......... .......... .......... .......... 11% 222M 11s
30100K .......... .......... .......... .......... .......... 11% 191M 11s
30150K .......... .......... .......... .......... .......... 11% 223M 11s
30200K .......... .......... .......... .......... .......... 11% 195M 11s
30250K .......... .......... .......... .......... .......... 11% 219M 11s
30300K .......... .......... .......... .......... .......... 11% 223M 11s
30350K .......... .......... .......... .......... .......... 11% 196M 10s
30400K .......... .......... .......... .......... .......... 11% 229M 10s
30450K .......... .......... .......... .......... .......... 11% 198M 10s
30500K .......... .......... .......... .......... .......... 11% 221M 10s
30550K .......... .......... .......... .......... .......... 11% 225M 10s
30600K .......... .......... .......... .......... .......... 11% 191M 10s
30650K .......... .......... .......... .......... .......... 11% 231M 10s
30700K .......... .......... .......... .......... .......... 11% 3.00M 10s
30750K .......... .......... .......... .......... .......... 11% 197M 10s
30800K .......... .......... .......... .......... .......... 11% 199M 10s
30850K .......... .......... .......... .......... .......... 11% 173M 10s
30900K .......... .......... .......... .......... .......... 11% 198M 10s
30950K .......... .......... .......... .......... .......... 11% 173M 10s
31000K .......... .......... .......... .......... .......... 11% 197M 10s
31050K .......... .......... .......... .......... .......... 11% 206M 10s
31100K .......... .......... .......... .......... .......... 11% 185M 10s
31150K .......... .......... .......... .......... .......... 11% 208M 10s
31200K .......... .......... .......... .......... .......... 11% 178M 10s
31250K .......... .......... .......... .......... .......... 11% 207M 10s
31300K .......... .......... .......... .......... .......... 11% 216M 10s
31350K .......... .......... .......... .......... .......... 11% 184M 10s
31400K .......... .......... .......... .......... .......... 11% 207M 10s
31450K .......... .......... .......... .......... .......... 11% 174M 10s
31500K .......... .......... .......... .......... .......... 11% 201M 10s
31550K .......... .......... .......... .......... .......... 11% 194M 10s
31600K .......... .......... .......... .......... .......... 11% 171M 10s
31650K .......... .......... .......... .......... .......... 11% 205M 10s
31700K .......... .......... .......... .......... .......... 11% 6.30M 10s
31750K .......... .......... .......... .......... .......... 11% 44.4M 10s
31800K .......... .......... .......... .......... .......... 11% 173M 10s
31850K .......... .......... .......... .......... .......... 12% 129M 10s
31900K .......... .......... .......... .......... .......... 12% 107M 10s
31950K .......... .......... .......... .......... .......... 12% 143M 10s
32000K .......... .......... .......... .......... .......... 12% 123M 10s
32050K .......... .......... .......... .......... .......... 12% 77.0M 10s
32100K .......... .......... .......... .......... .......... 12% 78.8M 10s
32150K .......... .......... .......... .......... .......... 12% 92.0M 10s
32200K .......... .......... .......... .......... .......... 12% 112M 10s
32250K .......... .......... .......... .......... .......... 12% 157M 10s
32300K .......... .......... .......... .......... .......... 12% 192M 10s
32350K .......... .......... .......... .......... .......... 12% 182M 10s
32400K .......... .......... .......... .......... .......... 12% 207M 10s
32450K .......... .......... .......... .......... .......... 12% 168M 10s
32500K .......... .......... .......... .......... .......... 12% 210M 10s
32550K .......... .......... .......... .......... .......... 12% 233M 10s
32600K .......... .......... .......... .......... .......... 12% 171M 10s
32650K .......... .......... .......... .......... .......... 12% 184M 10s
32700K .......... .......... .......... .......... .......... 12% 109M 10s
32750K .......... .......... .......... .......... .......... 12% 3.19M 10s
32800K .......... .......... .......... .......... .......... 12% 210M 10s
32850K .......... .......... .......... .......... .......... 12% 184M 10s
32900K .......... .......... .......... .......... .......... 12% 222M 10s
32950K .......... .......... .......... .......... .......... 12% 194M 10s
33000K .......... .......... .......... .......... .......... 12% 219M 10s
33050K .......... .......... .......... .......... .......... 12% 178M 10s
33100K .......... .......... .......... .......... .......... 12% 98.0M 10s
33150K .......... .......... .......... .......... .......... 12% 168M 10s
33200K .......... .......... .......... .......... .......... 12% 81.9M 10s
33250K .......... .......... .......... .......... .......... 12% 104M 10s
33300K .......... .......... .......... .......... .......... 12% 97.7M 10s
33350K .......... .......... .......... .......... .......... 12% 187M 10s
33400K .......... .......... .......... .......... .......... 12% 103M 10s
33450K .......... .......... .......... .......... .......... 12% 129M 10s
33500K .......... .......... .......... .......... .......... 12% 142M 10s
33550K .......... .......... .......... .......... .......... 12% 191M 10s
33600K .......... .......... .......... .......... .......... 12% 199M 10s
33650K .......... .......... .......... .......... .......... 12% 200M 10s
33700K .......... .......... .......... .......... .......... 12% 166M 10s
33750K .......... .......... .......... .......... .......... 12% 859K 10s
33800K .......... .......... .......... .......... .......... 12% 207M 10s
33850K .......... .......... .......... .......... .......... 12% 188M 10s
33900K .......... .......... .......... .......... .......... 12% 198M 10s
33950K .......... .......... .......... .......... .......... 12% 174M 10s
34000K .......... .......... .......... .......... .......... 12% 194M 10s
34050K .......... .......... .......... .......... .......... 12% 198M 10s
34100K .......... .......... .......... .......... .......... 12% 174M 10s
34150K .......... .......... .......... .......... .......... 12% 205M 10s
34200K .......... .......... .......... .......... .......... 12% 176M 10s
34250K .......... .......... .......... .......... .......... 12% 207M 10s
34300K .......... .......... .......... .......... .......... 12% 204M 10s
34350K .......... .......... .......... .......... .......... 12% 167M 10s
34400K .......... .......... .......... .......... .......... 12% 201M 10s
34450K .......... .......... .......... .......... .......... 12% 176M 10s
34500K .......... .......... .......... .......... .......... 13% 203M 10s
34550K .......... .......... .......... .......... .......... 13% 201M 10s
34600K .......... .......... .......... .......... .......... 13% 173M 10s
34650K .......... .......... .......... .......... .......... 13% 198M 10s
34700K .......... .......... .......... .......... .......... 13% 169M 10s
34750K .......... .......... .......... .......... .......... 13% 195M 10s
34800K .......... .......... .......... .......... .......... 13% 123M 10s
34850K .......... .......... .......... .......... .......... 13% 173M 10s
34900K .......... .......... .......... .......... .......... 13% 201M 10s
34950K .......... .......... .......... .......... .......... 13% 177M 10s
35000K .......... .......... .......... .......... .......... 13% 186M 10s
35050K .......... .......... .......... .......... .......... 13% 194M 10s
35100K .......... .......... .......... .......... .......... 13% 175M 10s
35150K .......... .......... .......... .......... .......... 13% 195M 10s
35200K .......... .......... .......... .......... .......... 13% 159M 10s
35250K .......... .......... .......... .......... .......... 13% 192M 10s
35300K .......... .......... .......... .......... .......... 13% 193M 10s
35350K .......... .......... .......... .......... .......... 13% 186M 10s
35400K .......... .......... .......... .......... .......... 13% 199M 10s
35450K .......... .......... .......... .......... .......... 13% 163M 10s
35500K .......... .......... .......... .......... .......... 13% 170M 10s
35550K .......... .......... .......... .......... .......... 13% 150M 10s
35600K .......... .......... .......... .......... .......... 13% 142M 10s
35650K .......... .......... .......... .......... .......... 13% 189M 10s
35700K .......... .......... .......... .......... .......... 13% 195M 10s
35750K .......... .......... .......... .......... .......... 13% 234M 10s
35800K .......... .......... .......... .......... .......... 13% 146M 10s
35850K .......... .......... .......... .......... .......... 13% 165M 10s
35900K .......... .......... .......... .......... .......... 13% 228M 9s
35950K .......... .......... .......... .......... .......... 13% 173M 9s
36000K .......... .......... .......... .......... .......... 13% 199M 9s
36050K .......... .......... .......... .......... .......... 13% 221M 9s
36100K .......... .......... .......... .......... .......... 13% 195M 9s
36150K .......... .......... .......... .......... .......... 13% 204M 9s
36200K .......... .......... .......... .......... .......... 13% 164M 9s
36250K .......... .......... .......... .......... .......... 13% 1.86M 10s
36300K .......... .......... .......... .......... .......... 13% 72.8M 10s
36350K .......... .......... .......... .......... .......... 13% 83.5M 10s
36400K .......... .......... .......... .......... .......... 13% 126M 10s
36450K .......... .......... .......... .......... .......... 13% 128M 10s
36500K .......... .......... .......... .......... .......... 13% 154M 9s
36550K .......... .......... .......... .......... .......... 13% 155M 9s
36600K .......... .......... .......... .......... .......... 13% 138M 9s
36650K .......... .......... .......... .......... .......... 13% 161M 9s
36700K .......... .......... .......... .......... .......... 13% 157M 9s
36750K .......... .......... .......... .......... .......... 13% 191M 9s
36800K .......... .......... .......... .......... .......... 13% 161M 9s
36850K .......... .......... .......... .......... .......... 13% 1.95M 10s
36900K .......... .......... .......... .......... .......... 13% 33.6M 10s
36950K .......... .......... .......... .......... .......... 13% 79.5M 10s
37000K .......... .......... .......... .......... .......... 13% 218M 10s
37050K .......... .......... .......... .......... .......... 13% 112M 10s
37100K .......... .......... .......... .......... .......... 13% 174M 10s
37150K .......... .......... .......... .......... .......... 13% 216M 9s
37200K .......... .......... .......... .......... .......... 14% 104M 9s
37250K .......... .......... .......... .......... .......... 14% 115M 9s
37300K .......... .......... .......... .......... .......... 14% 198M 9s
37350K .......... .......... .......... .......... .......... 14% 188M 9s
37400K .......... .......... .......... .......... .......... 14% 230M 9s
37450K .......... .......... .......... .......... .......... 14% 198M 9s
37500K .......... .......... .......... .......... .......... 14% 231M 9s
37550K .......... .......... .......... .......... .......... 14% 235M 9s
37600K .......... .......... .......... .......... .......... 14% 164M 9s
37650K .......... .......... .......... .......... .......... 14% 211M 9s
37700K .......... .......... .......... .......... .......... 14% 192M 9s
37750K .......... .......... .......... .......... .......... 14% 229M 9s
37800K .......... .......... .......... .......... .......... 14% 231M 9s
37850K .......... .......... .......... .......... .......... 14% 1.26M 10s
37900K .......... .......... .......... .......... .......... 14% 112M 10s
37950K .......... .......... .......... .......... .......... 14% 56.0M 10s
38000K .......... .......... .......... .......... .......... 14% 99.4M 10s
38050K .......... .......... .......... .......... .......... 14% 116M 9s
38100K .......... .......... .......... .......... .......... 14% 191M 9s
38150K .......... .......... .......... .......... .......... 14% 229M 9s
38200K .......... .......... .......... .......... .......... 14% 189M 9s
38250K .......... .......... .......... .......... .......... 14% 44.3M 9s
38300K .......... .......... .......... .......... .......... 14% 13.0M 9s
38350K .......... .......... .......... .......... .......... 14% 94.3M 9s
38400K .......... .......... .......... .......... .......... 14% 136M 9s
38450K .......... .......... .......... .......... .......... 14% 117M 9s
38500K .......... .......... .......... .......... .......... 14% 127M 9s
38550K .......... .......... .......... .......... .......... 14% 96.3M 9s
38600K .......... .......... .......... .......... .......... 14% 49.3M 9s
38650K .......... .......... .......... .......... .......... 14% 60.1M 9s
38700K .......... .......... .......... .......... .......... 14% 185M 9s
38750K .......... .......... .......... .......... .......... 14% 213M 9s
38800K .......... .......... .......... .......... .......... 14% 218M 9s
38850K .......... .......... .......... .......... .......... 14% 188M 9s
38900K .......... .......... .......... .......... .......... 14% 880K 10s
38950K .......... .......... .......... .......... .......... 14% 9.52M 10s
39000K .......... .......... .......... .......... .......... 14% 18.4M 10s
39050K .......... .......... .......... .......... .......... 14% 13.3M 10s
39100K .......... .......... .......... .......... .......... 14% 11.3M 10s
39150K .......... .......... .......... .......... .......... 14% 15.1M 10s
39200K .......... .......... .......... .......... .......... 14% 10.9M 10s
39250K .......... .......... .......... .......... .......... 14% 211M 10s
39300K .......... .......... .......... .......... .......... 14% 222M 10s
39350K .......... .......... .......... .......... .......... 14% 197M 10s
39400K .......... .......... .......... .......... .......... 14% 229M 10s
39450K .......... .......... .......... .......... .......... 14% 147M 10s
39500K .......... .......... .......... .......... .......... 14% 184M 10s
39550K .......... .......... .......... .......... .......... 14% 132M 10s
39600K .......... .......... .......... .......... .......... 14% 165M 10s
39650K .......... .......... .......... .......... .......... 14% 227M 10s
39700K .......... .......... .......... .......... .......... 14% 195M 10s
39750K .......... .......... .......... .......... .......... 14% 222M 10s
39800K .......... .......... .......... .......... .......... 14% 228M 10s
39850K .......... .......... .......... .......... .......... 15% 193M 10s
39900K .......... .......... .......... .......... .......... 15% 1.35M 10s
39950K .......... .......... .......... .......... .......... 15% 61.3M 10s
40000K .......... .......... .......... .......... .......... 15% 2.01M 10s
40050K .......... .......... .......... .......... .......... 15% 8.53M 10s
40100K .......... .......... .......... .......... .......... 15% 64.9M 10s
40150K .......... .......... .......... .......... .......... 15% 218M 10s
40200K .......... .......... .......... .......... .......... 15% 130M 10s
40250K .......... .......... .......... .......... .......... 15% 182M 10s
40300K .......... .......... .......... .......... .......... 15% 182M 10s
40350K .......... .......... .......... .......... .......... 15% 171M 10s
40400K .......... .......... .......... .......... .......... 15% 156M 10s
40450K .......... .......... .......... .......... .......... 15% 180M 10s
40500K .......... .......... .......... .......... .......... 15% 221M 10s
40550K .......... .......... .......... .......... .......... 15% 217M 10s
40600K .......... .......... .......... .......... .......... 15% 138M 10s
40650K .......... .......... .......... .......... .......... 15% 177M 10s
40700K .......... .......... .......... .......... .......... 15% 196M 10s
40750K .......... .......... .......... .......... .......... 15% 229M 10s
40800K .......... .......... .......... .......... .......... 15% 229M 10s
40850K .......... .......... .......... .......... .......... 15% 190M 10s
40900K .......... .......... .......... .......... .......... 15% 221M 10s
40950K .......... .......... .......... .......... .......... 15% 2.46M 10s
41000K .......... .......... .......... .......... .......... 15% 64.5M 10s
41050K .......... .......... .......... .......... .......... 15% 103M 10s
41100K .......... .......... .......... .......... .......... 15% 142M 10s
41150K .......... .......... .......... .......... .......... 15% 133M 10s
41200K .......... .......... .......... .......... .......... 15% 131M 10s
41250K .......... .......... .......... .......... .......... 15% 171M 10s
41300K .......... .......... .......... .......... .......... 15% 188M 10s
41350K .......... .......... .......... .......... .......... 15% 188M 10s
41400K .......... .......... .......... .......... .......... 15% 212M 10s
41450K .......... .......... .......... .......... .......... 15% 179M 10s
41500K .......... .......... .......... .......... .......... 15% 211M 10s
41550K .......... .......... .......... .......... .......... 15% 211M 10s
41600K .......... .......... .......... .......... .......... 15% 728K 10s
41650K .......... .......... .......... .......... .......... 15% 134M 10s
41700K .......... .......... .......... .......... .......... 15% 150M 10s
41750K .......... .......... .......... .......... .......... 15% 123M 10s
41800K .......... .......... .......... .......... .......... 15% 73.3M 10s
41850K .......... .......... .......... .......... .......... 15% 32.3M 10s
41900K .......... .......... .......... .......... .......... 15% 94.8M 10s
41950K .......... .......... .......... .......... .......... 15% 3.45M 10s
42000K .......... .......... .......... .......... .......... 15% 146M 10s
42050K .......... .......... .......... .......... .......... 15% 201M 10s
42100K .......... .......... .......... .......... .......... 15% 166M 10s
42150K .......... .......... .......... .......... .......... 15% 194M 10s
42200K .......... .......... .......... .......... .......... 15% 153M 10s
42250K .......... .......... .......... .......... .......... 15% 198M 10s
42300K .......... .......... .......... .......... .......... 15% 197M 10s
42350K .......... .......... .......... .......... .......... 15% 166M 10s
42400K .......... .......... .......... .......... .......... 15% 171M 10s
42450K .......... .......... .......... .......... .......... 15% 166M 10s
42500K .......... .......... .......... .......... .......... 16% 241M 10s
42550K .......... .......... .......... .......... .......... 16% 242M 10s
42600K .......... .......... .......... .......... .......... 16% 210M 10s
42650K .......... .......... .......... .......... .......... 16% 242M 10s
42700K .......... .......... .......... .......... .......... 16% 213M 10s
42750K .......... .......... .......... .......... .......... 16% 247M 10s
42800K .......... .......... .......... .......... .......... 16% 249M 10s
42850K .......... .......... .......... .......... .......... 16% 211M 10s
42900K .......... .......... .......... .......... .......... 16% 236M 10s
42950K .......... .......... .......... .......... .......... 16% 117M 10s
43000K .......... .......... .......... .......... .......... 16% 9.29M 10s
43050K .......... .......... .......... .......... .......... 16% 200M 10s
43100K .......... .......... .......... .......... .......... 16% 18.1M 10s
43150K .......... .......... .......... .......... .......... 16% 32.4M 10s
43200K .......... .......... .......... .......... .......... 16% 163M 10s
43250K .......... .......... .......... .......... .......... 16% 180M 10s
43300K .......... .......... .......... .......... .......... 16% 185M 10s
43350K .......... .......... .......... .......... .......... 16% 158M 10s
43400K .......... .......... .......... .......... .......... 16% 195M 10s
43450K .......... .......... .......... .......... .......... 16% 182M 10s
43500K .......... .......... .......... .......... .......... 16% 200M 10s
43550K .......... .......... .......... .......... .......... 16% 194M 10s
43600K .......... .......... .......... .......... .......... 16% 157M 10s
43650K .......... .......... .......... .......... .......... 16% 191M 10s
43700K .......... .......... .......... .......... .......... 16% 157M 10s
43750K .......... .......... .......... .......... .......... 16% 185M 10s
43800K .......... .......... .......... .......... .......... 16% 193M 10s
43850K .......... .......... .......... .......... .......... 16% 161M 10s
43900K .......... .......... .......... .......... .......... 16% 189M 10s
43950K .......... .......... .......... .......... .......... 16% 158M 10s
44000K .......... .......... .......... .......... .......... 16% 123M 9s
44050K .......... .......... .......... .......... .......... 16% 184M 9s
44100K .......... .......... .......... .......... .......... 16% 170M 9s
44150K .......... .......... .......... .......... .......... 16% 189M 9s
44200K .......... .......... .......... .......... .......... 16% 164M 9s
44250K .......... .......... .......... .......... .......... 16% 203M 9s
44300K .......... .......... .......... .......... .......... 16% 198M 9s
44350K .......... .......... .......... .......... .......... 16% 171M 9s
44400K .......... .......... .......... .......... .......... 16% 233M 9s
44450K .......... .......... .......... .......... .......... 16% 203M 9s
44500K .......... .......... .......... .......... .......... 16% 233M 9s
44550K .......... .......... .......... .......... .......... 16% 239M 9s
44600K .......... .......... .......... .......... .......... 16% 203M 9s
44650K .......... .......... .......... .......... .......... 16% 234M 9s
44700K .......... .......... .......... .......... .......... 16% 172M 9s
44750K .......... .......... .......... .......... .......... 16% 230M 9s
44800K .......... .......... .......... .......... .......... 16% 234M 9s
44850K .......... .......... .......... .......... .......... 16% 202M 9s
44900K .......... .......... .......... .......... .......... 16% 235M 9s
44950K .......... .......... .......... .......... .......... 16% 205M 9s
45000K .......... .......... .......... .......... .......... 16% 214M 9s
45050K .......... .......... .......... .......... .......... 16% 406K 10s
45100K .......... .......... .......... .......... .......... 16% 46.4M 10s
45150K .......... .......... .......... .......... .......... 17% 70.3M 10s
45200K .......... .......... .......... .......... .......... 17% 47.3M 10s
45250K .......... .......... .......... .......... .......... 17% 157M 10s
45300K .......... .......... .......... .......... .......... 17% 130M 10s
45350K .......... .......... .......... .......... .......... 17% 61.0M 10s
45400K .......... .......... .......... .......... .......... 17% 190M 10s
45450K .......... .......... .......... .......... .......... 17% 161M 10s
45500K .......... .......... .......... .......... .......... 17% 130M 10s
45550K .......... .......... .......... .......... .......... 17% 114M 10s
45600K .......... .......... .......... .......... .......... 17% 133M 10s
45650K .......... .......... .......... .......... .......... 17% 178M 10s
45700K .......... .......... .......... .......... .......... 17% 96.3M 10s
45750K .......... .......... .......... .......... .......... 17% 173M 10s
45800K .......... .......... .......... .......... .......... 17% 166M 10s
45850K .......... .......... .......... .......... .......... 17% 117M 10s
45900K .......... .......... .......... .......... .......... 17% 102M 10s
45950K .......... .......... .......... .......... .......... 17% 151M 10s
46000K .......... .......... .......... .......... .......... 17% 158M 10s
46050K .......... .......... .......... .......... .......... 17% 66.4M 10s
46100K .......... .......... .......... .......... .......... 17% 115M 10s
46150K .......... .......... .......... .......... .......... 17% 135M 10s
46200K .......... .......... .......... .......... .......... 17% 168M 10s
46250K .......... .......... .......... .......... .......... 17% 203M 10s
46300K .......... .......... .......... .......... .......... 17% 204M 10s
46350K .......... .......... .......... .......... .......... 17% 176M 10s
46400K .......... .......... .......... .......... .......... 17% 205M 10s
46450K .......... .......... .......... .......... .......... 17% 186M 10s
46500K .......... .......... .......... .......... .......... 17% 203M 10s
46550K .......... .......... .......... .......... .......... 17% 203M 10s
46600K .......... .......... .......... .......... .......... 17% 170M 10s
46650K .......... .......... .......... .......... .......... 17% 191M 10s
46700K .......... .......... .......... .......... .......... 17% 185M 9s
46750K .......... .......... .......... .......... .......... 17% 213M 9s
46800K .......... .......... .......... .......... .......... 17% 190M 9s
46850K .......... .......... .......... .......... .......... 17% 181M 9s
46900K .......... .......... .......... .......... .......... 17% 225M 9s
46950K .......... .......... .......... .......... .......... 17% 186M 9s
47000K .......... .......... .......... .......... .......... 17% 230M 9s
47050K .......... .......... .......... .......... .......... 17% 221M 9s
47100K .......... .......... .......... .......... .......... 17% 1.77M 10s
47150K .......... .......... .......... .......... .......... 17% 58.1M 10s
47200K .......... .......... .......... .......... .......... 17% 166M 10s
47250K .......... .......... .......... .......... .......... 17% 106M 10s
47300K .......... .......... .......... .......... .......... 17% 176M 9s
47350K .......... .......... .......... .......... .......... 17% 131M 9s
47400K .......... .......... .......... .......... .......... 17% 38.9M 9s
47450K .......... .......... .......... .......... .......... 17% 151M 9s
47500K .......... .......... .......... .......... .......... 17% 210M 9s
47550K .......... .......... .......... .......... .......... 17% 119M 9s
47600K .......... .......... .......... .......... .......... 17% 99.4M 9s
47650K .......... .......... .......... .......... .......... 17% 108M 9s
47700K .......... .......... .......... .......... .......... 17% 152M 9s
47750K .......... .......... .......... .......... .......... 17% 223M 9s
47800K .......... .......... .......... .......... .......... 18% 225M 9s
47850K .......... .......... .......... .......... .......... 18% 194M 9s
47900K .......... .......... .......... .......... .......... 18% 194M 9s
47950K .......... .......... .......... .......... .......... 18% 168M 9s
48000K .......... .......... .......... .......... .......... 18% 227M 9s
48050K .......... .......... .......... .......... .......... 18% 203M 9s
48100K .......... .......... .......... .......... .......... 18% 1.95M 9s
48150K .......... .......... .......... .......... .......... 18% 164M 9s
48200K .......... .......... .......... .......... .......... 18% 177M 9s
48250K .......... .......... .......... .......... .......... 18% 202M 9s
48300K .......... .......... .......... .......... .......... 18% 212M 9s
48350K .......... .......... .......... .......... .......... 18% 188M 9s
48400K .......... .......... .......... .......... .......... 18% 218M 9s
48450K .......... .......... .......... .......... .......... 18% 189M 9s
48500K .......... .......... .......... .......... .......... 18% 210M 9s
48550K .......... .......... .......... .......... .......... 18% 206M 9s
48600K .......... .......... .......... .......... .......... 18% 100M 9s
48650K .......... .......... .......... .......... .......... 18% 210M 9s
48700K .......... .......... .......... .......... .......... 18% 199M 9s
48750K .......... .......... .......... .......... .......... 18% 224M 9s
48800K .......... .......... .......... .......... .......... 18% 234M 9s
48850K .......... .......... .......... .......... .......... 18% 210M 9s
48900K .......... .......... .......... .......... .......... 18% 236M 9s
48950K .......... .......... .......... .......... .......... 18% 210M 9s
49000K .......... .......... .......... .......... .......... 18% 244M 9s
49050K .......... .......... .......... .......... .......... 18% 242M 9s
49100K .......... .......... .......... .......... .......... 18% 125M 9s
49150K .......... .......... .......... .......... .......... 18% 3.53M 9s
49200K .......... .......... .......... .......... .......... 18% 168M 9s
49250K .......... .......... .......... .......... .......... 18% 216M 9s
49300K .......... .......... .......... .......... .......... 18% 153M 9s
49350K .......... .......... .......... .......... .......... 18% 184M 9s
49400K .......... .......... .......... .......... .......... 18% 65.1M 9s
49450K .......... .......... .......... .......... .......... 18% 123M 9s
49500K .......... .......... .......... .......... .......... 18% 191M 9s
49550K .......... .......... .......... .......... .......... 18% 201M 9s
49600K .......... .......... .......... .......... .......... 18% 189M 9s
49650K .......... .......... .......... .......... .......... 18% 73.0M 9s
49700K .......... .......... .......... .......... .......... 18% 180M 9s
49750K .......... .......... .......... .......... .......... 18% 97.3M 9s
49800K .......... .......... .......... .......... .......... 18% 103M 9s
49850K .......... .......... .......... .......... .......... 18% 98.2M 9s
49900K .......... .......... .......... .......... .......... 18% 215M 9s
49950K .......... .......... .......... .......... .......... 18% 196M 9s
50000K .......... .......... .......... .......... .......... 18% 225M 9s
50050K .......... .......... .......... .......... .......... 18% 216M 9s
50100K .......... .......... .......... .......... .......... 18% 195M 9s
50150K .......... .......... .......... .......... .......... 18% 1.08M 9s
50200K .......... .......... .......... .......... .......... 18% 7.46M 9s
50250K .......... .......... .......... .......... .......... 18% 6.08M 9s
50300K .......... .......... .......... .......... .......... 18% 11.3M 9s
50350K .......... .......... .......... .......... .......... 18% 12.0M 9s
50400K .......... .......... .......... .......... .......... 18% 22.7M 9s
50450K .......... .......... .......... .......... .......... 19% 70.9M 9s
50500K .......... .......... .......... .......... .......... 19% 4.78M 9s
50550K .......... .......... .......... .......... .......... 19% 209M 9s
50600K .......... .......... .......... .......... .......... 19% 197M 9s
50650K .......... .......... .......... .......... .......... 19% 225M 9s
50700K .......... .......... .......... .......... .......... 19% 190M 9s
50750K .......... .......... .......... .......... .......... 19% 110M 9s
50800K .......... .......... .......... .......... .......... 19% 2.10M 9s
50850K .......... .......... .......... .......... .......... 19% 6.50M 9s
50900K .......... .......... .......... .......... .......... 19% 16.1M 9s
50950K .......... .......... .......... .......... .......... 19% 7.25M 9s
51000K .......... .......... .......... .......... .......... 19% 17.6M 9s
51050K .......... .......... .......... .......... .......... 19% 183M 9s
51100K .......... .......... .......... .......... .......... 19% 60.5M 9s
51150K .......... .......... .......... .......... .......... 19% 99.9M 9s
51200K .......... .......... .......... .......... .......... 19% 106M 9s
51250K .......... .......... .......... .......... .......... 19% 219M 9s
51300K .......... .......... .......... .......... .......... 19% 110M 9s
51350K .......... .......... .......... .......... .......... 19% 14.9M 9s
51400K .......... .......... .......... .......... .......... 19% 220M 9s
51450K .......... .......... .......... .......... .......... 19% 188M 9s
51500K .......... .......... .......... .......... .......... 19% 233M 9s
51550K .......... .......... .......... .......... .......... 19% 214M 9s
51600K .......... .......... .......... .......... .......... 19% 185M 9s
51650K .......... .......... .......... .......... .......... 19% 225M 9s
51700K .......... .......... .......... .......... .......... 19% 201M 9s
51750K .......... .......... .......... .......... .......... 19% 1.62M 9s
51800K .......... .......... .......... .......... .......... 19% 37.0M 9s
51850K .......... .......... .......... .......... .......... 19% 91.3M 9s
51900K .......... .......... .......... .......... .......... 19% 210M 9s
51950K .......... .......... .......... .......... .......... 19% 189M 9s
52000K .......... .......... .......... .......... .......... 19% 219M 9s
52050K .......... .......... .......... .......... .......... 19% 224M 9s
52100K .......... .......... .......... .......... .......... 19% 189M 9s
52150K .......... .......... .......... .......... .......... 19% 219M 9s
52200K .......... .......... .......... .......... .......... 19% 8.26M 9s
52250K .......... .......... .......... .......... .......... 19% 144M 9s
52300K .......... .......... .......... .......... .......... 19% 185M 9s
52350K .......... .......... .......... .......... .......... 19% 134M 9s
52400K .......... .......... .......... .......... .......... 19% 177M 9s
52450K .......... .......... .......... .......... .......... 19% 136M 9s
52500K .......... .......... .......... .......... .......... 19% 160M 9s
52550K .......... .......... .......... .......... .......... 19% 223M 9s
52600K .......... .......... .......... .......... .......... 19% 140M 9s
52650K .......... .......... .......... .......... .......... 19% 139M 9s
52700K .......... .......... .......... .......... .......... 19% 138M 9s
52750K .......... .......... .......... .......... .......... 19% 181M 9s
52800K .......... .......... .......... .......... .......... 19% 135M 9s
52850K .......... .......... .......... .......... .......... 19% 145M 9s
52900K .......... .......... .......... .......... .......... 19% 226M 9s
52950K .......... .......... .......... .......... .......... 19% 203M 9s
53000K .......... .......... .......... .......... .......... 19% 237M 9s
53050K .......... .......... .......... .......... .......... 19% 239M 9s
53100K .......... .......... .......... .......... .......... 20% 202M 9s
53150K .......... .......... .......... .......... .......... 20% 223M 9s
53200K .......... .......... .......... .......... .......... 20% 9.80M 9s
53250K .......... .......... .......... .......... .......... 20% 106M 9s
53300K .......... .......... .......... .......... .......... 20% 144M 9s
53350K .......... .......... .......... .......... .......... 20% 48.2M 9s
53400K .......... .......... .......... .......... .......... 20% 97.3M 9s
53450K .......... .......... .......... .......... .......... 20% 86.7M 9s
53500K .......... .......... .......... .......... .......... 20% 113M 9s
53550K .......... .......... .......... .......... .......... 20% 107M 9s
53600K .......... .......... .......... .......... .......... 20% 85.4M 9s
53650K .......... .......... .......... .......... .......... 20% 130M 9s
53700K .......... .......... .......... .......... .......... 20% 23.5M 9s
53750K .......... .......... .......... .......... .......... 20% 188M 9s
53800K .......... .......... .......... .......... .......... 20% 181M 9s
53850K .......... .......... .......... .......... .......... 20% 184M 9s
53900K .......... .......... .......... .......... .......... 20% 195M 9s
53950K .......... .......... .......... .......... .......... 20% 128M 9s
54000K .......... .......... .......... .......... .......... 20% 184M 9s
54050K .......... .......... .......... .......... .......... 20% 144M 9s
54100K .......... .......... .......... .......... .......... 20% 150M 9s
54150K .......... .......... .......... .......... .......... 20% 191M 9s
54200K .......... .......... .......... .......... .......... 20% 173M 9s
54250K .......... .......... .......... .......... .......... 20% 7.09M 9s
54300K .......... .......... .......... .......... .......... 20% 207M 9s
54350K .......... .......... .......... .......... .......... 20% 55.6M 9s
54400K .......... .......... .......... .......... .......... 20% 210M 9s
54450K .......... .......... .......... .......... .......... 20% 198M 9s
54500K .......... .......... .......... .......... .......... 20% 141M 9s
54550K .......... .......... .......... .......... .......... 20% 218M 9s
54600K .......... .......... .......... .......... .......... 20% 197M 9s
54650K .......... .......... .......... .......... .......... 20% 221M 9s
54700K .......... .......... .......... .......... .......... 20% 89.1M 9s
54750K .......... .......... .......... .......... .......... 20% 153M 9s
54800K .......... .......... .......... .......... .......... 20% 210M 9s
54850K .......... .......... .......... .......... .......... 20% 194M 9s
54900K .......... .......... .......... .......... .......... 20% 210M 9s
54950K .......... .......... .......... .......... .......... 20% 158M 9s
55000K .......... .......... .......... .......... .......... 20% 229M 9s
55050K .......... .......... .......... .......... .......... 20% 231M 9s
55100K .......... .......... .......... .......... .......... 20% 195M 9s
55150K .......... .......... .......... .......... .......... 20% 206M 9s
55200K .......... .......... .......... .......... .......... 20% 191M 9s
55250K .......... .......... .......... .......... .......... 20% 2.63M 9s
55300K .......... .......... .......... .......... .......... 20% 158M 9s
55350K .......... .......... .......... .......... .......... 20% 195M 9s
55400K .......... .......... .......... .......... .......... 20% 224M 9s
55450K .......... .......... .......... .......... .......... 20% 191M 9s
55500K .......... .......... .......... .......... .......... 20% 217M 9s
55550K .......... .......... .......... .......... .......... 20% 213M 9s
55600K .......... .......... .......... .......... .......... 20% 147M 9s
55650K .......... .......... .......... .......... .......... 20% 142M 9s
55700K .......... .......... .......... .......... .......... 20% 172M 9s
55750K .......... .......... .......... .......... .......... 20% 227M 9s
55800K .......... .......... .......... .......... .......... 21% 233M 9s
55850K .......... .......... .......... .......... .......... 21% 209M 9s
55900K .......... .......... .......... .......... .......... 21% 242M 9s
55950K .......... .......... .......... .......... .......... 21% 207M 9s
56000K .......... .......... .......... .......... .......... 21% 211M 9s
56050K .......... .......... .......... .......... .......... 21% 217M 9s
56100K .......... .......... .......... .......... .......... 21% 189M 9s
56150K .......... .......... .......... .......... .......... 21% 218M 9s
56200K .......... .......... .......... .......... .......... 21% 203M 9s
56250K .......... .......... .......... .......... .......... 21% 227M 9s
56300K .......... .......... .......... .......... .......... 21% 2.37M 9s
56350K .......... .......... .......... .......... .......... 21% 176M 9s
56400K .......... .......... .......... .......... .......... 21% 81.4M 9s
56450K .......... .......... .......... .......... .......... 21% 179M 9s
56500K .......... .......... .......... .......... .......... 21% 220M 9s
56550K .......... .......... .......... .......... .......... 21% 195M 9s
56600K .......... .......... .......... .......... .......... 21% 165M 9s
56650K .......... .......... .......... .......... .......... 21% 209M 9s
56700K .......... .......... .......... .......... .......... 21% 179M 9s
56750K .......... .......... .......... .......... .......... 21% 208M 9s
56800K .......... .......... .......... .......... .......... 21% 195M 9s
56850K .......... .......... .......... .......... .......... 21% 42.3M 9s
56900K .......... .......... .......... .......... .......... 21% 110M 9s
56950K .......... .......... .......... .......... .......... 21% 116M 9s
57000K .......... .......... .......... .......... .......... 21% 135M 9s
57050K .......... .......... .......... .......... .......... 21% 121M 9s
57100K .......... .......... .......... .......... .......... 21% 131M 9s
57150K .......... .......... .......... .......... .......... 21% 136M 9s
57200K .......... .......... .......... .......... .......... 21% 104M 9s
57250K .......... .......... .......... .......... .......... 21% 135M 9s
57300K .......... .......... .......... .......... .......... 21% 107M 9s
57350K .......... .......... .......... .......... .......... 21% 2.42M 9s
57400K .......... .......... .......... .......... .......... 21% 54.1M 9s
57450K .......... .......... .......... .......... .......... 21% 168M 9s
57500K .......... .......... .......... .......... .......... 21% 198M 9s
57550K .......... .......... .......... .......... .......... 21% 194M 9s
57600K .......... .......... .......... .......... .......... 21% 174M 9s
57650K .......... .......... .......... .......... .......... 21% 208M 9s
57700K .......... .......... .......... .......... .......... 21% 171M 9s
57750K .......... .......... .......... .......... .......... 21% 216M 9s
57800K .......... .......... .......... .......... .......... 21% 208M 9s
57850K .......... .......... .......... .......... .......... 21% 157M 9s
57900K .......... .......... .......... .......... .......... 21% 189M 9s
57950K .......... .......... .......... .......... .......... 21% 180M 9s
58000K .......... .......... .......... .......... .......... 21% 214M 9s
58050K .......... .......... .......... .......... .......... 21% 221M 9s
58100K .......... .......... .......... .......... .......... 21% 205M 9s
58150K .......... .......... .......... .......... .......... 21% 245M 9s
58200K .......... .......... .......... .......... .......... 21% 215M 9s
58250K .......... .......... .......... .......... .......... 21% 249M 9s
58300K .......... .......... .......... .......... .......... 21% 247M 9s
58350K .......... .......... .......... .......... .......... 21% 4.17M 9s
58400K .......... .......... .......... .......... .......... 21% 108M 9s
58450K .......... .......... .......... .......... .......... 22% 67.2M 9s
58500K .......... .......... .......... .......... .......... 22% 186M 9s
58550K .......... .......... .......... .......... .......... 22% 192M 9s
58600K .......... .......... .......... .......... .......... 22% 156M 9s
58650K .......... .......... .......... .......... .......... 22% 233M 9s
58700K .......... .......... .......... .......... .......... 22% 204M 8s
58750K .......... .......... .......... .......... .......... 22% 207M 8s
58800K .......... .......... .......... .......... .......... 22% 195M 8s
58850K .......... .......... .......... .......... .......... 22% 198M 8s
58900K .......... .......... .......... .......... .......... 22% 235M 8s
58950K .......... .......... .......... .......... .......... 22% 156M 8s
59000K .......... .......... .......... .......... .......... 22% 193M 8s
59050K .......... .......... .......... .......... .......... 22% 173M 8s
59100K .......... .......... .......... .......... .......... 22% 127M 8s
59150K .......... .......... .......... .......... .......... 22% 206M 8s
59200K .......... .......... .......... .......... .......... 22% 146M 8s
59250K .......... .......... .......... .......... .......... 22% 182M 8s
59300K .......... .......... .......... .......... .......... 22% 211M 8s
59350K .......... .......... .......... .......... .......... 22% 2.26M 8s
59400K .......... .......... .......... .......... .......... 22% 192M 8s
59450K .......... .......... .......... .......... .......... 22% 173M 8s
59500K .......... .......... .......... .......... .......... 22% 70.4M 8s
59550K .......... .......... .......... .......... .......... 22% 66.5M 8s
59600K .......... .......... .......... .......... .......... 22% 178M 8s
59650K .......... .......... .......... .......... .......... 22% 199M 8s
59700K .......... .......... .......... .......... .......... 22% 191M 8s
59750K .......... .......... .......... .......... .......... 22% 207M 8s
59800K .......... .......... .......... .......... .......... 22% 189M 8s
59850K .......... .......... .......... .......... .......... 22% 180M 8s
59900K .......... .......... .......... .......... .......... 22% 208M 8s
59950K .......... .......... .......... .......... .......... 22% 161M 8s
60000K .......... .......... .......... .......... .......... 22% 197M 8s
60050K .......... .......... .......... .......... .......... 22% 208M 8s
60100K .......... .......... .......... .......... .......... 22% 169M 8s
60150K .......... .......... .......... .......... .......... 22% 214M 8s
60200K .......... .......... .......... .......... .......... 22% 191M 8s
60250K .......... .......... .......... .......... .......... 22% 215M 8s
60300K .......... .......... .......... .......... .......... 22% 227M 8s
60350K .......... .......... .......... .......... .......... 22% 163M 8s
60400K .......... .......... .......... .......... .......... 22% 791K 9s
60450K .......... .......... .......... .......... .......... 22% 185M 9s
60500K .......... .......... .......... .......... .......... 22% 224M 8s
60550K .......... .......... .......... .......... .......... 22% 212M 8s
60600K .......... .......... .......... .......... .......... 22% 198M 8s
60650K .......... .......... .......... .......... .......... 22% 224M 8s
60700K .......... .......... .......... .......... .......... 22% 197M 8s
60750K .......... .......... .......... .......... .......... 22% 7.49M 8s
60800K .......... .......... .......... .......... .......... 22% 218M 8s
60850K .......... .......... .......... .......... .......... 22% 159M 8s
60900K .......... .......... .......... .......... .......... 22% 229M 8s
60950K .......... .......... .......... .......... .......... 22% 204M 8s
61000K .......... .......... .......... .......... .......... 22% 245M 8s
61050K .......... .......... .......... .......... .......... 22% 9.68M 8s
61100K .......... .......... .......... .......... .......... 23% 80.0M 8s
61150K .......... .......... .......... .......... .......... 23% 211M 8s
61200K .......... .......... .......... .......... .......... 23% 30.1M 8s
61250K .......... .......... .......... .......... .......... 23% 215M 8s
61300K .......... .......... .......... .......... .......... 23% 227M 8s
61350K .......... .......... .......... .......... .......... 23% 189M 8s
61400K .......... .......... .......... .......... .......... 23% 2.14M 8s
61450K .......... .......... .......... .......... .......... 23% 152M 8s
61500K .......... .......... .......... .......... .......... 23% 218M 8s
61550K .......... .......... .......... .......... .......... 23% 206M 8s
61600K .......... .......... .......... .......... .......... 23% 174M 8s
61650K .......... .......... .......... .......... .......... 23% 217M 8s
61700K .......... .......... .......... .......... .......... 23% 191M 8s
61750K .......... .......... .......... .......... .......... 23% 207M 8s
61800K .......... .......... .......... .......... .......... 23% 197M 8s
61850K .......... .......... .......... .......... .......... 23% 164M 8s
61900K .......... .......... .......... .......... .......... 23% 214M 8s
61950K .......... .......... .......... .......... .......... 23% 170M 8s
62000K .......... .......... .......... .......... .......... 23% 213M 8s
62050K .......... .......... .......... .......... .......... 23% 200M 8s
62100K .......... .......... .......... .......... .......... 23% 178M 8s
62150K .......... .......... .......... .......... .......... 23% 223M 8s
62200K .......... .......... .......... .......... .......... 23% 195M 8s
62250K .......... .......... .......... .......... .......... 23% 200M 8s
62300K .......... .......... .......... .......... .......... 23% 200M 8s
62350K .......... .......... .......... .......... .......... 23% 191M 8s
62400K .......... .......... .......... .......... .......... 23% 5.72M 8s
62450K .......... .......... .......... .......... .......... 23% 73.6M 8s
62500K .......... .......... .......... .......... .......... 23% 43.6M 8s
62550K .......... .......... .......... .......... .......... 23% 167M 8s
62600K .......... .......... .......... .......... .......... 23% 135M 8s
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62700K .......... .......... .......... .......... .......... 23% 176M 8s
62750K .......... .......... .......... .......... .......... 23% 206M 8s
62800K .......... .......... .......... .......... .......... 23% 204M 8s
62850K .......... .......... .......... .......... .......... 23% 176M 8s
62900K .......... .......... .......... .......... .......... 23% 230M 8s
62950K .......... .......... .......... .......... .......... 23% 189M 8s
63000K .......... .......... .......... .......... .......... 23% 235M 8s
63050K .......... .......... .......... .......... .......... 23% 234M 8s
63100K .......... .......... .......... .......... .......... 23% 189M 8s
63150K .......... .......... .......... .......... .......... 23% 208M 8s
63200K .......... .......... .......... .......... .......... 23% 170M 8s
63250K .......... .......... .......... .......... .......... 23% 194M 8s
63300K .......... .......... .......... .......... .......... 23% 220M 8s
63350K .......... .......... .......... .......... .......... 23% 191M 8s
63400K .......... .......... .......... .......... .......... 23% 197M 8s
63450K .......... .......... .......... .......... .......... 23% 1.70M 8s
63500K .......... .......... .......... .......... .......... 23% 40.6M 8s
63550K .......... .......... .......... .......... .......... 23% 162M 8s
63600K .......... .......... .......... .......... .......... 23% 136M 8s
63650K .......... .......... .......... .......... .......... 23% 219M 8s
63700K .......... .......... .......... .......... .......... 23% 182M 8s
63750K .......... .......... .......... .......... .......... 24% 199M 8s
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63850K .......... .......... .......... .......... .......... 24% 178M 8s
63900K .......... .......... .......... .......... .......... 24% 186M 8s
63950K .......... .......... .......... .......... .......... 24% 204M 8s
64000K .......... .......... .......... .......... .......... 24% 229M 8s
64050K .......... .......... .......... .......... .......... 24% 220M 8s
64100K .......... .......... .......... .......... .......... 24% 159M 8s
64150K .......... .......... .......... .......... .......... 24% 186M 8s
64200K .......... .......... .......... .......... .......... 24% 169M 8s
64250K .......... .......... .......... .......... .......... 24% 231M 8s
64300K .......... .......... .......... .......... .......... 24% 230M 8s
64350K .......... .......... .......... .......... .......... 24% 193M 8s
64400K .......... .......... .......... .......... .......... 24% 203M 8s
64450K .......... .......... .......... .......... .......... 24% 178M 8s
64500K .......... .......... .......... .......... .......... 24% 734K 8s
64550K .......... .......... .......... .......... .......... 24% 141M 8s
64600K .......... .......... .......... .......... .......... 24% 136M 8s
64650K .......... .......... .......... .......... .......... 24% 66.0M 8s
64700K .......... .......... .......... .......... .......... 24% 92.1M 8s
64750K .......... .......... .......... .......... .......... 24% 221M 8s
64800K .......... .......... .......... .......... .......... 24% 122M 8s
64850K .......... .......... .......... .......... .......... 24% 133M 8s
64900K .......... .......... .......... .......... .......... 24% 172M 8s
64950K .......... .......... .......... .......... .......... 24% 163M 8s
65000K .......... .......... .......... .......... .......... 24% 166M 8s
65050K .......... .......... .......... .......... .......... 24% 130M 8s
65100K .......... .......... .......... .......... .......... 24% 136M 8s
65150K .......... .......... .......... .......... .......... 24% 171M 8s
65200K .......... .......... .......... .......... .......... 24% 148M 8s
65250K .......... .......... .......... .......... .......... 24% 218M 8s
65300K .......... .......... .......... .......... .......... 24% 168M 8s
65350K .......... .......... .......... .......... .......... 24% 198M 8s
65400K .......... .......... .......... .......... .......... 24% 83.5M 8s
65450K .......... .......... .......... .......... .......... 24% 189M 8s
65500K .......... .......... .......... .......... .......... 24% 6.69M 8s
65550K .......... .......... .......... .......... .......... 24% 53.0M 8s
65600K .......... .......... .......... .......... .......... 24% 212M 8s
65650K .......... .......... .......... .......... .......... 24% 258M 8s
65700K .......... .......... .......... .......... .......... 24% 31.5M 8s
65750K .......... .......... .......... .......... .......... 24% 13.9M 8s
65800K .......... .......... .......... .......... .......... 24% 16.2M 8s
65850K .......... .......... .......... .......... .......... 24% 15.5M 8s
65900K .......... .......... .......... .......... .......... 24% 17.2M 8s
65950K .......... .......... .......... .......... .......... 24% 16.5M 8s
66000K .......... .......... .......... .......... .......... 24% 184M 8s
66050K .......... .......... .......... .......... .......... 24% 201M 8s
66100K .......... .......... .......... .......... .......... 24% 176M 8s
66150K .......... .......... .......... .......... .......... 24% 198M 8s
66200K .......... .......... .......... .......... .......... 24% 182M 8s
66250K .......... .......... .......... .......... .......... 24% 205M 8s
66300K .......... .......... .......... .......... .......... 24% 194M 8s
66350K .......... .......... .......... .......... .......... 24% 176M 8s
66400K .......... .......... .......... .......... .......... 25% 219M 8s
66450K .......... .......... .......... .......... .......... 25% 182M 8s
66500K .......... .......... .......... .......... .......... 25% 222M 8s
66550K .......... .......... .......... .......... .......... 25% 4.55M 8s
66600K .......... .......... .......... .......... .......... 25% 1.94M 8s
66650K .......... .......... .......... .......... .......... 25% 77.8M 8s
66700K .......... .......... .......... .......... .......... 25% 127M 8s
66750K .......... .......... .......... .......... .......... 25% 164M 8s
66800K .......... .......... .......... .......... .......... 25% 181M 8s
66850K .......... .......... .......... .......... .......... 25% 160M 8s
66900K .......... .......... .......... .......... .......... 25% 162M 8s
66950K .......... .......... .......... .......... .......... 25% 114M 8s
67000K .......... .......... .......... .......... .......... 25% 122M 8s
67050K .......... .......... .......... .......... .......... 25% 201M 8s
67100K .......... .......... .......... .......... .......... 25% 148M 8s
67150K .......... .......... .......... .......... .......... 25% 159M 8s
67200K .......... .......... .......... .......... .......... 25% 55.7M 8s
67250K .......... .......... .......... .......... .......... 25% 209M 8s
67300K .......... .......... .......... .......... .......... 25% 200M 8s
67350K .......... .......... .......... .......... .......... 25% 176M 8s
67400K .......... .......... .......... .......... .......... 25% 168M 8s
67450K .......... .......... .......... .......... .......... 25% 178M 8s
67500K .......... .......... .......... .......... .......... 25% 199M 8s
67550K .......... .......... .......... .......... .......... 25% 14.4M 8s
67600K .......... .......... .......... .......... .......... 25% 2.17M 8s
67650K .......... .......... .......... .......... .......... 25% 119M 8s
67700K .......... .......... .......... .......... .......... 25% 191M 8s
67750K .......... .......... .......... .......... .......... 25% 228M 8s
67800K .......... .......... .......... .......... .......... 25% 28.9M 8s
67850K .......... .......... .......... .......... .......... 25% 7.20M 8s
67900K .......... .......... .......... .......... .......... 25% 180M 8s
67950K .......... .......... .......... .......... .......... 25% 171M 8s
68000K .......... .......... .......... .......... .......... 25% 212M 8s
68050K .......... .......... .......... .......... .......... 25% 67.6M 8s
68100K .......... .......... .......... .......... .......... 25% 171M 8s
68150K .......... .......... .......... .......... .......... 25% 16.2M 8s
68200K .......... .......... .......... .......... .......... 25% 172M 8s
68250K .......... .......... .......... .......... .......... 25% 223M 8s
68300K .......... .......... .......... .......... .......... 25% 220M 8s
68350K .......... .......... .......... .......... .......... 25% 192M 8s
68400K .......... .......... .......... .......... .......... 25% 226M 8s
68450K .......... .......... .......... .......... .......... 25% 198M 8s
68500K .......... .......... .......... .......... .......... 25% 225M 8s
68550K .......... .......... .......... .......... .......... 25% 225M 8s
68600K .......... .......... .......... .......... .......... 25% 913K 8s
68650K .......... .......... .......... .......... .......... 25% 79.4M 8s
68700K .......... .......... .......... .......... .......... 25% 180M 8s
68750K .......... .......... .......... .......... .......... 25% 206M 8s
68800K .......... .......... .......... .......... .......... 25% 198M 8s
68850K .......... .......... .......... .......... .......... 25% 170M 8s
68900K .......... .......... .......... .......... .......... 25% 198M 8s
68950K .......... .......... .......... .......... .......... 25% 73.3M 8s
69000K .......... .......... .......... .......... .......... 25% 185M 8s
69050K .......... .......... .......... .......... .......... 26% 149M 8s
69100K .......... .......... .......... .......... .......... 26% 113M 8s
69150K .......... .......... .......... .......... .......... 26% 128M 8s
69200K .......... .......... .......... .......... .......... 26% 196M 8s
69250K .......... .......... .......... .......... .......... 26% 121M 8s
69300K .......... .......... .......... .......... .......... 26% 56.9M 8s
69350K .......... .......... .......... .......... .......... 26% 120M 8s
69400K .......... .......... .......... .......... .......... 26% 236M 8s
69450K .......... .......... .......... .......... .......... 26% 141M 8s
69500K .......... .......... .......... .......... .......... 26% 125M 8s
69550K .......... .......... .......... .......... .......... 26% 189M 8s
69600K .......... .......... .......... .......... .......... 26% 128M 8s
69650K .......... .......... .......... .......... .......... 26% 222M 8s
69700K .......... .......... .......... .......... .......... 26% 168M 8s
69750K .......... .......... .......... .......... .......... 26% 168M 8s
69800K .......... .......... .......... .......... .......... 26% 158M 8s
69850K .......... .......... .......... .......... .......... 26% 155M 8s
69900K .......... .......... .......... .......... .......... 26% 218M 8s
69950K .......... .......... .......... .......... .......... 26% 195M 8s
70000K .......... .......... .......... .......... .......... 26% 227M 8s
70050K .......... .......... .......... .......... .......... 26% 222M 8s
70100K .......... .......... .......... .......... .......... 26% 171M 8s
70150K .......... .......... .......... .......... .......... 26% 223M 8s
70200K .......... .......... .......... .......... .......... 26% 184M 8s
70250K .......... .......... .......... .......... .......... 26% 222M 8s
70300K .......... .......... .......... .......... .......... 26% 216M 8s
70350K .......... .......... .......... .......... .......... 26% 169M 8s
70400K .......... .......... .......... .......... .......... 26% 206M 8s
70450K .......... .......... .......... .......... .......... 26% 199M 8s
70500K .......... .......... .......... .......... .......... 26% 230M 8s
70550K .......... .......... .......... .......... .......... 26% 133M 8s
70600K .......... .......... .......... .......... .......... 26% 111M 8s
70650K .......... .......... .......... .......... .......... 26% 7.27M 8s
70700K .......... .......... .......... .......... .......... 26% 92.7M 8s
70750K .......... .......... .......... .......... .......... 26% 130M 8s
70800K .......... .......... .......... .......... .......... 26% 199M 8s
70850K .......... .......... .......... .......... .......... 26% 78.9M 8s
70900K .......... .......... .......... .......... .......... 26% 144M 8s
70950K .......... .......... .......... .......... .......... 26% 188M 8s
71000K .......... .......... .......... .......... .......... 26% 4.72M 8s
71050K .......... .......... .......... .......... .......... 26% 74.8M 8s
71100K .......... .......... .......... .......... .......... 26% 59.4M 8s
71150K .......... .......... .......... .......... .......... 26% 207M 8s
71200K .......... .......... .......... .......... .......... 26% 192M 8s
71250K .......... .......... .......... .......... .......... 26% 195M 8s
71300K .......... .......... .......... .......... .......... 26% 206M 8s
71350K .......... .......... .......... .......... .......... 26% 190M 8s
71400K .......... .......... .......... .......... .......... 26% 203M 8s
71450K .......... .......... .......... .......... .......... 26% 168M 8s
71500K .......... .......... .......... .......... .......... 26% 212M 8s
71550K .......... .......... .......... .......... .......... 26% 208M 8s
71600K .......... .......... .......... .......... .......... 26% 183M 8s
71650K .......... .......... .......... .......... .......... 26% 4.27M 8s
71700K .......... .......... .......... .......... .......... 27% 59.3M 8s
71750K .......... .......... .......... .......... .......... 27% 89.9M 8s
71800K .......... .......... .......... .......... .......... 27% 128M 8s
71850K .......... .......... .......... .......... .......... 27% 104M 8s
71900K .......... .......... .......... .......... .......... 27% 166M 8s
71950K .......... .......... .......... .......... .......... 27% 169M 8s
72000K .......... .......... .......... .......... .......... 27% 191M 8s
72050K .......... .......... .......... .......... .......... 27% 178M 8s
72100K .......... .......... .......... .......... .......... 27% 166M 8s
72150K .......... .......... .......... .......... .......... 27% 224M 8s
72200K .......... .......... .......... .......... .......... 27% 162M 8s
72250K .......... .......... .......... .......... .......... 27% 175M 8s
72300K .......... .......... .......... .......... .......... 27% 230M 8s
72350K .......... .......... .......... .......... .......... 27% 208M 8s
72400K .......... .......... .......... .......... .......... 27% 238M 8s
72450K .......... .......... .......... .......... .......... 27% 201M 8s
72500K .......... .......... .......... .......... .......... 27% 113M 8s
72550K .......... .......... .......... .......... .......... 27% 176M 8s
72600K .......... .......... .......... .......... .......... 27% 144M 8s
72650K .......... .......... .......... .......... .......... 27% 225M 8s
72700K .......... .......... .......... .......... .......... 27% 16.0M 8s
72750K .......... .......... .......... .......... .......... 27% 78.9M 8s
72800K .......... .......... .......... .......... .......... 27% 119M 8s
72850K .......... .......... .......... .......... .......... 27% 127M 8s
72900K .......... .......... .......... .......... .......... 27% 186M 8s
72950K .......... .......... .......... .......... .......... 27% 170M 8s
73000K .......... .......... .......... .......... .......... 27% 212M 8s
73050K .......... .......... .......... .......... .......... 27% 193M 8s
73100K .......... .......... .......... .......... .......... 27% 161M 8s
73150K .......... .......... .......... .......... .......... 27% 191M 8s
73200K .......... .......... .......... .......... .......... 27% 19.6M 8s
73250K .......... .......... .......... .......... .......... 27% 199M 8s
73300K .......... .......... .......... .......... .......... 27% 227M 8s
73350K .......... .......... .......... .......... .......... 27% 199M 8s
73400K .......... .......... .......... .......... .......... 27% 228M 8s
73450K .......... .......... .......... .......... .......... 27% 190M 8s
73500K .......... .......... .......... .......... .......... 27% 215M 8s
73550K .......... .......... .......... .......... .......... 27% 218M 8s
73600K .......... .......... .......... .......... .......... 27% 194M 8s
73650K .......... .......... .......... .......... .......... 27% 227M 8s
73700K .......... .......... .......... .......... .......... 27% 1.30M 8s
73750K .......... .......... .......... .......... .......... 27% 189M 8s
73800K .......... .......... .......... .......... .......... 27% 185M 8s
73850K .......... .......... .......... .......... .......... 27% 58.6M 8s
73900K .......... .......... .......... .......... .......... 27% 50.7M 8s
73950K .......... .......... .......... .......... .......... 27% 59.5M 8s
74000K .......... .......... .......... .......... .......... 27% 199M 8s
74050K .......... .......... .......... .......... .......... 27% 212M 8s
74100K .......... .......... .......... .......... .......... 27% 148M 8s
74150K .......... .......... .......... .......... .......... 27% 227M 8s
74200K .......... .......... .......... .......... .......... 27% 118M 8s
74250K .......... .......... .......... .......... .......... 27% 215M 8s
74300K .......... .......... .......... .......... .......... 27% 219M 8s
74350K .......... .......... .......... .......... .......... 27% 3.01M 8s
74400K .......... .......... .......... .......... .......... 28% 44.3M 8s
74450K .......... .......... .......... .......... .......... 28% 61.0M 8s
74500K .......... .......... .......... .......... .......... 28% 56.5M 8s
74550K .......... .......... .......... .......... .......... 28% 78.0M 8s
74600K .......... .......... .......... .......... .......... 28% 83.0M 8s
74650K .......... .......... .......... .......... .......... 28% 77.0M 8s
74700K .......... .......... .......... .......... .......... 28% 85.1M 8s
74750K .......... .......... .......... .......... .......... 28% 1.39M 8s
74800K .......... .......... .......... .......... .......... 28% 210M 8s
74850K .......... .......... .......... .......... .......... 28% 82.5M 8s
74900K .......... .......... .......... .......... .......... 28% 3.17M 8s
74950K .......... .......... .......... .......... .......... 28% 189M 8s
75000K .......... .......... .......... .......... .......... 28% 231M 8s
75050K .......... .......... .......... .......... .......... 28% 92.5M 8s
75100K .......... .......... .......... .......... .......... 28% 34.5M 8s
75150K .......... .......... .......... .......... .......... 28% 51.0M 8s
75200K .......... .......... .......... .......... .......... 28% 45.2M 8s
75250K .......... .......... .......... .......... .......... 28% 111M 8s
75300K .......... .......... .......... .......... .......... 28% 79.1M 8s
75350K .......... .......... .......... .......... .......... 28% 189M 8s
75400K .......... .......... .......... .......... .......... 28% 216M 8s
75450K .......... .......... .......... .......... .......... 28% 3.32M 8s
75500K .......... .......... .......... .......... .......... 28% 69.2M 8s
75550K .......... .......... .......... .......... .......... 28% 93.4M 8s
75600K .......... .......... .......... .......... .......... 28% 38.7M 8s
75650K .......... .......... .......... .......... .......... 28% 73.0M 8s
75700K .......... .......... .......... .......... .......... 28% 105M 8s
75750K .......... .......... .......... .......... .......... 28% 42.6M 8s
75800K .......... .......... .......... .......... .......... 28% 97.3M 8s
75850K .......... .......... .......... .......... .......... 28% 156M 8s
75900K .......... .......... .......... .......... .......... 28% 62.8M 8s
75950K .......... .......... .......... .......... .......... 28% 3.30M 8s
76000K .......... .......... .......... .......... .......... 28% 125M 8s
76050K .......... .......... .......... .......... .......... 28% 235M 8s
76100K .......... .......... .......... .......... .......... 28% 34.3M 8s
76150K .......... .......... .......... .......... .......... 28% 71.2M 8s
76200K .......... .......... .......... .......... .......... 28% 142M 8s
76250K .......... .......... .......... .......... .......... 28% 206M 8s
76300K .......... .......... .......... .......... .......... 28% 221M 8s
76350K .......... .......... .......... .......... .......... 28% 51.5M 8s
76400K .......... .......... .......... .......... .......... 28% 141M 8s
76450K .......... .......... .......... .......... .......... 28% 192M 8s
76500K .......... .......... .......... .......... .......... 28% 2.70M 8s
76550K .......... .......... .......... .......... .......... 28% 74.2M 8s
76600K .......... .......... .......... .......... .......... 28% 167M 8s
76650K .......... .......... .......... .......... .......... 28% 153M 8s
76700K .......... .......... .......... .......... .......... 28% 184M 8s
76750K .......... .......... .......... .......... .......... 28% 211M 8s
76800K .......... .......... .......... .......... .......... 28% 129M 8s
76850K .......... .......... .......... .......... .......... 28% 158M 8s
76900K .......... .......... .......... .......... .......... 28% 210M 8s
76950K .......... .......... .......... .......... .......... 28% 189M 8s
77000K .......... .......... .......... .......... .......... 28% 217M 8s
77050K .......... .......... .......... .......... .......... 29% 2.64M 8s
77100K .......... .......... .......... .......... .......... 29% 189M 8s
77150K .......... .......... .......... .......... .......... 29% 40.7M 8s
77200K .......... .......... .......... .......... .......... 29% 132M 8s
77250K .......... .......... .......... .......... .......... 29% 228M 8s
77300K .......... .......... .......... .......... .......... 29% 233M 8s
77350K .......... .......... .......... .......... .......... 29% 207M 8s
77400K .......... .......... .......... .......... .......... 29% 96.5M 8s
77450K .......... .......... .......... .......... .......... 29% 128M 8s
77500K .......... .......... .......... .......... .......... 29% 224M 8s
77550K .......... .......... .......... .......... .......... 29% 226M 8s
77600K .......... .......... .......... .......... .......... 29% 3.12M 8s
77650K .......... .......... .......... .......... .......... 29% 199M 8s
77700K .......... .......... .......... .......... .......... 29% 178M 8s
77750K .......... .......... .......... .......... .......... 29% 202M 8s
77800K .......... .......... .......... .......... .......... 29% 133M 8s
77850K .......... .......... .......... .......... .......... 29% 194M 8s
77900K .......... .......... .......... .......... .......... 29% 229M 8s
77950K .......... .......... .......... .......... .......... 29% 201M 8s
78000K .......... .......... .......... .......... .......... 29% 220M 8s
78050K .......... .......... .......... .......... .......... 29% 222M 8s
78100K .......... .......... .......... .......... .......... 29% 202M 8s
78150K .......... .......... .......... .......... .......... 29% 1.86M 8s
78200K .......... .......... .......... .......... .......... 29% 79.9M 8s
78250K .......... .......... .......... .......... .......... 29% 152M 8s
78300K .......... .......... .......... .......... .......... 29% 201M 8s
78350K .......... .......... .......... .......... .......... 29% 188M 8s
78400K .......... .......... .......... .......... .......... 29% 123M 8s
78450K .......... .......... .......... .......... .......... 29% 172M 8s
78500K .......... .......... .......... .......... .......... 29% 107M 8s
78550K .......... .......... .......... .......... .......... 29% 222M 8s
78600K .......... .......... .......... .......... .......... 29% 45.3M 8s
78650K .......... .......... .......... .......... .......... 29% 124M 8s
78700K .......... .......... .......... .......... .......... 29% 1.44M 8s
78750K .......... .......... .......... .......... .......... 29% 228M 8s
78800K .......... .......... .......... .......... .......... 29% 196M 8s
78850K .......... .......... .......... .......... .......... 29% 75.2M 8s
78900K .......... .......... .......... .......... .......... 29% 133M 8s
78950K .......... .......... .......... .......... .......... 29% 162M 8s
79000K .......... .......... .......... .......... .......... 29% 193M 8s
79050K .......... .......... .......... .......... .......... 29% 186M 8s
79100K .......... .......... .......... .......... .......... 29% 154M 8s
79150K .......... .......... .......... .......... .......... 29% 188M 8s
79200K .......... .......... .......... .......... .......... 29% 3.34M 8s
79250K .......... .......... .......... .......... .......... 29% 170M 8s
79300K .......... .......... .......... .......... .......... 29% 183M 8s
79350K .......... .......... .......... .......... .......... 29% 159M 8s
79400K .......... .......... .......... .......... .......... 29% 180M 8s
79450K .......... .......... .......... .......... .......... 29% 157M 8s
79500K .......... .......... .......... .......... .......... 29% 217M 8s
79550K .......... .......... .......... .......... .......... 29% 220M 8s
79600K .......... .......... .......... .......... .......... 29% 195M 8s
79650K .......... .......... .......... .......... .......... 29% 158M 8s
79700K .......... .......... .......... .......... .......... 30% 176M 8s
79750K .......... .......... .......... .......... .......... 30% 3.38M 8s
79800K .......... .......... .......... .......... .......... 30% 202M 8s
79850K .......... .......... .......... .......... .......... 30% 71.7M 8s
79900K .......... .......... .......... .......... .......... 30% 169M 8s
79950K .......... .......... .......... .......... .......... 30% 200M 8s
80000K .......... .......... .......... .......... .......... 30% 217M 7s
80050K .......... .......... .......... .......... .......... 30% 224M 7s
80100K .......... .......... .......... .......... .......... 30% 178M 7s
80150K .......... .......... .......... .......... .......... 30% 227M 7s
80200K .......... .......... .......... .......... .......... 30% 193M 7s
80250K .......... .......... .......... .......... .......... 30% 218M 7s
80300K .......... .......... .......... .......... .......... 30% 3.21M 7s
80350K .......... .......... .......... .......... .......... 30% 189M 7s
80400K .......... .......... .......... .......... .......... 30% 203M 7s
80450K .......... .......... .......... .......... .......... 30% 82.5M 7s
80500K .......... .......... .......... .......... .......... 30% 228M 7s
80550K .......... .......... .......... .......... .......... 30% 88.8M 7s
80600K .......... .......... .......... .......... .......... 30% 55.9M 7s
80650K .......... .......... .......... .......... .......... 30% 181M 7s
80700K .......... .......... .......... .......... .......... 30% 160M 7s
80750K .......... .......... .......... .......... .......... 30% 131M 7s
80800K .......... .......... .......... .......... .......... 30% 143M 7s
80850K .......... .......... .......... .......... .......... 30% 341K 8s
80900K .......... .......... .......... .......... .......... 30% 57.8M 8s
80950K .......... .......... .......... .......... .......... 30% 189M 8s
81000K .......... .......... .......... .......... .......... 30% 126M 8s
81050K .......... .......... .......... .......... .......... 30% 208M 8s
81100K .......... .......... .......... .......... .......... 30% 196M 8s
81150K .......... .......... .......... .......... .......... 30% 231M 8s
81200K .......... .......... .......... .......... .......... 30% 202M 8s
81250K .......... .......... .......... .......... .......... 30% 199M 8s
81300K .......... .......... .......... .......... .......... 30% 87.5M 8s
81350K .......... .......... .......... .......... .......... 30% 49.6M 8s
81400K .......... .......... .......... .......... .......... 30% 1.10M 8s
81450K .......... .......... .......... .......... .......... 30% 74.5M 8s
81500K .......... .......... .......... .......... .......... 30% 84.9M 8s
81550K .......... .......... .......... .......... .......... 30% 61.4M 8s
81600K .......... .......... .......... .......... .......... 30% 35.5M 8s
81650K .......... .......... .......... .......... .......... 30% 55.4M 8s
81700K .......... .......... .......... .......... .......... 30% 38.5M 8s
81750K .......... .......... .......... .......... .......... 30% 152M 8s
81800K .......... .......... .......... .......... .......... 30% 188M 8s
81850K .......... .......... .......... .......... .......... 30% 120M 8s
81900K .......... .......... .......... .......... .......... 30% 54.1M 8s
81950K .......... .......... .......... .......... .......... 30% 3.25M 8s
82000K .......... .......... .......... .......... .......... 30% 59.7M 8s
82050K .......... .......... .......... .......... .......... 30% 196M 8s
82100K .......... .......... .......... .......... .......... 30% 168M 8s
82150K .......... .......... .......... .......... .......... 30% 218M 8s
82200K .......... .......... .......... .......... .......... 30% 195M 8s
82250K .......... .......... .......... .......... .......... 30% 108M 8s
82300K .......... .......... .......... .......... .......... 30% 167M 8s
82350K .......... .......... .......... .......... .......... 31% 185M 8s
82400K .......... .......... .......... .......... .......... 31% 196M 8s
82450K .......... .......... .......... .......... .......... 31% 178M 8s
82500K .......... .......... .......... .......... .......... 31% 3.20M 8s
82550K .......... .......... .......... .......... .......... 31% 222M 8s
82600K .......... .......... .......... .......... .......... 31% 194M 8s
82650K .......... .......... .......... .......... .......... 31% 229M 8s
82700K .......... .......... .......... .......... .......... 31% 194M 8s
82750K .......... .......... .......... .......... .......... 31% 228M 8s
82800K .......... .......... .......... .......... .......... 31% 228M 8s
82850K .......... .......... .......... .......... .......... 31% 195M 8s
82900K .......... .......... .......... .......... .......... 31% 125M 8s
82950K .......... .......... .......... .......... .......... 31% 186M 8s
83000K .......... .......... .......... .......... .......... 31% 212M 8s
83050K .......... .......... .......... .......... .......... 31% 3.25M 8s
83100K .......... .......... .......... .......... .......... 31% 184M 8s
83150K .......... .......... .......... .......... .......... 31% 199M 8s
83200K .......... .......... .......... .......... .......... 31% 190M 8s
83250K .......... .......... .......... .......... .......... 31% 223M 8s
83300K .......... .......... .......... .......... .......... 31% 224M 8s
83350K .......... .......... .......... .......... .......... 31% 184M 8s
83400K .......... .......... .......... .......... .......... 31% 223M 8s
83450K .......... .......... .......... .......... .......... 31% 191M 8s
83500K .......... .......... .......... .......... .......... 31% 221M 8s
83550K .......... .......... .......... .......... .......... 31% 221M 8s
83600K .......... .......... .......... .......... .......... 31% 3.35M 8s
83650K .......... .......... .......... .......... .......... 31% 214M 8s
83700K .......... .......... .......... .......... .......... 31% 201M 8s
83750K .......... .......... .......... .......... .......... 31% 230M 8s
83800K .......... .......... .......... .......... .......... 31% 128M 8s
83850K .......... .......... .......... .......... .......... 31% 179M 8s
83900K .......... .......... .......... .......... .......... 31% 219M 8s
83950K .......... .......... .......... .......... .......... 31% 117M 8s
84000K .......... .......... .......... .......... .......... 31% 124M 8s
84050K .......... .......... .......... .......... .......... 31% 219M 8s
84100K .......... .......... .......... .......... .......... 31% 193M 8s
84150K .......... .......... .......... .......... .......... 31% 3.03M 8s
84200K .......... .......... .......... .......... .......... 31% 188M 8s
84250K .......... .......... .......... .......... .......... 31% 79.8M 8s
84300K .......... .......... .......... .......... .......... 31% 170M 8s
84350K .......... .......... .......... .......... .......... 31% 144M 8s
84400K .......... .......... .......... .......... .......... 31% 160M 8s
84450K .......... .......... .......... .......... .......... 31% 118M 8s
84500K .......... .......... .......... .......... .......... 31% 162M 8s
84550K .......... .......... .......... .......... .......... 31% 177M 8s
84600K .......... .......... .......... .......... .......... 31% 156M 8s
84650K .......... .......... .......... .......... .......... 31% 131M 8s
84700K .......... .......... .......... .......... .......... 31% 2.78M 8s
84750K .......... .......... .......... .......... .......... 31% 182M 8s
84800K .......... .......... .......... .......... .......... 31% 202M 8s
84850K .......... .......... .......... .......... .......... 31% 71.3M 8s
84900K .......... .......... .......... .......... .......... 31% 23.6M 8s
84950K .......... .......... .......... .......... .......... 31% 9.85M 8s
85000K .......... .......... .......... .......... .......... 32% 178M 8s
85050K .......... .......... .......... .......... .......... 32% 209M 8s
85100K .......... .......... .......... .......... .......... 32% 196M 8s
85150K .......... .......... .......... .......... .......... 32% 226M 8s
85200K .......... .......... .......... .......... .......... 32% 2.20M 8s
85250K .......... .......... .......... .......... .......... 32% 171M 8s
85300K .......... .......... .......... .......... .......... 32% 219M 8s
85350K .......... .......... .......... .......... .......... 32% 172M 8s
85400K .......... .......... .......... .......... .......... 32% 158M 8s
85450K .......... .......... .......... .......... .......... 32% 188M 8s
85500K .......... .......... .......... .......... .......... 32% 223M 8s
85550K .......... .......... .......... .......... .......... 32% 199M 8s
85600K .......... .......... .......... .......... .......... 32% 187M 8s
85650K .......... .......... .......... .......... .......... 32% 166M 8s
85700K .......... .......... .......... .......... .......... 32% 191M 8s
85750K .......... .......... .......... .......... .......... 32% 208M 8s
85800K .......... .......... .......... .......... .......... 32% 2.01M 8s
85850K .......... .......... .......... .......... .......... 32% 25.6M 8s
85900K .......... .......... .......... .......... .......... 32% 206M 8s
85950K .......... .......... .......... .......... .......... 32% 198M 8s
86000K .......... .......... .......... .......... .......... 32% 335K 8s
86050K .......... .......... .......... .......... .......... 32% 211M 8s
86100K .......... .......... .......... .......... .......... 32% 191M 8s
86150K .......... .......... .......... .......... .......... 32% 66.6M 8s
86200K .......... .......... .......... .......... .......... 32% 161M 8s
86250K .......... .......... .......... .......... .......... 32% 212M 8s
86300K .......... .......... .......... .......... .......... 32% 208M 8s
86350K .......... .......... .......... .......... .......... 32% 163M 8s
86400K .......... .......... .......... .......... .......... 32% 203M 8s
86450K .......... .......... .......... .......... .......... 32% 152M 8s
86500K .......... .......... .......... .......... .......... 32% 174M 8s
86550K .......... .......... .......... .......... .......... 32% 180M 8s
86600K .......... .......... .......... .......... .......... 32% 135M 8s
86650K .......... .......... .......... .......... .......... 32% 120M 8s
86700K .......... .......... .......... .......... .......... 32% 181M 8s
86750K .......... .......... .......... .......... .......... 32% 84.6M 8s
86800K .......... .......... .......... .......... .......... 32% 204M 8s
86850K .......... .......... .......... .......... .......... 32% 166M 8s
86900K .......... .......... .......... .......... .......... 32% 186M 8s
86950K .......... .......... .......... .......... .......... 32% 151M 8s
87000K .......... .......... .......... .......... .......... 32% 72.3M 8s
87050K .......... .......... .......... .......... .......... 32% 78.5M 8s
87100K .......... .......... .......... .......... .......... 32% 2.47M 8s
87150K .......... .......... .......... .......... .......... 32% 157M 8s
87200K .......... .......... .......... .......... .......... 32% 106M 8s
87250K .......... .......... .......... .......... .......... 32% 105M 8s
87300K .......... .......... .......... .......... .......... 32% 48.1M 8s
87350K .......... .......... .......... .......... .......... 32% 140M 8s
87400K .......... .......... .......... .......... .......... 32% 96.7M 8s
87450K .......... .......... .......... .......... .......... 32% 141M 8s
87500K .......... .......... .......... .......... .......... 32% 227M 8s
87550K .......... .......... .......... .......... .......... 32% 219M 8s
87600K .......... .......... .......... .......... .......... 32% 193M 8s
87650K .......... .......... .......... .......... .......... 33% 2.70M 8s
87700K .......... .......... .......... .......... .......... 33% 173M 8s
87750K .......... .......... .......... .......... .......... 33% 86.0M 8s
87800K .......... .......... .......... .......... .......... 33% 227M 8s
87850K .......... .......... .......... .......... .......... 33% 34.1M 8s
87900K .......... .......... .......... .......... .......... 33% 221M 8s
87950K .......... .......... .......... .......... .......... 33% 193M 8s
88000K .......... .......... .......... .......... .......... 33% 230M 8s
88050K .......... .......... .......... .......... .......... 33% 115M 8s
88100K .......... .......... .......... .......... .......... 33% 134M 8s
88150K .......... .......... .......... .......... .......... 33% 144M 8s
88200K .......... .......... .......... .......... .......... 33% 1.77M 8s
88250K .......... .......... .......... .......... .......... 33% 223M 8s
88300K .......... .......... .......... .......... .......... 33% 224M 8s
88350K .......... .......... .......... .......... .......... 33% 202M 8s
88400K .......... .......... .......... .......... .......... 33% 217M 8s
88450K .......... .......... .......... .......... .......... 33% 114M 8s
88500K .......... .......... .......... .......... .......... 33% 229M 8s
88550K .......... .......... .......... .......... .......... 33% 224M 8s
88600K .......... .......... .......... .......... .......... 33% 206M 8s
88650K .......... .......... .......... .......... .......... 33% 211M 8s
88700K .......... .......... .......... .......... .......... 33% 158M 8s
88750K .......... .......... .......... .......... .......... 33% 3.43M 8s
88800K .......... .......... .......... .......... .......... 33% 227M 8s
88850K .......... .......... .......... .......... .......... 33% 199M 8s
88900K .......... .......... .......... .......... .......... 33% 235M 8s
88950K .......... .......... .......... .......... .......... 33% 118M 8s
89000K .......... .......... .......... .......... .......... 33% 229M 8s
89050K .......... .......... .......... .......... .......... 33% 136M 8s
89100K .......... .......... .......... .......... .......... 33% 183M 8s
89150K .......... .......... .......... .......... .......... 33% 82.6M 8s
89200K .......... .......... .......... .......... .......... 33% 143M 8s
89250K .......... .......... .......... .......... .......... 33% 208M 8s
89300K .......... .......... .......... .......... .......... 33% 3.18M 8s
89350K .......... .......... .......... .......... .......... 33% 201M 8s
89400K .......... .......... .......... .......... .......... 33% 244M 8s
89450K .......... .......... .......... .......... .......... 33% 213M 8s
89500K .......... .......... .......... .......... .......... 33% 239M 8s
89550K .......... .......... .......... .......... .......... 33% 239M 8s
89600K .......... .......... .......... .......... .......... 33% 200M 8s
89650K .......... .......... .......... .......... .......... 33% 235M 8s
89700K .......... .......... .......... .......... .......... 33% 203M 8s
89750K .......... .......... .......... .......... .......... 33% 237M 8s
89800K .......... .......... .......... .......... .......... 33% 229M 8s
89850K .......... .......... .......... .......... .......... 33% 3.39M 8s
89900K .......... .......... .......... .......... .......... 33% 225M 8s
89950K .......... .......... .......... .......... .......... 33% 206M 8s
90000K .......... .......... .......... .......... .......... 33% 229M 8s
90050K .......... .......... .......... .......... .......... 33% 151M 8s
90100K .......... .......... .......... .......... .......... 33% 126M 8s
90150K .......... .......... .......... .......... .......... 33% 207M 8s
90200K .......... .......... .......... .......... .......... 33% 187M 8s
90250K .......... .......... .......... .......... .......... 33% 210M 8s
90300K .......... .......... .......... .......... .......... 34% 155M 8s
90350K .......... .......... .......... .......... .......... 34% 174M 8s
90400K .......... .......... .......... .......... .......... 34% 3.35M 8s
90450K .......... .......... .......... .......... .......... 34% 193M 8s
90500K .......... .......... .......... .......... .......... 34% 242M 8s
90550K .......... .......... .......... .......... .......... 34% 239M 8s
90600K .......... .......... .......... .......... .......... 34% 151M 8s
90650K .......... .......... .......... .......... .......... 34% 248M 8s
90700K .......... .......... .......... .......... .......... 34% 202M 8s
90750K .......... .......... .......... .......... .......... 34% 224M 8s
90800K .......... .......... .......... .......... .......... 34% 242M 8s
90850K .......... .......... .......... .......... .......... 34% 144M 8s
90900K .......... .......... .......... .......... .......... 34% 184M 8s
90950K .......... .......... .......... .......... .......... 34% 3.05M 8s
91000K .......... .......... .......... .......... .......... 34% 207M 8s
91050K .......... .......... .......... .......... .......... 34% 65.6M 8s
91100K .......... .......... .......... .......... .......... 34% 138M 8s
91150K .......... .......... .......... .......... .......... 34% 229M 8s
91200K .......... .......... .......... .......... .......... 34% 199M 8s
91250K .......... .......... .......... .......... .......... 34% 179M 8s
91300K .......... .......... .......... .......... .......... 34% 234M 8s
91350K .......... .......... .......... .......... .......... 34% 4.53M 8s
91400K .......... .......... .......... .......... .......... 34% 124M 8s
91450K .......... .......... .......... .......... .......... 34% 194M 8s
91500K .......... .......... .......... .......... .......... 34% 231M 8s
91550K .......... .......... .......... .......... .......... 34% 239M 8s
91600K .......... .......... .......... .......... .......... 34% 195M 8s
91650K .......... .......... .......... .......... .......... 34% 231M 8s
91700K .......... .......... .......... .......... .......... 34% 204M 8s
91750K .......... .......... .......... .......... .......... 34% 233M 7s
91800K .......... .......... .......... .......... .......... 34% 231M 7s
91850K .......... .......... .......... .......... .......... 34% 204M 7s
91900K .......... .......... .......... .......... .......... 34% 3.13M 8s
91950K .......... .......... .......... .......... .......... 34% 187M 8s
92000K .......... .......... .......... .......... .......... 34% 236M 7s
92050K .......... .......... .......... .......... .......... 34% 239M 7s
92100K .......... .......... .......... .......... .......... 34% 208M 7s
92150K .......... .......... .......... .......... .......... 34% 79.0M 7s
92200K .......... .......... .......... .......... .......... 34% 87.5M 7s
92250K .......... .......... .......... .......... .......... 34% 198M 7s
92300K .......... .......... .......... .......... .......... 34% 202M 7s
92350K .......... .......... .......... .......... .......... 34% 195M 7s
92400K .......... .......... .......... .......... .......... 34% 222M 7s
92450K .......... .......... .......... .......... .......... 34% 3.15M 7s
92500K .......... .......... .......... .......... .......... 34% 109M 7s
92550K .......... .......... .......... .......... .......... 34% 67.5M 7s
92600K .......... .......... .......... .......... .......... 34% 153M 7s
92650K .......... .......... .......... .......... .......... 34% 170M 7s
92700K .......... .......... .......... .......... .......... 34% 115M 7s
92750K .......... .......... .......... .......... .......... 34% 213M 7s
92800K .......... .......... .......... .......... .......... 34% 223M 7s
92850K .......... .......... .......... .......... .......... 34% 184M 7s
92900K .......... .......... .......... .......... .......... 34% 210M 7s
92950K .......... .......... .......... .......... .......... 34% 89.9M 7s
93000K .......... .......... .......... .......... .......... 35% 3.32M 7s
93050K .......... .......... .......... .......... .......... 35% 173M 7s
93100K .......... .......... .......... .......... .......... 35% 92.7M 7s
93150K .......... .......... .......... .......... .......... 35% 83.6M 7s
93200K .......... .......... .......... .......... .......... 35% 74.0M 7s
93250K .......... .......... .......... .......... .......... 35% 201M 7s
93300K .......... .......... .......... .......... .......... 35% 146M 7s
93350K .......... .......... .......... .......... .......... 35% 182M 7s
93400K .......... .......... .......... .......... .......... 35% 173M 7s
93450K .......... .......... .......... .......... .......... 35% 119M 7s
93500K .......... .......... .......... .......... .......... 35% 162M 7s
93550K .......... .......... .......... .......... .......... 35% 3.35M 7s
93600K .......... .......... .......... .......... .......... 35% 153M 7s
93650K .......... .......... .......... .......... .......... 35% 228M 7s
93700K .......... .......... .......... .......... .......... 35% 188M 7s
93750K .......... .......... .......... .......... .......... 35% 230M 7s
93800K .......... .......... .......... .......... .......... 35% 230M 7s
93850K .......... .......... .......... .......... .......... 35% 184M 7s
93900K .......... .......... .......... .......... .......... 35% 217M 7s
93950K .......... .......... .......... .......... .......... 35% 186M 7s
94000K .......... .......... .......... .......... .......... 35% 216M 7s
94050K .......... .......... .......... .......... .......... 35% 224M 7s
94100K .......... .......... .......... .......... .......... 35% 3.14M 7s
94150K .......... .......... .......... .......... .......... 35% 86.0M 7s
94200K .......... .......... .......... .......... .......... 35% 84.6M 7s
94250K .......... .......... .......... .......... .......... 35% 198M 7s
94300K .......... .......... .......... .......... .......... 35% 213M 7s
94350K .......... .......... .......... .......... .......... 35% 171M 7s
94400K .......... .......... .......... .......... .......... 35% 155M 7s
94450K .......... .......... .......... .......... .......... 35% 130M 7s
94500K .......... .......... .......... .......... .......... 35% 201M 7s
94550K .......... .......... .......... .......... .......... 35% 133M 7s
94600K .......... .......... .......... .......... .......... 35% 160M 7s
94650K .......... .......... .......... .......... .......... 35% 167M 7s
94700K .......... .......... .......... .......... .......... 35% 3.18M 7s
94750K .......... .......... .......... .......... .......... 35% 94.1M 7s
94800K .......... .......... .......... .......... .......... 35% 206M 7s
94850K .......... .......... .......... .......... .......... 35% 192M 7s
94900K .......... .......... .......... .......... .......... 35% 229M 7s
94950K .......... .......... .......... .......... .......... 35% 182M 7s
95000K .......... .......... .......... .......... .......... 35% 234M 7s
95050K .......... .......... .......... .......... .......... 35% 109M 7s
95100K .......... .......... .......... .......... .......... 35% 158M 7s
95150K .......... .......... .......... .......... .......... 35% 192M 7s
95200K .......... .......... .......... .......... .......... 35% 90.8M 7s
95250K .......... .......... .......... .......... .......... 35% 3.07M 7s
95300K .......... .......... .......... .......... .......... 35% 176M 7s
95350K .......... .......... .......... .......... .......... 35% 132M 7s
95400K .......... .......... .......... .......... .......... 35% 172M 7s
95450K .......... .......... .......... .......... .......... 35% 144M 7s
95500K .......... .......... .......... .......... .......... 35% 63.5M 7s
95550K .......... .......... .......... .......... .......... 35% 75.5M 7s
95600K .......... .......... .......... .......... .......... 35% 97.1M 7s
95650K .......... .......... .......... .......... .......... 36% 109M 7s
95700K .......... .......... .......... .......... .......... 36% 111M 7s
95750K .......... .......... .......... .......... .......... 36% 66.3M 7s
95800K .......... .......... .......... .......... .......... 36% 2.52M 7s
95850K .......... .......... .......... .......... .......... 36% 154M 7s
95900K .......... .......... .......... .......... .......... 36% 222M 7s
95950K .......... .......... .......... .......... .......... 36% 201M 7s
96000K .......... .......... .......... .......... .......... 36% 235M 7s
96050K .......... .......... .......... .......... .......... 36% 219M 7s
96100K .......... .......... .......... .......... .......... 36% 158M 7s
96150K .......... .......... .......... .......... .......... 36% 217M 7s
96200K .......... .......... .......... .......... .......... 36% 198M 7s
96250K .......... .......... .......... .......... .......... 36% 2.71M 7s
96300K .......... .......... .......... .......... .......... 36% 171M 7s
96350K .......... .......... .......... .......... .......... 36% 2.24M 7s
96400K .......... .......... .......... .......... .......... 36% 84.5M 7s
96450K .......... .......... .......... .......... .......... 36% 183M 7s
96500K .......... .......... .......... .......... .......... 36% 153M 7s
96550K .......... .......... .......... .......... .......... 36% 84.6M 7s
96600K .......... .......... .......... .......... .......... 36% 195M 7s
96650K .......... .......... .......... .......... .......... 36% 231M 7s
96700K .......... .......... .......... .......... .......... 36% 197M 7s
96750K .......... .......... .......... .......... .......... 36% 231M 7s
96800K .......... .......... .......... .......... .......... 36% 227M 7s
96850K .......... .......... .......... .......... .......... 36% 195M 7s
96900K .......... .......... .......... .......... .......... 36% 1.08M 7s
96950K .......... .......... .......... .......... .......... 36% 131M 7s
97000K .......... .......... .......... .......... .......... 36% 195M 7s
97050K .......... .......... .......... .......... .......... 36% 105M 7s
97100K .......... .......... .......... .......... .......... 36% 97.5M 7s
97150K .......... .......... .......... .......... .......... 36% 86.1M 7s
97200K .......... .......... .......... .......... .......... 36% 145M 7s
97250K .......... .......... .......... .......... .......... 36% 119M 7s
97300K .......... .......... .......... .......... .......... 36% 114M 7s
97350K .......... .......... .......... .......... .......... 36% 142M 7s
97400K .......... .......... .......... .......... .......... 36% 148M 7s
97450K .......... .......... .......... .......... .......... 36% 168M 7s
97500K .......... .......... .......... .......... .......... 36% 3.09M 7s
97550K .......... .......... .......... .......... .......... 36% 49.0M 7s
97600K .......... .......... .......... .......... .......... 36% 27.1M 7s
97650K .......... .......... .......... .......... .......... 36% 64.0M 7s
97700K .......... .......... .......... .......... .......... 36% 43.2M 7s
97750K .......... .......... .......... .......... .......... 36% 122M 7s
97800K .......... .......... .......... .......... .......... 36% 176M 7s
97850K .......... .......... .......... .......... .......... 36% 149M 7s
97900K .......... .......... .......... .......... .......... 36% 131M 7s
97950K .......... .......... .......... .......... .......... 36% 168M 7s
98000K .......... .......... .......... .......... .......... 36% 178M 7s
98050K .......... .......... .......... .......... .......... 36% 3.09M 7s
98100K .......... .......... .......... .......... .......... 36% 138M 7s
98150K .......... .......... .......... .......... .......... 36% 189M 7s
98200K .......... .......... .......... .......... .......... 36% 163M 7s
98250K .......... .......... .......... .......... .......... 36% 189M 7s
98300K .......... .......... .......... .......... .......... 37% 105M 7s
98350K .......... .......... .......... .......... .......... 37% 100M 7s
98400K .......... .......... .......... .......... .......... 37% 85.7M 7s
98450K .......... .......... .......... .......... .......... 37% 122M 7s
98500K .......... .......... .......... .......... .......... 37% 72.3M 7s
98550K .......... .......... .......... .......... .......... 37% 208M 7s
98600K .......... .......... .......... .......... .......... 37% 3.03M 7s
98650K .......... .......... .......... .......... .......... 37% 227M 7s
98700K .......... .......... .......... .......... .......... 37% 205M 7s
98750K .......... .......... .......... .......... .......... 37% 124M 7s
98800K .......... .......... .......... .......... .......... 37% 178M 7s
98850K .......... .......... .......... .......... .......... 37% 162M 7s
98900K .......... .......... .......... .......... .......... 37% 193M 7s
98950K .......... .......... .......... .......... .......... 37% 176M 7s
99000K .......... .......... .......... .......... .......... 37% 198M 7s
99050K .......... .......... .......... .......... .......... 37% 202M 7s
99100K .......... .......... .......... .......... .......... 37% 174M 7s
99150K .......... .......... .......... .......... .......... 37% 2.73M 7s
99200K .......... .......... .......... .......... .......... 37% 172M 7s
99250K .......... .......... .......... .......... .......... 37% 226M 7s
99300K .......... .......... .......... .......... .......... 37% 143M 7s
99350K .......... .......... .......... .......... .......... 37% 186M 7s
99400K .......... .......... .......... .......... .......... 37% 162M 7s
99450K .......... .......... .......... .......... .......... 37% 197M 7s
99500K .......... .......... .......... .......... .......... 37% 234M 7s
99550K .......... .......... .......... .......... .......... 37% 230M 7s
99600K .......... .......... .......... .......... .......... 37% 195M 7s
99650K .......... .......... .......... .......... .......... 37% 221M 7s
99700K .......... .......... .......... .......... .......... 37% 196M 7s
99750K .......... .......... .......... .......... .......... 37% 2.25M 7s
99800K .......... .......... .......... .......... .......... 37% 211M 7s
99850K .......... .......... .......... .......... .......... 37% 192M 7s
99900K .......... .......... .......... .......... .......... 37% 235M 7s
99950K .......... .......... .......... .......... .......... 37% 187M 7s
100000K .......... .......... .......... .......... .......... 37% 233M 7s
100050K .......... .......... .......... .......... .......... 37% 261M 7s
100100K .......... .......... .......... .......... .......... 37% 201M 7s
100150K .......... .......... .......... .......... .......... 37% 241M 7s
100200K .......... .......... .......... .......... .......... 37% 206M 7s
100250K .......... .......... .......... .......... .......... 37% 238M 7s
100300K .......... .......... .......... .......... .......... 37% 1.56M 7s
100350K .......... .......... .......... .......... .......... 37% 89.4M 7s
100400K .......... .......... .......... .......... .......... 37% 91.6M 7s
100450K .......... .......... .......... .......... .......... 37% 190M 7s
100500K .......... .......... .......... .......... .......... 37% 231M 7s
100550K .......... .......... .......... .......... .......... 37% 230M 7s
100600K .......... .......... .......... .......... .......... 37% 200M 7s
100650K .......... .......... .......... .......... .......... 37% 220M 7s
100700K .......... .......... .......... .......... .......... 37% 194M 7s
100750K .......... .......... .......... .......... .......... 37% 227M 7s
100800K .......... .......... .......... .......... .......... 37% 227M 7s
100850K .......... .......... .......... .......... .......... 37% 1.41M 7s
100900K .......... .......... .......... .......... .......... 37% 214M 7s
100950K .......... .......... .......... .......... .......... 38% 173M 7s
101000K .......... .......... .......... .......... .......... 38% 205M 7s
101050K .......... .......... .......... .......... .......... 38% 187M 7s
101100K .......... .......... .......... .......... .......... 38% 171M 7s
101150K .......... .......... .......... .......... .......... 38% 122M 7s
101200K .......... .......... .......... .......... .......... 38% 124M 7s
101250K .......... .......... .......... .......... .......... 38% 231M 7s
101300K .......... .......... .......... .......... .......... 38% 230M 7s
101350K .......... .......... .......... .......... .......... 38% 126M 7s
101400K .......... .......... .......... .......... .......... 38% 218M 7s
101450K .......... .......... .......... .......... .......... 38% 2.41M 7s
101500K .......... .......... .......... .......... .......... 38% 130M 7s
101550K .......... .......... .......... .......... .......... 38% 164M 7s
101600K .......... .......... .......... .......... .......... 38% 147M 7s
101650K .......... .......... .......... .......... .......... 38% 155M 7s
101700K .......... .......... .......... .......... .......... 38% 109M 7s
101750K .......... .......... .......... .......... .......... 38% 89.4M 7s
101800K .......... .......... .......... .......... .......... 38% 103M 7s
101850K .......... .......... .......... .......... .......... 38% 151M 7s
101900K .......... .......... .......... .......... .......... 38% 191M 7s
101950K .......... .......... .......... .......... .......... 38% 153M 7s
102000K .......... .......... .......... .......... .......... 38% 3.03M 7s
102050K .......... .......... .......... .......... .......... 38% 200M 7s
102100K .......... .......... .......... .......... .......... 38% 114M 7s
102150K .......... .......... .......... .......... .......... 38% 120M 7s
102200K .......... .......... .......... .......... .......... 38% 71.1M 7s
102250K .......... .......... .......... .......... .......... 38% 93.9M 7s
102300K .......... .......... .......... .......... .......... 38% 155M 7s
102350K .......... .......... .......... .......... .......... 38% 119M 7s
102400K .......... .......... .......... .......... .......... 38% 2.48M 7s
102450K .......... .......... .......... .......... .......... 38% 71.1M 7s
102500K .......... .......... .......... .......... .......... 38% 104M 7s
102550K .......... .......... .......... .......... .......... 38% 3.19M 7s
102600K .......... .......... .......... .......... .......... 38% 84.2M 7s
102650K .......... .......... .......... .......... .......... 38% 106M 7s
102700K .......... .......... .......... .......... .......... 38% 113M 7s
102750K .......... .......... .......... .......... .......... 38% 73.2M 7s
102800K .......... .......... .......... .......... .......... 38% 162M 7s
102850K .......... .......... .......... .......... .......... 38% 102M 7s
102900K .......... .......... .......... .......... .......... 38% 129M 7s
102950K .......... .......... .......... .......... .......... 38% 109M 7s
103000K .......... .......... .......... .......... .......... 38% 131M 7s
103050K .......... .......... .......... .......... .......... 38% 195M 7s
103100K .......... .......... .......... .......... .......... 38% 182M 7s
103150K .......... .......... .......... .......... .......... 38% 3.30M 7s
103200K .......... .......... .......... .......... .......... 38% 140M 7s
103250K .......... .......... .......... .......... .......... 38% 111M 7s
103300K .......... .......... .......... .......... .......... 38% 96.5M 7s
103350K .......... .......... .......... .......... .......... 38% 69.5M 7s
103400K .......... .......... .......... .......... .......... 38% 21.1M 7s
103450K .......... .......... .......... .......... .......... 38% 113M 7s
103500K .......... .......... .......... .......... .......... 38% 29.2M 7s
103550K .......... .......... .......... .......... .......... 38% 61.1M 7s
103600K .......... .......... .......... .......... .......... 39% 72.7M 7s
103650K .......... .......... .......... .......... .......... 39% 173M 7s
103700K .......... .......... .......... .......... .......... 39% 2.83M 7s
103750K .......... .......... .......... .......... .......... 39% 191M 7s
103800K .......... .......... .......... .......... .......... 39% 214M 7s
103850K .......... .......... .......... .......... .......... 39% 173M 7s
103900K .......... .......... .......... .......... .......... 39% 182M 7s
103950K .......... .......... .......... .......... .......... 39% 80.2M 7s
104000K .......... .......... .......... .......... .......... 39% 160M 7s
104050K .......... .......... .......... .......... .......... 39% 167M 7s
104100K .......... .......... .......... .......... .......... 39% 162M 7s
104150K .......... .......... .......... .......... .......... 39% 173M 7s
104200K .......... .......... .......... .......... .......... 39% 162M 7s
104250K .......... .......... .......... .......... .......... 39% 2.78M 7s
104300K .......... .......... .......... .......... .......... 39% 182M 7s
104350K .......... .......... .......... .......... .......... 39% 182M 7s
104400K .......... .......... .......... .......... .......... 39% 52.1M 7s
104450K .......... .......... .......... .......... .......... 39% 85.5M 7s
104500K .......... .......... .......... .......... .......... 39% 210M 7s
104550K .......... .......... .......... .......... .......... 39% 117M 7s
104600K .......... .......... .......... .......... .......... 39% 192M 7s
104650K .......... .......... .......... .......... .......... 39% 48.2M 7s
104700K .......... .......... .......... .......... .......... 39% 115M 7s
104750K .......... .......... .......... .......... .......... 39% 192M 7s
104800K .......... .......... .......... .......... .......... 39% 153M 7s
104850K .......... .......... .......... .......... .......... 39% 2.99M 7s
104900K .......... .......... .......... .......... .......... 39% 209M 7s
104950K .......... .......... .......... .......... .......... 39% 78.6M 7s
105000K .......... .......... .......... .......... .......... 39% 218M 7s
105050K .......... .......... .......... .......... .......... 39% 134M 7s
105100K .......... .......... .......... .......... .......... 39% 71.0M 7s
105150K .......... .......... .......... .......... .......... 39% 198M 7s
105200K .......... .......... .......... .......... .......... 39% 191M 7s
105250K .......... .......... .......... .......... .......... 39% 214M 7s
105300K .......... .......... .......... .......... .......... 39% 4.77M 7s
105350K .......... .......... .......... .......... .......... 39% 182M 7s
105400K .......... .......... .......... .......... .......... 39% 2.49M 7s
105450K .......... .......... .......... .......... .......... 39% 123M 7s
105500K .......... .......... .......... .......... .......... 39% 217M 7s
105550K .......... .......... .......... .......... .......... 39% 220M 7s
105600K .......... .......... .......... .......... .......... 39% 208M 7s
105650K .......... .......... .......... .......... .......... 39% 263M 7s
105700K .......... .......... .......... .......... .......... 39% 3.78M 7s
105750K .......... .......... .......... .......... .......... 39% 211M 7s
105800K .......... .......... .......... .......... .......... 39% 225M 7s
105850K .......... .......... .......... .......... .......... 39% 199M 7s
105900K .......... .......... .......... .......... .......... 39% 229M 7s
105950K .......... .......... .......... .......... .......... 39% 200M 7s
106000K .......... .......... .......... .......... .......... 39% 1.92M 7s
106050K .......... .......... .......... .......... .......... 39% 235M 7s
106100K .......... .......... .......... .......... .......... 39% 203M 7s
106150K .......... .......... .......... .......... .......... 39% 235M 7s
106200K .......... .......... .......... .......... .......... 39% 195M 7s
106250K .......... .......... .......... .......... .......... 40% 92.0M 7s
106300K .......... .......... .......... .......... .......... 40% 81.9M 7s
106350K .......... .......... .......... .......... .......... 40% 168M 7s
106400K .......... .......... .......... .......... .......... 40% 196M 7s
106450K .......... .......... .......... .......... .......... 40% 126M 7s
106500K .......... .......... .......... .......... .......... 40% 191M 7s
106550K .......... .......... .......... .......... .......... 40% 2.71M 7s
106600K .......... .......... .......... .......... .......... 40% 144M 7s
106650K .......... .......... .......... .......... .......... 40% 221M 7s
106700K .......... .......... .......... .......... .......... 40% 126M 7s
106750K .......... .......... .......... .......... .......... 40% 214M 7s
106800K .......... .......... .......... .......... .......... 40% 211M 7s
106850K .......... .......... .......... .......... .......... 40% 189M 7s
106900K .......... .......... .......... .......... .......... 40% 204M 7s
106950K .......... .......... .......... .......... .......... 40% 20.0M 7s
107000K .......... .......... .......... .......... .......... 40% 188M 7s
107050K .......... .......... .......... .......... .......... 40% 208M 7s
107100K .......... .......... .......... .......... .......... 40% 185M 7s
107150K .......... .......... .......... .......... .......... 40% 2.92M 7s
107200K .......... .......... .......... .......... .......... 40% 102M 7s
107250K .......... .......... .......... .......... .......... 40% 91.8M 7s
107300K .......... .......... .......... .......... .......... 40% 149M 7s
107350K .......... .......... .......... .......... .......... 40% 146M 7s
107400K .......... .......... .......... .......... .......... 40% 126M 7s
107450K .......... .......... .......... .......... .......... 40% 85.2M 7s
107500K .......... .......... .......... .......... .......... 40% 97.5M 7s
107550K .......... .......... .......... .......... .......... 40% 149M 7s
107600K .......... .......... .......... .......... .......... 40% 156M 7s
107650K .......... .......... .......... .......... .......... 40% 192M 7s
107700K .......... .......... .......... .......... .......... 40% 2.78M 7s
107750K .......... .......... .......... .......... .......... 40% 141M 7s
107800K .......... .......... .......... .......... .......... 40% 130M 7s
107850K .......... .......... .......... .......... .......... 40% 137M 7s
107900K .......... .......... .......... .......... .......... 40% 207M 7s
107950K .......... .......... .......... .......... .......... 40% 181M 7s
108000K .......... .......... .......... .......... .......... 40% 210M 7s
108050K .......... .......... .......... .......... .......... 40% 198M 7s
108100K .......... .......... .......... .......... .......... 40% 140M 7s
108150K .......... .......... .......... .......... .......... 40% 174M 7s
108200K .......... .......... .......... .......... .......... 40% 155M 7s
108250K .......... .......... .......... .......... .......... 40% 203M 7s
108300K .......... .......... .......... .......... .......... 40% 2.45M 7s
108350K .......... .......... .......... .......... .......... 40% 69.6M 7s
108400K .......... .......... .......... .......... .......... 40% 163M 7s
108450K .......... .......... .......... .......... .......... 40% 181M 7s
108500K .......... .......... .......... .......... .......... 40% 23.2M 7s
108550K .......... .......... .......... .......... .......... 40% 195M 7s
108600K .......... .......... .......... .......... .......... 40% 193M 7s
108650K .......... .......... .......... .......... .......... 40% 172M 7s
108700K .......... .......... .......... .......... .......... 40% 191M 7s
108750K .......... .......... .......... .......... .......... 40% 220M 7s
108800K .......... .......... .......... .......... .......... 40% 219M 7s
108850K .......... .......... .......... .......... .......... 40% 2.63M 7s
108900K .......... .......... .......... .......... .......... 41% 95.7M 7s
108950K .......... .......... .......... .......... .......... 41% 135M 7s
109000K .......... .......... .......... .......... .......... 41% 95.0M 7s
109050K .......... .......... .......... .......... .......... 41% 102M 7s
109100K .......... .......... .......... .......... .......... 41% 131M 7s
109150K .......... .......... .......... .......... .......... 41% 61.3M 7s
109200K .......... .......... .......... .......... .......... 41% 180M 7s
109250K .......... .......... .......... .......... .......... 41% 217M 7s
109300K .......... .......... .......... .......... .......... 41% 184M 7s
109350K .......... .......... .......... .......... .......... 41% 66.3M 7s
109400K .......... .......... .......... .......... .......... 41% 149M 7s
109450K .......... .......... .......... .......... .......... 41% 2.92M 7s
109500K .......... .......... .......... .......... .......... 41% 97.9M 7s
109550K .......... .......... .......... .......... .......... 41% 115M 7s
109600K .......... .......... .......... .......... .......... 41% 137M 7s
109650K .......... .......... .......... .......... .......... 41% 140M 7s
109700K .......... .......... .......... .......... .......... 41% 105M 7s
109750K .......... .......... .......... .......... .......... 41% 136M 7s
109800K .......... .......... .......... .......... .......... 41% 143M 7s
109850K .......... .......... .......... .......... .......... 41% 98.0M 7s
109900K .......... .......... .......... .......... .......... 41% 166M 7s
109950K .......... .......... .......... .......... .......... 41% 184M 7s
110000K .......... .......... .......... .......... .......... 41% 2.76M 7s
110050K .......... .......... .......... .......... .......... 41% 137M 7s
110100K .......... .......... .......... .......... .......... 41% 168M 7s
110150K .......... .......... .......... .......... .......... 41% 238M 7s
110200K .......... .......... .......... .......... .......... 41% 198M 7s
110250K .......... .......... .......... .......... .......... 41% 228M 7s
110300K .......... .......... .......... .......... .......... 41% 242M 7s
110350K .......... .......... .......... .......... .......... 41% 212M 7s
110400K .......... .......... .......... .......... .......... 41% 242M 7s
110450K .......... .......... .......... .......... .......... 41% 205M 7s
110500K .......... .......... .......... .......... .......... 41% 247M 7s
110550K .......... .......... .......... .......... .......... 41% 138M 7s
110600K .......... .......... .......... .......... .......... 41% 2.98M 7s
110650K .......... .......... .......... .......... .......... 41% 210M 7s
110700K .......... .......... .......... .......... .......... 41% 154M 7s
110750K .......... .......... .......... .......... .......... 41% 168M 7s
110800K .......... .......... .......... .......... .......... 41% 217M 7s
110850K .......... .......... .......... .......... .......... 41% 174M 7s
110900K .......... .......... .......... .......... .......... 41% 210M 7s
110950K .......... .......... .......... .......... .......... 41% 200M 7s
111000K .......... .......... .......... .......... .......... 41% 237M 7s
111050K .......... .......... .......... .......... .......... 41% 158M 7s
111100K .......... .......... .......... .......... .......... 41% 200M 7s
111150K .......... .......... .......... .......... .......... 41% 226M 7s
111200K .......... .......... .......... .......... .......... 41% 3.02M 7s
111250K .......... .......... .......... .......... .......... 41% 109M 7s
111300K .......... .......... .......... .......... .......... 41% 157M 7s
111350K .......... .......... .......... .......... .......... 41% 127M 7s
111400K .......... .......... .......... .......... .......... 41% 133M 7s
111450K .......... .......... .......... .......... .......... 41% 34.9M 7s
111500K .......... .......... .......... .......... .......... 41% 229M 7s
111550K .......... .......... .......... .......... .......... 41% 235M 7s
111600K .......... .......... .......... .......... .......... 42% 1.56M 7s
111650K .......... .......... .......... .......... .......... 42% 214M 7s
111700K .......... .......... .......... .......... .......... 42% 155M 7s
111750K .......... .......... .......... .......... .......... 42% 2.96M 7s
111800K .......... .......... .......... .......... .......... 42% 237M 7s
111850K .......... .......... .......... .......... .......... 42% 213M 7s
111900K .......... .......... .......... .......... .......... 42% 247M 7s
111950K .......... .......... .......... .......... .......... 42% 212M 7s
112000K .......... .......... .......... .......... .......... 42% 241M 7s
112050K .......... .......... .......... .......... .......... 42% 245M 7s
112100K .......... .......... .......... .......... .......... 42% 211M 7s
112150K .......... .......... .......... .......... .......... 42% 243M 7s
112200K .......... .......... .......... .......... .......... 42% 212M 7s
112250K .......... .......... .......... .......... .......... 42% 242M 7s
112300K .......... .......... .......... .......... .......... 42% 241M 7s
112350K .......... .......... .......... .......... .......... 42% 3.02M 7s
112400K .......... .......... .......... .......... .......... 42% 205M 7s
112450K .......... .......... .......... .......... .......... 42% 163M 7s
112500K .......... .......... .......... .......... .......... 42% 196M 7s
112550K .......... .......... .......... .......... .......... 42% 224M 7s
112600K .......... .......... .......... .......... .......... 42% 112M 7s
112650K .......... .......... .......... .......... .......... 42% 216M 7s
112700K .......... .......... .......... .......... .......... 42% 122M 7s
112750K .......... .......... .......... .......... .......... 42% 209M 7s
112800K .......... .......... .......... .......... .......... 42% 211M 7s
112850K .......... .......... .......... .......... .......... 42% 194M 7s
112900K .......... .......... .......... .......... .......... 42% 2.95M 7s
112950K .......... .......... .......... .......... .......... 42% 83.9M 7s
113000K .......... .......... .......... .......... .......... 42% 63.2M 7s
113050K .......... .......... .......... .......... .......... 42% 62.8M 7s
113100K .......... .......... .......... .......... .......... 42% 56.6M 7s
113150K .......... .......... .......... .......... .......... 42% 83.9M 7s
113200K .......... .......... .......... .......... .......... 42% 150M 7s
113250K .......... .......... .......... .......... .......... 42% 79.4M 7s
113300K .......... .......... .......... .......... .......... 42% 167M 7s
113350K .......... .......... .......... .......... .......... 42% 163M 7s
113400K .......... .......... .......... .......... .......... 42% 167M 7s
113450K .......... .......... .......... .......... .......... 42% 139M 7s
113500K .......... .......... .......... .......... .......... 42% 2.92M 7s
113550K .......... .......... .......... .......... .......... 42% 204M 7s
113600K .......... .......... .......... .......... .......... 42% 142M 7s
113650K .......... .......... .......... .......... .......... 42% 109M 7s
113700K .......... .......... .......... .......... .......... 42% 127M 7s
113750K .......... .......... .......... .......... .......... 42% 203M 7s
113800K .......... .......... .......... .......... .......... 42% 133M 7s
113850K .......... .......... .......... .......... .......... 42% 184M 7s
113900K .......... .......... .......... .......... .......... 42% 225M 7s
113950K .......... .......... .......... .......... .......... 42% 199M 7s
114000K .......... .......... .......... .......... .......... 42% 186M 7s
114050K .......... .......... .......... .......... .......... 42% 135M 7s
114100K .......... .......... .......... .......... .......... 42% 2.65M 7s
114150K .......... .......... .......... .......... .......... 42% 182M 7s
114200K .......... .......... .......... .......... .......... 42% 194M 7s
114250K .......... .......... .......... .......... .......... 43% 173M 7s
114300K .......... .......... .......... .......... .......... 43% 130M 7s
114350K .......... .......... .......... .......... .......... 43% 105M 7s
114400K .......... .......... .......... .......... .......... 43% 205M 7s
114450K .......... .......... .......... .......... .......... 43% 126M 7s
114500K .......... .......... .......... .......... .......... 43% 211M 7s
114550K .......... .......... .......... .......... .......... 43% 221M 7s
114600K .......... .......... .......... .......... .......... 43% 185M 7s
114650K .......... .......... .......... .......... .......... 43% 2.60M 7s
114700K .......... .......... .......... .......... .......... 43% 196M 7s
114750K .......... .......... .......... .......... .......... 43% 122M 7s
114800K .......... .......... .......... .......... .......... 43% 221M 7s
114850K .......... .......... .......... .......... .......... 43% 141M 7s
114900K .......... .......... .......... .......... .......... 43% 221M 7s
114950K .......... .......... .......... .......... .......... 43% 202M 7s
115000K .......... .......... .......... .......... .......... 43% 178M 7s
115050K .......... .......... .......... .......... .......... 43% 214M 7s
115100K .......... .......... .......... .......... .......... 43% 200M 7s
115150K .......... .......... .......... .......... .......... 43% 238M 6s
115200K .......... .......... .......... .......... .......... 43% 191M 6s
115250K .......... .......... .......... .......... .......... 43% 2.84M 7s
115300K .......... .......... .......... .......... .......... 43% 200M 7s
115350K .......... .......... .......... .......... .......... 43% 55.0M 7s
115400K .......... .......... .......... .......... .......... 43% 203M 6s
115450K .......... .......... .......... .......... .......... 43% 168M 6s
115500K .......... .......... .......... .......... .......... 43% 172M 6s
115550K .......... .......... .......... .......... .......... 43% 93.9M 6s
115600K .......... .......... .......... .......... .......... 43% 135M 6s
115650K .......... .......... .......... .......... .......... 43% 121M 6s
115700K .......... .......... .......... .......... .......... 43% 113M 6s
115750K .......... .......... .......... .......... .......... 43% 223M 6s
115800K .......... .......... .......... .......... .......... 43% 37.4M 6s
115850K .......... .......... .......... .......... .......... 43% 773K 7s
115900K .......... .......... .......... .......... .......... 43% 224M 7s
115950K .......... .......... .......... .......... .......... 43% 198M 7s
116000K .......... .......... .......... .......... .......... 43% 152M 7s
116050K .......... .......... .......... .......... .......... 43% 233M 7s
116100K .......... .......... .......... .......... .......... 43% 198M 7s
116150K .......... .......... .......... .......... .......... 43% 220M 7s
116200K .......... .......... .......... .......... .......... 43% 196M 7s
116250K .......... .......... .......... .......... .......... 43% 167M 7s
116300K .......... .......... .......... .......... .......... 43% 215M 6s
116350K .......... .......... .......... .......... .......... 43% 202M 6s
116400K .......... .......... .......... .......... .......... 43% 3.00M 7s
116450K .......... .......... .......... .......... .......... 43% 85.8M 7s
116500K .......... .......... .......... .......... .......... 43% 224M 7s
116550K .......... .......... .......... .......... .......... 43% 230M 6s
116600K .......... .......... .......... .......... .......... 43% 202M 6s
116650K .......... .......... .......... .......... .......... 43% 216M 6s
116700K .......... .......... .......... .......... .......... 43% 128M 6s
116750K .......... .......... .......... .......... .......... 43% 222M 6s
116800K .......... .......... .......... .......... .......... 43% 186M 6s
116850K .......... .......... .......... .......... .......... 43% 184M 6s
116900K .......... .......... .......... .......... .......... 44% 237M 6s
116950K .......... .......... .......... .......... .......... 44% 200M 6s
117000K .......... .......... .......... .......... .......... 44% 2.96M 6s
117050K .......... .......... .......... .......... .......... 44% 219M 6s
117100K .......... .......... .......... .......... .......... 44% 191M 6s
117150K .......... .......... .......... .......... .......... 44% 163M 6s
117200K .......... .......... .......... .......... .......... 44% 182M 6s
117250K .......... .......... .......... .......... .......... 44% 222M 6s
117300K .......... .......... .......... .......... .......... 44% 118M 6s
117350K .......... .......... .......... .......... .......... 44% 105M 6s
117400K .......... .......... .......... .......... .......... 44% 208M 6s
117450K .......... .......... .......... .......... .......... 44% 184M 6s
117500K .......... .......... .......... .......... .......... 44% 223M 6s
117550K .......... .......... .......... .......... .......... 44% 222M 6s
117600K .......... .......... .......... .......... .......... 44% 3.01M 6s
117650K .......... .......... .......... .......... .......... 44% 224M 6s
117700K .......... .......... .......... .......... .......... 44% 192M 6s
117750K .......... .......... .......... .......... .......... 44% 80.3M 6s
117800K .......... .......... .......... .......... .......... 44% 201M 6s
117850K .......... .......... .......... .......... .......... 44% 193M 6s
117900K .......... .......... .......... .......... .......... 44% 225M 6s
117950K .......... .......... .......... .......... .......... 44% 147M 6s
118000K .......... .......... .......... .......... .......... 44% 223M 6s
118050K .......... .......... .......... .......... .......... 44% 228M 6s
118100K .......... .......... .......... .......... .......... 44% 195M 6s
118150K .......... .......... .......... .......... .......... 44% 234M 6s
118200K .......... .......... .......... .......... .......... 44% 2.74M 6s
118250K .......... .......... .......... .......... .......... 44% 209M 6s
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118350K .......... .......... .......... .......... .......... 44% 182M 6s
118400K .......... .......... .......... .......... .......... 44% 227M 6s
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118500K .......... .......... .......... .......... .......... 44% 239M 6s
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118650K .......... .......... .......... .......... .......... 44% 230M 6s
118700K .......... .......... .......... .......... .......... 44% 199M 6s
118750K .......... .......... .......... .......... .......... 44% 2.93M 6s
118800K .......... .......... .......... .......... .......... 44% 3.25M 6s
118850K .......... .......... .......... .......... .......... 44% 161M 6s
118900K .......... .......... .......... .......... .......... 44% 187M 6s
118950K .......... .......... .......... .......... .......... 44% 168M 6s
119000K .......... .......... .......... .......... .......... 44% 131M 6s
119050K .......... .......... .......... .......... .......... 44% 62.5M 6s
119100K .......... .......... .......... .......... .......... 44% 184M 6s
119150K .......... .......... .......... .......... .......... 44% 227M 6s
119200K .......... .......... .......... .......... .......... 44% 196M 6s
119250K .......... .......... .......... .......... .......... 44% 229M 6s
119300K .......... .......... .......... .......... .......... 44% 61.6M 6s
119350K .......... .......... .......... .......... .......... 44% 2.48M 6s
119400K .......... .......... .......... .......... .......... 44% 93.5M 6s
119450K .......... .......... .......... .......... .......... 44% 73.9M 6s
119500K .......... .......... .......... .......... .......... 44% 161M 6s
119550K .......... .......... .......... .......... .......... 45% 227M 6s
119600K .......... .......... .......... .......... .......... 45% 188M 6s
119650K .......... .......... .......... .......... .......... 45% 226M 6s
119700K .......... .......... .......... .......... .......... 45% 186M 6s
119750K .......... .......... .......... .......... .......... 45% 196M 6s
119800K .......... .......... .......... .......... .......... 45% 121M 6s
119850K .......... .......... .......... .......... .......... 45% 131M 6s
119900K .......... .......... .......... .......... .......... 45% 237M 6s
119950K .......... .......... .......... .......... .......... 45% 2.84M 6s
120000K .......... .......... .......... .......... .......... 45% 228M 6s
120050K .......... .......... .......... .......... .......... 45% 226M 6s
120100K .......... .......... .......... .......... .......... 45% 205M 6s
120150K .......... .......... .......... .......... .......... 45% 212M 6s
120200K .......... .......... .......... .......... .......... 45% 184M 6s
120250K .......... .......... .......... .......... .......... 45% 189M 6s
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120550K .......... .......... .......... .......... .......... 45% 2.97M 6s
120600K .......... .......... .......... .......... .......... 45% 162M 6s
120650K .......... .......... .......... .......... .......... 45% 198M 6s
120700K .......... .......... .......... .......... .......... 45% 54.4M 6s
120750K .......... .......... .......... .......... .......... 45% 168M 6s
120800K .......... .......... .......... .......... .......... 45% 86.1M 6s
120850K .......... .......... .......... .......... .......... 45% 23.2M 6s
120900K .......... .......... .......... .......... .......... 45% 61.0M 6s
120950K .......... .......... .......... .......... .......... 45% 176M 6s
121000K .......... .......... .......... .......... .......... 45% 231M 6s
121050K .......... .......... .......... .......... .......... 45% 34.2M 6s
121100K .......... .......... .......... .......... .......... 45% 188M 6s
121150K .......... .......... .......... .......... .......... 45% 2.88M 6s
121200K .......... .......... .......... .......... .......... 45% 198M 6s
121250K .......... .......... .......... .......... .......... 45% 237M 6s
121300K .......... .......... .......... .......... .......... 45% 132M 6s
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121400K .......... .......... .......... .......... .......... 45% 233M 6s
121450K .......... .......... .......... .......... .......... 45% 215M 6s
121500K .......... .......... .......... .......... .......... 45% 252M 6s
121550K .......... .......... .......... .......... .......... 45% 252M 6s
121600K .......... .......... .......... .......... .......... 45% 217M 6s
121650K .......... .......... .......... .......... .......... 45% 173M 6s
121700K .......... .......... .......... .......... .......... 45% 2.99M 6s
121750K .......... .......... .......... .......... .......... 45% 123M 6s
121800K .......... .......... .......... .......... .......... 45% 192M 6s
121850K .......... .......... .......... .......... .......... 45% 60.7M 6s
121900K .......... .......... .......... .......... .......... 45% 218M 6s
121950K .......... .......... .......... .......... .......... 45% 207M 6s
122000K .......... .......... .......... .......... .......... 45% 229M 6s
122050K .......... .......... .......... .......... .......... 45% 154M 6s
122100K .......... .......... .......... .......... .......... 45% 194M 6s
122150K .......... .......... .......... .......... .......... 45% 234M 6s
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122250K .......... .......... .......... .......... .......... 46% 238M 6s
122300K .......... .......... .......... .......... .......... 46% 2.91M 6s
122350K .......... .......... .......... .......... .......... 46% 98.0M 6s
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122500K .......... .......... .......... .......... .......... 46% 149M 6s
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122800K .......... .......... .......... .......... .......... 46% 226M 6s
122850K .......... .......... .......... .......... .......... 46% 74.9M 6s
122900K .......... .......... .......... .......... .......... 46% 2.32M 6s
122950K .......... .......... .......... .......... .......... 46% 161M 6s
123000K .......... .......... .......... .......... .......... 46% 57.3M 6s
123050K .......... .......... .......... .......... .......... 46% 150M 6s
123100K .......... .......... .......... .......... .......... 46% 176M 6s
123150K .......... .......... .......... .......... .......... 46% 34.1M 6s
123200K .......... .......... .......... .......... .......... 46% 109M 6s
123250K .......... .......... .......... .......... .......... 46% 122M 6s
123300K .......... .......... .......... .......... .......... 46% 202M 6s
123350K .......... .......... .......... .......... .......... 46% 162M 6s
123400K .......... .......... .......... .......... .......... 46% 208M 6s
123450K .......... .......... .......... .......... .......... 46% 185M 6s
123500K .......... .......... .......... .......... .......... 46% 2.22M 6s
123550K .......... .......... .......... .......... .......... 46% 202M 6s
123600K .......... .......... .......... .......... .......... 46% 124M 6s
123650K .......... .......... .......... .......... .......... 46% 207M 6s
123700K .......... .......... .......... .......... .......... 46% 195M 6s
123750K .......... .......... .......... .......... .......... 46% 230M 6s
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123850K .......... .......... .......... .......... .......... 46% 138M 6s
123900K .......... .......... .......... .......... .......... 46% 84.5M 6s
123950K .......... .......... .......... .......... .......... 46% 193M 6s
124000K .......... .......... .......... .......... .......... 46% 205M 6s
124050K .......... .......... .......... .......... .......... 46% 159M 6s
124100K .......... .......... .......... .......... .......... 46% 1.25M 6s
124150K .......... .......... .......... .......... .......... 46% 137M 6s
124200K .......... .......... .......... .......... .......... 46% 182M 6s
124250K .......... .......... .......... .......... .......... 46% 142M 6s
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124650K .......... .......... .......... .......... .......... 46% 44.6M 6s
124700K .......... .......... .......... .......... .......... 46% 1.35M 6s
124750K .......... .......... .......... .......... .......... 46% 148M 6s
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124900K .......... .......... .......... .......... .......... 47% 124M 6s
124950K .......... .......... .......... .......... .......... 47% 186M 6s
125000K .......... .......... .......... .......... .......... 47% 213M 6s
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125100K .......... .......... .......... .......... .......... 47% 195M 6s
125150K .......... .......... .......... .......... .......... 47% 227M 6s
125200K .......... .......... .......... .......... .......... 47% 192M 6s
125250K .......... .......... .......... .......... .......... 47% 227M 6s
125300K .......... .......... .......... .......... .......... 47% 2.56M 6s
125350K .......... .......... .......... .......... .......... 47% 108M 6s
125400K .......... .......... .......... .......... .......... 47% 188M 6s
125450K .......... .......... .......... .......... .......... 47% 147M 6s
125500K .......... .......... .......... .......... .......... 47% 188M 6s
125550K .......... .......... .......... .......... .......... 47% 164M 6s
125600K .......... .......... .......... .......... .......... 47% 150M 6s
125650K .......... .......... .......... .......... .......... 47% 178M 6s
125700K .......... .......... .......... .......... .......... 47% 138M 6s
125750K .......... .......... .......... .......... .......... 47% 209M 6s
125800K .......... .......... .......... .......... .......... 47% 213M 6s
125850K .......... .......... .......... .......... .......... 47% 180M 6s
125900K .......... .......... .......... .......... .......... 47% 2.08M 6s
125950K .......... .......... .......... .......... .......... 47% 90.9M 6s
126000K .......... .......... .......... .......... .......... 47% 132M 6s
126050K .......... .......... .......... .......... .......... 47% 205M 6s
126100K .......... .......... .......... .......... .......... 47% 185M 6s
126150K .......... .......... .......... .......... .......... 47% 178M 6s
126200K .......... .......... .......... .......... .......... 47% 123M 6s
126250K .......... .......... .......... .......... .......... 47% 229M 6s
126300K .......... .......... .......... .......... .......... 47% 231M 6s
126350K .......... .......... .......... .......... .......... 47% 197M 6s
126400K .......... .......... .......... .......... .......... 47% 235M 6s
126450K .......... .......... .......... .......... .......... 47% 203M 6s
126500K .......... .......... .......... .......... .......... 47% 1.98M 6s
126550K .......... .......... .......... .......... .......... 47% 212M 6s
126600K .......... .......... .......... .......... .......... 47% 75.6M 6s
126650K .......... .......... .......... .......... .......... 47% 214M 6s
126700K .......... .......... .......... .......... .......... 47% 181M 6s
126750K .......... .......... .......... .......... .......... 47% 206M 6s
126800K .......... .......... .......... .......... .......... 47% 73.3M 6s
126850K .......... .......... .......... .......... .......... 47% 194M 6s
126900K .......... .......... .......... .......... .......... 47% 228M 6s
126950K .......... .......... .......... .......... .......... 47% 51.0M 6s
127000K .......... .......... .......... .......... .......... 47% 220M 6s
127050K .......... .......... .......... .......... .......... 47% 217M 6s
127100K .......... .......... .......... .......... .......... 47% 2.41M 6s
127150K .......... .......... .......... .......... .......... 47% 123M 6s
127200K .......... .......... .......... .......... .......... 47% 178M 6s
127250K .......... .......... .......... .......... .......... 47% 198M 6s
127300K .......... .......... .......... .......... .......... 47% 198M 6s
127350K .......... .......... .......... .......... .......... 47% 171M 6s
127400K .......... .......... .......... .......... .......... 47% 194M 6s
127450K .......... .......... .......... .......... .......... 47% 171M 6s
127500K .......... .......... .......... .......... .......... 47% 200M 6s
127550K .......... .......... .......... .......... .......... 48% 195M 6s
127600K .......... .......... .......... .......... .......... 48% 178M 6s
127650K .......... .......... .......... .......... .......... 48% 201M 6s
127700K .......... .......... .......... .......... .......... 48% 2.69M 6s
127750K .......... .......... .......... .......... .......... 48% 228M 6s
127800K .......... .......... .......... .......... .......... 48% 237M 6s
127850K .......... .......... .......... .......... .......... 48% 202M 6s
127900K .......... .......... .......... .......... .......... 48% 236M 6s
127950K .......... .......... .......... .......... .......... 48% 202M 6s
128000K .......... .......... .......... .......... .......... 48% 128M 6s
128050K .......... .......... .......... .......... .......... 48% 231M 6s
128100K .......... .......... .......... .......... .......... 48% 197M 6s
128150K .......... .......... .......... .......... .......... 48% 234M 6s
128200K .......... .......... .......... .......... .......... 48% 197M 6s
128250K .......... .......... .......... .......... .......... 48% 234M 6s
128300K .......... .......... .......... .......... .......... 48% 2.83M 6s
128350K .......... .......... .......... .......... .......... 48% 131M 6s
128400K .......... .......... .......... .......... .......... 48% 197M 6s
128450K .......... .......... .......... .......... .......... 48% 170M 6s
128500K .......... .......... .......... .......... .......... 48% 193M 6s
128550K .......... .......... .......... .......... .......... 48% 198M 6s
128600K .......... .......... .......... .......... .......... 48% 128M 6s
128650K .......... .......... .......... .......... .......... 48% 190M 6s
128700K .......... .......... .......... .......... .......... 48% 175M 6s
128750K .......... .......... .......... .......... .......... 48% 196M 6s
128800K .......... .......... .......... .......... .......... 48% 137M 6s
128850K .......... .......... .......... .......... .......... 48% 169M 6s
128900K .......... .......... .......... .......... .......... 48% 2.78M 6s
128950K .......... .......... .......... .......... .......... 48% 46.9M 6s
129000K .......... .......... .......... .......... .......... 48% 105M 6s
129050K .......... .......... .......... .......... .......... 48% 228M 6s
129100K .......... .......... .......... .......... .......... 48% 59.3M 6s
129150K .......... .......... .......... .......... .......... 48% 207M 6s
129200K .......... .......... .......... .......... .......... 48% 166M 6s
129250K .......... .......... .......... .......... .......... 48% 190M 6s
129300K .......... .......... .......... .......... .......... 48% 214M 6s
129350K .......... .......... .......... .......... .......... 48% 188M 6s
129400K .......... .......... .......... .......... .......... 48% 216M 6s
129450K .......... .......... .......... .......... .......... 48% 191M 6s
129500K .......... .......... .......... .......... .......... 48% 2.30M 6s
129550K .......... .......... .......... .......... .......... 48% 225M 6s
129600K .......... .......... .......... .......... .......... 48% 174M 6s
129650K .......... .......... .......... .......... .......... 48% 3.50M 6s
129700K .......... .......... .......... .......... .......... 48% 102M 6s
129750K .......... .......... .......... .......... .......... 48% 42.8M 6s
129800K .......... .......... .......... .......... .......... 48% 26.5M 6s
129850K .......... .......... .......... .......... .......... 48% 25.3M 6s
129900K .......... .......... .......... .......... .......... 48% 27.6M 6s
129950K .......... .......... .......... .......... .......... 48% 32.3M 6s
130000K .......... .......... .......... .......... .......... 48% 35.4M 6s
130050K .......... .......... .......... .......... .......... 48% 13.4M 6s
130100K .......... .......... .......... .......... .......... 48% 2.69M 6s
130150K .......... .......... .......... .......... .......... 48% 84.3M 6s
130200K .......... .......... .......... .......... .......... 49% 31.1M 6s
130250K .......... .......... .......... .......... .......... 49% 39.4M 6s
130300K .......... .......... .......... .......... .......... 49% 51.4M 6s
130350K .......... .......... .......... .......... .......... 49% 22.6M 6s
130400K .......... .......... .......... .......... .......... 49% 210M 6s
130450K .......... .......... .......... .......... .......... 49% 192M 6s
130500K .......... .......... .......... .......... .......... 49% 164M 6s
130550K .......... .......... .......... .......... .......... 49% 33.2M 6s
130600K .......... .......... .......... .......... .......... 49% 37.2M 6s
130650K .......... .......... .......... .......... .......... 49% 63.5M 6s
130700K .......... .......... .......... .......... .......... 49% 2.65M 6s
130750K .......... .......... .......... .......... .......... 49% 54.1M 6s
130800K .......... .......... .......... .......... .......... 49% 79.1M 6s
130850K .......... .......... .......... .......... .......... 49% 81.4M 6s
130900K .......... .......... .......... .......... .......... 49% 129M 6s
130950K .......... .......... .......... .......... .......... 49% 132M 6s
131000K .......... .......... .......... .......... .......... 49% 143M 6s
131050K .......... .......... .......... .......... .......... 49% 93.7M 6s
131100K .......... .......... .......... .......... .......... 49% 159M 6s
131150K .......... .......... .......... .......... .......... 49% 186M 6s
131200K .......... .......... .......... .......... .......... 49% 168M 6s
131250K .......... .......... .......... .......... .......... 49% 217M 6s
131300K .......... .......... .......... .......... .......... 49% 1.54M 6s
131350K .......... .......... .......... .......... .......... 49% 111M 6s
131400K .......... .......... .......... .......... .......... 49% 90.4M 6s
131450K .......... .......... .......... .......... .......... 49% 51.6M 6s
131500K .......... .......... .......... .......... .......... 49% 145M 6s
131550K .......... .......... .......... .......... .......... 49% 130M 6s
131600K .......... .......... .......... .......... .......... 49% 112M 6s
131650K .......... .......... .......... .......... .......... 49% 85.7M 6s
131700K .......... .......... .......... .......... .......... 49% 65.7M 6s
131750K .......... .......... .......... .......... .......... 49% 53.2M 6s
131800K .......... .......... .......... .......... .......... 49% 66.6M 6s
131850K .......... .......... .......... .......... .......... 49% 89.1M 6s
131900K .......... .......... .......... .......... .......... 49% 2.33M 6s
131950K .......... .......... .......... .......... .......... 49% 134M 6s
132000K .......... .......... .......... .......... .......... 49% 83.0M 6s
132050K .......... .......... .......... .......... .......... 49% 184M 6s
132100K .......... .......... .......... .......... .......... 49% 72.0M 6s
132150K .......... .......... .......... .......... .......... 49% 141M 6s
132200K .......... .......... .......... .......... .......... 49% 16.7M 6s
132250K .......... .......... .......... .......... .......... 49% 148M 6s
132300K .......... .......... .......... .......... .......... 49% 87.5M 6s
132350K .......... .......... .......... .......... .......... 49% 135M 6s
132400K .......... .......... .......... .......... .......... 49% 148M 6s
132450K .......... .......... .......... .......... .......... 49% 61.6M 6s
132500K .......... .......... .......... .......... .......... 49% 2.77M 6s
132550K .......... .......... .......... .......... .......... 49% 158M 6s
132600K .......... .......... .......... .......... .......... 49% 145M 6s
132650K .......... .......... .......... .......... .......... 49% 148M 6s
132700K .......... .......... .......... .......... .......... 49% 91.8M 6s
132750K .......... .......... .......... .......... .......... 49% 126M 6s
132800K .......... .......... .......... .......... .......... 49% 58.5M 6s
132850K .......... .......... .......... .......... .......... 50% 86.9M 6s
132900K .......... .......... .......... .......... .......... 50% 84.8M 6s
132950K .......... .......... .......... .......... .......... 50% 166M 6s
133000K .......... .......... .......... .......... .......... 50% 202M 6s
133050K .......... .......... .......... .......... .......... 50% 164M 6s
133100K .......... .......... .......... .......... .......... 50% 515K 6s
133150K .......... .......... .......... .......... .......... 50% 2.81M 6s
133200K .......... .......... .......... .......... .......... 50% 192M 6s
133250K .......... .......... .......... .......... .......... 50% 248M 6s
133300K .......... .......... .......... .......... .......... 50% 180M 6s
133350K .......... .......... .......... .......... .......... 50% 204M 6s
133400K .......... .......... .......... .......... .......... 50% 247M 6s
133450K .......... .......... .......... .......... .......... 50% 201M 6s
133500K .......... .......... .......... .......... .......... 50% 242M 6s
133550K .......... .......... .......... .......... .......... 50% 241M 6s
133600K .......... .......... .......... .......... .......... 50% 203M 6s
133650K .......... .......... .......... .......... .......... 50% 166M 6s
133700K .......... .......... .......... .......... .......... 50% 193M 6s
133750K .......... .......... .......... .......... .......... 50% 2.87M 6s
133800K .......... .......... .......... .......... .......... 50% 184M 6s
133850K .......... .......... .......... .......... .......... 50% 172M 6s
133900K .......... .......... .......... .......... .......... 50% 195M 6s
133950K .......... .......... .......... .......... .......... 50% 168M 6s
134000K .......... .......... .......... .......... .......... 50% 191M 6s
134050K .......... .......... .......... .......... .......... 50% 203M 6s
134100K .......... .......... .......... .......... .......... 50% 84.9M 6s
134150K .......... .......... .......... .......... .......... 50% 214M 6s
134200K .......... .......... .......... .......... .......... 50% 130M 6s
134250K .......... .......... .......... .......... .......... 50% 199M 6s
134300K .......... .......... .......... .......... .......... 50% 184M 6s
134350K .......... .......... .......... .......... .......... 50% 2.51M 6s
134400K .......... .......... .......... .......... .......... 50% 210M 6s
134450K .......... .......... .......... .......... .......... 50% 187M 6s
134500K .......... .......... .......... .......... .......... 50% 177M 6s
134550K .......... .......... .......... .......... .......... 50% 217M 6s
134600K .......... .......... .......... .......... .......... 50% 186M 6s
134650K .......... .......... .......... .......... .......... 50% 216M 6s
134700K .......... .......... .......... .......... .......... 50% 195M 6s
134750K .......... .......... .......... .......... .......... 50% 212M 6s
134800K .......... .......... .......... .......... .......... 50% 133M 6s
134850K .......... .......... .......... .......... .......... 50% 180M 6s
134900K .......... .......... .......... .......... .......... 50% 215M 6s
134950K .......... .......... .......... .......... .......... 50% 2.73M 6s
135000K .......... .......... .......... .......... .......... 50% 166M 6s
135050K .......... .......... .......... .......... .......... 50% 124M 6s
135100K .......... .......... .......... .......... .......... 50% 118M 6s
135150K .......... .......... .......... .......... .......... 50% 113M 6s
135200K .......... .......... .......... .......... .......... 50% 181M 6s
135250K .......... .......... .......... .......... .......... 50% 147M 6s
135300K .......... .......... .......... .......... .......... 50% 135M 6s
135350K .......... .......... .......... .......... .......... 50% 133M 6s
135400K .......... .......... .......... .......... .......... 50% 78.4M 6s
135450K .......... .......... .......... .......... .......... 50% 101M 6s
135500K .......... .......... .......... .......... .......... 51% 184M 6s
135550K .......... .......... .......... .......... .......... 51% 2.73M 6s
135600K .......... .......... .......... .......... .......... 51% 82.1M 6s
135650K .......... .......... .......... .......... .......... 51% 128M 6s
135700K .......... .......... .......... .......... .......... 51% 84.5M 6s
135750K .......... .......... .......... .......... .......... 51% 97.3M 6s
135800K .......... .......... .......... .......... .......... 51% 113M 6s
135850K .......... .......... .......... .......... .......... 51% 137M 6s
135900K .......... .......... .......... .......... .......... 51% 161M 6s
135950K .......... .......... .......... .......... .......... 51% 79.0M 6s
136000K .......... .......... .......... .......... .......... 51% 223M 6s
136050K .......... .......... .......... .......... .......... 51% 212M 6s
136100K .......... .......... .......... .......... .......... 51% 111M 6s
136150K .......... .......... .......... .......... .......... 51% 105M 6s
136200K .......... .......... .......... .......... .......... 51% 2.76M 6s
136250K .......... .......... .......... .......... .......... 51% 219M 6s
136300K .......... .......... .......... .......... .......... 51% 163M 6s
136350K .......... .......... .......... .......... .......... 51% 64.4M 6s
136400K .......... .......... .......... .......... .......... 51% 220M 6s
136450K .......... .......... .......... .......... .......... 51% 196M 6s
136500K .......... .......... .......... .......... .......... 51% 97.3M 6s
136550K .......... .......... .......... .......... .......... 51% 234M 6s
136600K .......... .......... .......... .......... .......... 51% 209M 6s
136650K .......... .......... .......... .......... .......... 51% 150M 6s
136700K .......... .......... .......... .......... .......... 51% 190M 6s
136750K .......... .......... .......... .......... .......... 51% 224M 6s
136800K .......... .......... .......... .......... .......... 51% 2.74M 6s
136850K .......... .......... .......... .......... .......... 51% 189M 6s
136900K .......... .......... .......... .......... .......... 51% 217M 6s
136950K .......... .......... .......... .......... .......... 51% 195M 6s
137000K .......... .......... .......... .......... .......... 51% 224M 6s
137050K .......... .......... .......... .......... .......... 51% 224M 6s
137100K .......... .......... .......... .......... .......... 51% 193M 6s
137150K .......... .......... .......... .......... .......... 51% 215M 6s
137200K .......... .......... .......... .......... .......... 51% 27.9M 6s
137250K .......... .......... .......... .......... .......... 51% 132M 6s
137300K .......... .......... .......... .......... .......... 51% 142M 6s
137350K .......... .......... .......... .......... .......... 51% 171M 6s
137400K .......... .......... .......... .......... .......... 51% 2.38M 6s
137450K .......... .......... .......... .......... .......... 51% 8.27M 6s
137500K .......... .......... .......... .......... .......... 51% 82.8M 6s
137550K .......... .......... .......... .......... .......... 51% 223M 6s
137600K .......... .......... .......... .......... .......... 51% 52.4M 6s
137650K .......... .......... .......... .......... .......... 51% 200M 6s
137700K .......... .......... .......... .......... .......... 51% 184M 6s
137750K .......... .......... .......... .......... .......... 51% 55.6M 6s
137800K .......... .......... .......... .......... .......... 51% 159M 6s
137850K .......... .......... .......... .......... .......... 51% 58.9M 6s
137900K .......... .......... .......... .......... .......... 51% 211M 6s
137950K .......... .......... .......... .......... .......... 51% 195M 6s
138000K .......... .......... .......... .......... .......... 51% 1.94M 6s
138050K .......... .......... .......... .......... .......... 51% 177M 6s
138100K .......... .......... .......... .......... .......... 51% 180M 6s
138150K .......... .......... .......... .......... .......... 52% 154M 6s
138200K .......... .......... .......... .......... .......... 52% 107M 6s
138250K .......... .......... .......... .......... .......... 52% 146M 6s
138300K .......... .......... .......... .......... .......... 52% 129M 6s
138350K .......... .......... .......... .......... .......... 52% 100M 6s
138400K .......... .......... .......... .......... .......... 52% 129M 6s
138450K .......... .......... .......... .......... .......... 52% 98.2M 6s
138500K .......... .......... .......... .......... .......... 52% 176M 6s
138550K .......... .......... .......... .......... .......... 52% 152M 6s
138600K .......... .......... .......... .......... .......... 52% 144M 6s
138650K .......... .......... .......... .......... .......... 52% 2.72M 6s
138700K .......... .......... .......... .......... .......... 52% 180M 6s
138750K .......... .......... .......... .......... .......... 52% 106M 6s
138800K .......... .......... .......... .......... .......... 52% 150M 6s
138850K .......... .......... .......... .......... .......... 52% 181M 6s
138900K .......... .......... .......... .......... .......... 52% 211M 6s
138950K .......... .......... .......... .......... .......... 52% 189M 6s
139000K .......... .......... .......... .......... .......... 52% 213M 6s
139050K .......... .......... .......... .......... .......... 52% 211M 6s
139100K .......... .......... .......... .......... .......... 52% 191M 6s
139150K .......... .......... .......... .......... .......... 52% 215M 6s
139200K .......... .......... .......... .......... .......... 52% 171M 6s
139250K .......... .......... .......... .......... .......... 52% 2.73M 6s
139300K .......... .......... .......... .......... .......... 52% 208M 6s
139350K .......... .......... .......... .......... .......... 52% 189M 6s
139400K .......... .......... .......... .......... .......... 52% 96.5M 6s
139450K .......... .......... .......... .......... .......... 52% 184M 6s
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139700K .......... .......... .......... .......... .......... 52% 188M 6s
139750K .......... .......... .......... .......... .......... 52% 224M 6s
139800K .......... .......... .......... .......... .......... 52% 219M 6s
139850K .......... .......... .......... .......... .......... 52% 2.69M 6s
139900K .......... .......... .......... .......... .......... 52% 210M 6s
139950K .......... .......... .......... .......... .......... 52% 186M 6s
140000K .......... .......... .......... .......... .......... 52% 143M 6s
140050K .......... .......... .......... .......... .......... 52% 104M 6s
140100K .......... .......... .......... .......... .......... 52% 192M 6s
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140200K .......... .......... .......... .......... .......... 52% 66.4M 6s
140250K .......... .......... .......... .......... .......... 52% 90.4M 6s
140300K .......... .......... .......... .......... .......... 52% 207M 6s
140350K .......... .......... .......... .......... .......... 52% 185M 6s
140400K .......... .......... .......... .......... .......... 52% 208M 5s
140450K .......... .......... .......... .......... .......... 52% 1.73M 6s
140500K .......... .......... .......... .......... .......... 52% 174M 6s
140550K .......... .......... .......... .......... .......... 52% 215M 6s
140600K .......... .......... .......... .......... .......... 52% 180M 6s
140650K .......... .......... .......... .......... .......... 52% 161M 6s
140700K .......... .......... .......... .......... .......... 52% 186M 5s
140750K .......... .......... .......... .......... .......... 52% 220M 5s
140800K .......... .......... .......... .......... .......... 53% 219M 5s
140850K .......... .......... .......... .......... .......... 53% 184M 5s
140900K .......... .......... .......... .......... .......... 53% 2.67M 5s
140950K .......... .......... .......... .......... .......... 53% 176M 5s
141000K .......... .......... .......... .......... .......... 53% 108M 5s
141050K .......... .......... .......... .......... .......... 53% 77.8M 5s
141100K .......... .......... .......... .......... .......... 53% 96.3M 5s
141150K .......... .......... .......... .......... .......... 53% 76.9M 5s
141200K .......... .......... .......... .......... .......... 53% 46.0M 5s
141250K .......... .......... .......... .......... .......... 53% 51.7M 5s
141300K .......... .......... .......... .......... .......... 53% 101M 5s
141350K .......... .......... .......... .......... .......... 53% 99.0M 5s
141400K .......... .......... .......... .......... .......... 53% 99.2M 5s
141450K .......... .......... .......... .......... .......... 53% 179M 5s
141500K .......... .......... .......... .......... .......... 53% 2.86M 5s
141550K .......... .......... .......... .......... .......... 53% 219M 5s
141600K .......... .......... .......... .......... .......... 53% 193M 5s
141650K .......... .......... .......... .......... .......... 53% 233M 5s
141700K .......... .......... .......... .......... .......... 53% 178M 5s
141750K .......... .......... .......... .......... .......... 53% 89.8M 5s
141800K .......... .......... .......... .......... .......... 53% 171M 5s
141850K .......... .......... .......... .......... .......... 53% 157M 5s
141900K .......... .......... .......... .......... .......... 53% 231M 5s
141950K .......... .......... .......... .......... .......... 53% 174M 5s
142000K .......... .......... .......... .......... .......... 53% 192M 5s
142050K .......... .......... .......... .......... .......... 53% 191M 5s
142100K .......... .......... .......... .......... .......... 53% 117M 5s
142150K .......... .......... .......... .......... .......... 53% 2.46M 5s
142200K .......... .......... .......... .......... .......... 53% 189M 5s
142250K .......... .......... .......... .......... .......... 53% 218M 5s
142300K .......... .......... .......... .......... .......... 53% 125M 5s
142350K .......... .......... .......... .......... .......... 53% 23.1M 5s
142400K .......... .......... .......... .......... .......... 53% 98.4M 5s
142450K .......... .......... .......... .......... .......... 53% 140M 5s
142500K .......... .......... .......... .......... .......... 53% 166M 5s
142550K .......... .......... .......... .......... .......... 53% 113M 5s
142600K .......... .......... .......... .......... .......... 53% 174M 5s
142650K .......... .......... .......... .......... .......... 53% 210M 5s
142700K .......... .......... .......... .......... .......... 53% 191M 5s
142750K .......... .......... .......... .......... .......... 53% 2.44M 5s
142800K .......... .......... .......... .......... .......... 53% 79.8M 5s
142850K .......... .......... .......... .......... .......... 53% 160M 5s
142900K .......... .......... .......... .......... .......... 53% 209M 5s
142950K .......... .......... .......... .......... .......... 53% 154M 5s
143000K .......... .......... .......... .......... .......... 53% 181M 5s
143050K .......... .......... .......... .......... .......... 53% 154M 5s
143100K .......... .......... .......... .......... .......... 53% 175M 5s
143150K .......... .......... .......... .......... .......... 53% 190M 5s
143200K .......... .......... .......... .......... .......... 53% 166M 5s
143250K .......... .......... .......... .......... .......... 53% 197M 5s
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143350K .......... .......... .......... .......... .......... 53% 2.72M 5s
143400K .......... .......... .......... .......... .......... 53% 176M 5s
143450K .......... .......... .......... .......... .......... 54% 189M 5s
143500K .......... .......... .......... .......... .......... 54% 230M 5s
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143650K .......... .......... .......... .......... .......... 54% 231M 5s
143700K .......... .......... .......... .......... .......... 54% 195M 5s
143750K .......... .......... .......... .......... .......... 54% 227M 5s
143800K .......... .......... .......... .......... .......... 54% 217M 5s
143850K .......... .......... .......... .......... .......... 54% 186M 5s
143900K .......... .......... .......... .......... .......... 54% 193M 5s
143950K .......... .......... .......... .......... .......... 54% 119M 5s
144000K .......... .......... .......... .......... .......... 54% 2.66M 5s
144050K .......... .......... .......... .......... .......... 54% 97.9M 5s
144100K .......... .......... .......... .......... .......... 54% 44.4M 5s
144150K .......... .......... .......... .......... .......... 54% 81.7M 5s
144200K .......... .......... .......... .......... .......... 54% 119M 5s
144250K .......... .......... .......... .......... .......... 54% 174M 5s
144300K .......... .......... .......... .......... .......... 54% 95.2M 5s
144350K .......... .......... .......... .......... .......... 54% 94.6M 5s
144400K .......... .......... .......... .......... .......... 54% 87.3M 5s
144450K .......... .......... .......... .......... .......... 54% 48.7M 5s
144500K .......... .......... .......... .......... .......... 54% 166M 5s
144550K .......... .......... .......... .......... .......... 54% 137M 5s
144600K .......... .......... .......... .......... .......... 54% 2.47M 5s
144650K .......... .......... .......... .......... .......... 54% 207M 5s
144700K .......... .......... .......... .......... .......... 54% 187M 5s
144750K .......... .......... .......... .......... .......... 54% 213M 5s
144800K .......... .......... .......... .......... .......... 54% 220M 5s
144850K .......... .......... .......... .......... .......... 54% 74.1M 5s
144900K .......... .......... .......... .......... .......... 54% 188M 5s
144950K .......... .......... .......... .......... .......... 54% 191M 5s
145000K .......... .......... .......... .......... .......... 54% 221M 5s
145050K .......... .......... .......... .......... .......... 54% 162M 5s
145100K .......... .......... .......... .......... .......... 54% 189M 5s
145150K .......... .......... .......... .......... .......... 54% 217M 5s
145200K .......... .......... .......... .......... .......... 54% 193M 5s
145250K .......... .......... .......... .......... .......... 54% 2.60M 5s
145300K .......... .......... .......... .......... .......... 54% 158M 5s
145350K .......... .......... .......... .......... .......... 54% 147M 5s
145400K .......... .......... .......... .......... .......... 54% 33.1M 5s
145450K .......... .......... .......... .......... .......... 54% 139M 5s
145500K .......... .......... .......... .......... .......... 54% 202M 5s
145550K .......... .......... .......... .......... .......... 54% 193M 5s
145600K .......... .......... .......... .......... .......... 54% 156M 5s
145650K .......... .......... .......... .......... .......... 54% 210M 5s
145700K .......... .......... .......... .......... .......... 54% 91.4M 5s
145750K .......... .......... .......... .......... .......... 54% 203M 5s
145800K .......... .......... .......... .......... .......... 54% 216M 5s
145850K .......... .......... .......... .......... .......... 54% 2.37M 5s
145900K .......... .......... .......... .......... .......... 54% 206M 5s
145950K .......... .......... .......... .......... .......... 54% 177M 5s
146000K .......... .......... .......... .......... .......... 54% 180M 5s
146050K .......... .......... .......... .......... .......... 54% 203M 5s
146100K .......... .......... .......... .......... .......... 54% 180M 5s
146150K .......... .......... .......... .......... .......... 55% 111M 5s
146200K .......... .......... .......... .......... .......... 55% 124M 5s
146250K .......... .......... .......... .......... .......... 55% 222M 5s
146300K .......... .......... .......... .......... .......... 55% 222M 5s
146350K .......... .......... .......... .......... .......... 55% 192M 5s
146400K .......... .......... .......... .......... .......... 55% 134M 5s
146450K .......... .......... .......... .......... .......... 55% 2.54M 5s
146500K .......... .......... .......... .......... .......... 55% 182M 5s
146550K .......... .......... .......... .......... .......... 55% 86.7M 5s
146600K .......... .......... .......... .......... .......... 55% 193M 5s
146650K .......... .......... .......... .......... .......... 55% 88.0M 5s
146700K .......... .......... .......... .......... .......... 55% 193M 5s
146750K .......... .......... .......... .......... .......... 55% 107M 5s
146800K .......... .......... .......... .......... .......... 55% 215M 5s
146850K .......... .......... .......... .......... .......... 55% 174M 5s
146900K .......... .......... .......... .......... .......... 55% 17.6M 5s
146950K .......... .......... .......... .......... .......... 55% 25.8M 5s
147000K .......... .......... .......... .......... .......... 55% 212M 5s
147050K .......... .......... .......... .......... .......... 55% 218M 5s
147100K .......... .......... .......... .......... .......... 55% 2.02M 5s
147150K .......... .......... .......... .......... .......... 55% 213M 5s
147200K .......... .......... .......... .......... .......... 55% 189M 5s
147250K .......... .......... .......... .......... .......... 55% 52.7M 5s
147300K .......... .......... .......... .......... .......... 55% 218M 5s
147350K .......... .......... .......... .......... .......... 55% 186M 5s
147400K .......... .......... .......... .......... .......... 55% 220M 5s
147450K .......... .......... .......... .......... .......... 55% 64.9M 5s
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147600K .......... .......... .......... .......... .......... 55% 170M 5s
147650K .......... .......... .......... .......... .......... 55% 206M 5s
147700K .......... .......... .......... .......... .......... 55% 2.57M 5s
147750K .......... .......... .......... .......... .......... 55% 35.0M 5s
147800K .......... .......... .......... .......... .......... 55% 10.3M 5s
147850K .......... .......... .......... .......... .......... 55% 49.9M 5s
147900K .......... .......... .......... .......... .......... 55% 41.7M 5s
147950K .......... .......... .......... .......... .......... 55% 192M 5s
148000K .......... .......... .......... .......... .......... 55% 57.6M 5s
148050K .......... .......... .......... .......... .......... 55% 49.1M 5s
148100K .......... .......... .......... .......... .......... 55% 194M 5s
148150K .......... .......... .......... .......... .......... 55% 102M 5s
148200K .......... .......... .......... .......... .......... 55% 79.0M 5s
148250K .......... .......... .......... .......... .......... 55% 102M 5s
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148350K .......... .......... .......... .......... .......... 55% 1.96M 5s
148400K .......... .......... .......... .......... .......... 55% 7.39M 5s
148450K .......... .......... .......... .......... .......... 55% 82.1M 5s
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148700K .......... .......... .......... .......... .......... 55% 59.6M 5s
148750K .......... .......... .......... .......... .......... 55% 15.4M 5s
148800K .......... .......... .......... .......... .......... 56% 42.3M 5s
148850K .......... .......... .......... .......... .......... 56% 69.9M 5s
148900K .......... .......... .......... .......... .......... 56% 190M 5s
148950K .......... .......... .......... .......... .......... 56% 18.0M 5s
149000K .......... .......... .......... .......... .......... 56% 2.55M 5s
149050K .......... .......... .......... .......... .......... 56% 111M 5s
149100K .......... .......... .......... .......... .......... 56% 165M 5s
149150K .......... .......... .......... .......... .......... 56% 59.6M 5s
149200K .......... .......... .......... .......... .......... 56% 27.8M 5s
149250K .......... .......... .......... .......... .......... 56% 66.9M 5s
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149350K .......... .......... .......... .......... .......... 56% 79.0M 5s
149400K .......... .......... .......... .......... .......... 56% 68.5M 5s
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149650K .......... .......... .......... .......... .......... 56% 156M 5s
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150000K .......... .......... .......... .......... .......... 56% 205M 5s
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150100K .......... .......... .......... .......... .......... 56% 171M 5s
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150200K .......... .......... .......... .......... .......... 56% 173M 5s
150250K .......... .......... .......... .......... .......... 56% 2.57M 5s
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150350K .......... .......... .......... .......... .......... 56% 174M 5s
150400K .......... .......... .......... .......... .......... 56% 192M 5s
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150550K .......... .......... .......... .......... .......... 56% 94.8M 5s
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150750K .......... .......... .......... .......... .......... 56% 163M 5s
150800K .......... .......... .......... .......... .......... 56% 32.6M 5s
150850K .......... .......... .......... .......... .......... 56% 2.61M 5s
150900K .......... .......... .......... .......... .......... 56% 48.2M 5s
150950K .......... .......... .......... .......... .......... 56% 107M 5s
151000K .......... .......... .......... .......... .......... 56% 222M 5s
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151100K .......... .......... .......... .......... .......... 56% 38.5M 5s
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151200K .......... .......... .......... .......... .......... 56% 185M 5s
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151400K .......... .......... .......... .......... .......... 56% 133M 5s
151450K .......... .......... .......... .......... .......... 57% 185M 5s
151500K .......... .......... .......... .......... .......... 57% 2.55M 5s
151550K .......... .......... .......... .......... .......... 57% 122M 5s
151600K .......... .......... .......... .......... .......... 57% 121M 5s
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151700K .......... .......... .......... .......... .......... 57% 187M 5s
151750K .......... .......... .......... .......... .......... 57% 206M 5s
151800K .......... .......... .......... .......... .......... 57% 219M 5s
151850K .......... .......... .......... .......... .......... 57% 170M 5s
151900K .......... .......... .......... .......... .......... 57% 144M 5s
151950K .......... .......... .......... .......... .......... 57% 163M 5s
152000K .......... .......... .......... .......... .......... 57% 206M 5s
152050K .......... .......... .......... .......... .......... 57% 183M 5s
152100K .......... .......... .......... .......... .......... 57% 2.53M 5s
152150K .......... .......... .......... .......... .......... 57% 118M 5s
152200K .......... .......... .......... .......... .......... 57% 103M 5s
152250K .......... .......... .......... .......... .......... 57% 213M 5s
152300K .......... .......... .......... .......... .......... 57% 149M 5s
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152500K .......... .......... .......... .......... .......... 57% 209M 5s
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152650K .......... .......... .......... .......... .......... 57% 125M 5s
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152750K .......... .......... .......... .......... .......... 57% 2.69M 5s
152800K .......... .......... .......... .......... .......... 57% 157M 5s
152850K .......... .......... .......... .......... .......... 57% 183M 5s
152900K .......... .......... .......... .......... .......... 57% 207M 5s
152950K .......... .......... .......... .......... .......... 57% 167M 5s
153000K .......... .......... .......... .......... .......... 57% 201M 5s
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153100K .......... .......... .......... .......... .......... 57% 98.0M 5s
153150K .......... .......... .......... .......... .......... 57% 138M 5s
153200K .......... .......... .......... .......... .......... 57% 105M 5s
153250K .......... .......... .......... .......... .......... 57% 162M 5s
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153400K .......... .......... .......... .......... .......... 57% 2.55M 5s
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153500K .......... .......... .......... .......... .......... 57% 66.5M 5s
153550K .......... .......... .......... .......... .......... 57% 119M 5s
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153850K .......... .......... .......... .......... .......... 57% 176M 5s
153900K .......... .......... .......... .......... .......... 57% 198M 5s
153950K .......... .......... .......... .......... .......... 57% 170M 5s
154000K .......... .......... .......... .......... .......... 57% 2.62M 5s
154050K .......... .......... .......... .......... .......... 57% 127M 5s
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154150K .......... .......... .......... .......... .......... 58% 180M 5s
154200K .......... .......... .......... .......... .......... 58% 208M 5s
154250K .......... .......... .......... .......... .......... 58% 241M 5s
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154450K .......... .......... .......... .......... .......... 58% 31.0M 5s
154500K .......... .......... .......... .......... .......... 58% 173M 5s
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154600K .......... .......... .......... .......... .......... 58% 93.9M 5s
154650K .......... .......... .......... .......... .......... 58% 1.72M 5s
154700K .......... .......... .......... .......... .......... 58% 189M 5s
154750K .......... .......... .......... .......... .......... 58% 130M 5s
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154850K .......... .......... .......... .......... .......... 58% 184M 5s
154900K .......... .......... .......... .......... .......... 58% 19.3M 5s
154950K .......... .......... .......... .......... .......... 58% 191M 5s
155000K .......... .......... .......... .......... .......... 58% 223M 5s
155050K .......... .......... .......... .......... .......... 58% 226M 5s
155100K .......... .......... .......... .......... .......... 58% 18.2M 5s
155150K .......... .......... .......... .......... .......... 58% 212M 5s
155200K .......... .......... .......... .......... .......... 58% 190M 5s
155250K .......... .......... .......... .......... .......... 58% 24.2M 5s
155300K .......... .......... .......... .......... .......... 58% 2.64M 5s
155350K .......... .......... .......... .......... .......... 58% 48.2M 5s
155400K .......... .......... .......... .......... .......... 58% 19.2M 5s
155450K .......... .......... .......... .......... .......... 58% 43.8M 5s
155500K .......... .......... .......... .......... .......... 58% 50.9M 5s
155550K .......... .......... .......... .......... .......... 58% 46.2M 5s
155600K .......... .......... .......... .......... .......... 58% 2.28M 5s
155650K .......... .......... .......... .......... .......... 58% 95.2M 5s
155700K .......... .......... .......... .......... .......... 58% 167M 5s
155750K .......... .......... .......... .......... .......... 58% 147M 5s
155800K .......... .......... .......... .......... .......... 58% 131M 5s
155850K .......... .......... .......... .......... .......... 58% 106M 5s
155900K .......... .......... .......... .......... .......... 58% 2.53M 5s
155950K .......... .......... .......... .......... .......... 58% 140M 5s
156000K .......... .......... .......... .......... .......... 58% 167M 5s
156050K .......... .......... .......... .......... .......... 58% 186M 5s
156100K .......... .......... .......... .......... .......... 58% 153M 5s
156150K .......... .......... .......... .......... .......... 58% 193M 5s
156200K .......... .......... .......... .......... .......... 58% 176M 5s
156250K .......... .......... .......... .......... .......... 58% 210M 5s
156300K .......... .......... .......... .......... .......... 58% 115M 5s
156350K .......... .......... .......... .......... .......... 58% 21.4M 5s
156400K .......... .......... .......... .......... .......... 58% 32.3M 5s
156450K .......... .......... .......... .......... .......... 58% 14.8M 5s
156500K .......... .......... .......... .......... .......... 58% 46.2M 5s
156550K .......... .......... .......... .......... .......... 58% 2.34M 5s
156600K .......... .......... .......... .......... .......... 58% 17.6M 5s
156650K .......... .......... .......... .......... .......... 58% 85.4M 5s
156700K .......... .......... .......... .......... .......... 58% 96.3M 5s
156750K .......... .......... .......... .......... .......... 59% 95.6M 5s
156800K .......... .......... .......... .......... .......... 59% 30.6M 5s
156850K .......... .......... .......... .......... .......... 59% 18.7M 5s
156900K .......... .......... .......... .......... .......... 59% 79.4M 5s
156950K .......... .......... .......... .......... .......... 59% 153M 5s
157000K .......... .......... .......... .......... .......... 59% 48.0M 5s
157050K .......... .......... .......... .......... .......... 59% 192M 5s
157100K .......... .......... .......... .......... .......... 59% 25.7M 5s
157150K .......... .......... .......... .......... .......... 59% 36.6M 5s
157200K .......... .......... .......... .......... .......... 59% 2.40M 5s
157250K .......... .......... .......... .......... .......... 59% 78.9M 5s
157300K .......... .......... .......... .......... .......... 59% 9.90M 5s
157350K .......... .......... .......... .......... .......... 59% 182M 5s
157400K .......... .......... .......... .......... .......... 59% 68.0M 5s
157450K .......... .......... .......... .......... .......... 59% 15.4M 5s
157500K .......... .......... .......... .......... .......... 59% 224M 5s
157550K .......... .......... .......... .......... .......... 59% 226M 5s
157600K .......... .......... .......... .......... .......... 59% 50.2M 5s
157650K .......... .......... .......... .......... .......... 59% 166M 5s
157700K .......... .......... .......... .......... .......... 59% 94.8M 5s
157750K .......... .......... .......... .......... .......... 59% 205M 5s
157800K .......... .......... .......... .......... .......... 59% 4.99M 5s
157850K .......... .......... .......... .......... .......... 59% 2.59M 5s
157900K .......... .......... .......... .......... .......... 59% 47.1M 5s
157950K .......... .......... .......... .......... .......... 59% 40.7M 5s
158000K .......... .......... .......... .......... .......... 59% 55.0M 5s
158050K .......... .......... .......... .......... .......... 59% 102M 5s
158100K .......... .......... .......... .......... .......... 59% 22.2M 5s
158150K .......... .......... .......... .......... .......... 59% 98.2M 5s
158200K .......... .......... .......... .......... .......... 59% 25.8M 5s
158250K .......... .......... .......... .......... .......... 59% 56.6M 5s
158300K .......... .......... .......... .......... .......... 59% 36.3M 5s
158350K .......... .......... .......... .......... .......... 59% 45.1M 5s
158400K .......... .......... .......... .......... .......... 59% 195M 5s
158450K .......... .......... .......... .......... .......... 59% 2.21M 5s
158500K .......... .......... .......... .......... .......... 59% 57.2M 5s
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158650K .......... .......... .......... .......... .......... 59% 212M 5s
158700K .......... .......... .......... .......... .......... 59% 43.9M 5s
158750K .......... .......... .......... .......... .......... 59% 32.7M 5s
158800K .......... .......... .......... .......... .......... 59% 41.8M 5s
158850K .......... .......... .......... .......... .......... 59% 38.4M 5s
158900K .......... .......... .......... .......... .......... 59% 94.6M 5s
158950K .......... .......... .......... .......... .......... 59% 149M 5s
159000K .......... .......... .......... .......... .......... 59% 115M 5s
159050K .......... .......... .......... .......... .......... 59% 89.1M 5s
159100K .......... .......... .......... .......... .......... 59% 2.37M 5s
159150K .......... .......... .......... .......... .......... 59% 208M 5s
159200K .......... .......... .......... .......... .......... 59% 43.1M 5s
159250K .......... .......... .......... .......... .......... 59% 52.5M 5s
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159350K .......... .......... .......... .......... .......... 59% 27.3M 5s
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159650K .......... .......... .......... .......... .......... 60% 44.3M 5s
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159800K .......... .......... .......... .......... .......... 60% 141M 5s
159850K .......... .......... .......... .......... .......... 60% 76.4M 5s
159900K .......... .......... .......... .......... .......... 60% 70.9M 5s
159950K .......... .......... .......... .......... .......... 60% 50.3M 5s
160000K .......... .......... .......... .......... .......... 60% 37.8M 5s
160050K .......... .......... .......... .......... .......... 60% 170M 5s
160100K .......... .......... .......... .......... .......... 60% 55.8M 5s
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160200K .......... .......... .......... .......... .......... 60% 183M 5s
160250K .......... .......... .......... .......... .......... 60% 125M 5s
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160450K .......... .......... .......... .......... .......... 60% 71.8M 5s
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160650K .......... .......... .......... .......... .......... 60% 65.6M 5s
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160900K .......... .......... .......... .......... .......... 60% 109M 5s
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161000K .......... .......... .......... .......... .......... 60% 68.8M 5s
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161100K .......... .......... .......... .......... .......... 60% 186M 5s
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161500K .......... .......... .......... .......... .......... 60% 36.4M 5s
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161600K .......... .......... .......... .......... .......... 60% 84.8M 5s
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161800K .......... .......... .......... .......... .......... 60% 213M 5s
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162000K .......... .......... .......... .......... .......... 60% 114M 5s
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162150K .......... .......... .......... .......... .......... 61% 203M 5s
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162250K .......... .......... .......... .......... .......... 61% 139M 5s
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171000K .......... .......... .......... .......... .......... 64% 6.16M 4s
171050K .......... .......... .......... .......... .......... 64% 40.2M 4s
171100K .......... .......... .......... .......... .......... 64% 160M 4s
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171200K .......... .......... .......... .......... .......... 64% 19.6M 4s
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171300K .......... .......... .......... .......... .......... 64% 8.14M 4s
171350K .......... .......... .......... .......... .......... 64% 193M 4s
171400K .......... .......... .......... .......... .......... 64% 457K 4s
171450K .......... .......... .......... .......... .......... 64% 52.1M 4s
171500K .......... .......... .......... .......... .......... 64% 39.3M 4s
171550K .......... .......... .......... .......... .......... 64% 10.2M 4s
171600K .......... .......... .......... .......... .......... 64% 3.38M 4s
171650K .......... .......... .......... .......... .......... 64% 151M 4s
171700K .......... .......... .......... .......... .......... 64% 17.2M 4s
171750K .......... .......... .......... .......... .......... 64% 176M 4s
171800K .......... .......... .......... .......... .......... 64% 3.91M 4s
171850K .......... .......... .......... .......... .......... 64% 114M 4s
171900K .......... .......... .......... .......... .......... 64% 140M 4s
171950K .......... .......... .......... .......... .......... 64% 27.0M 4s
172000K .......... .......... .......... .......... .......... 64% 35.1M 4s
172050K .......... .......... .......... .......... .......... 64% 24.1M 4s
172100K .......... .......... .......... .......... .......... 64% 24.2M 4s
172150K .......... .......... .......... .......... .......... 64% 58.1M 4s
172200K .......... .......... .......... .......... .......... 64% 14.5M 4s
172250K .......... .......... .......... .......... .......... 64% 45.4M 4s
172300K .......... .......... .......... .......... .......... 64% 22.6M 4s
172350K .......... .......... .......... .......... .......... 64% 87.8M 4s
172400K .......... .......... .......... .......... .......... 64% 10.8M 4s
172450K .......... .......... .......... .......... .......... 64% 35.9M 4s
172500K .......... .......... .......... .......... .......... 64% 186M 4s
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172750K .......... .......... .......... .......... .......... 65% 63.7M 4s
172800K .......... .......... .......... .......... .......... 65% 35.8M 4s
172850K .......... .......... .......... .......... .......... 65% 23.3M 4s
172900K .......... .......... .......... .......... .......... 65% 2.69M 4s
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173000K .......... .......... .......... .......... .......... 65% 159M 4s
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173100K .......... .......... .......... .......... .......... 65% 78.9M 4s
173150K .......... .......... .......... .......... .......... 65% 216M 4s
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173250K .......... .......... .......... .......... .......... 65% 220M 4s
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174000K .......... .......... .......... .......... .......... 65% 224M 4s
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174100K .......... .......... .......... .......... .......... 65% 186M 4s
174150K .......... .......... .......... .......... .......... 65% 228M 4s
174200K .......... .......... .......... .......... .......... 65% 2.31M 4s
174250K .......... .......... .......... .......... .......... 65% 118M 4s
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175100K .......... .......... .......... .......... .......... 65% 94.8M 4s
175150K .......... .......... .......... .......... .......... 65% 211M 4s
175200K .......... .......... .......... .......... .......... 65% 186M 4s
175250K .......... .......... .......... .......... .......... 65% 219M 4s
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175650K .......... .......... .......... .......... .......... 66% 115M 4s
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176250K .......... .......... .......... .......... .......... 66% 144M 4s
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176900K .......... .......... .......... .......... .......... 66% 74.5M 4s
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177200K .......... .......... .......... .......... .......... 66% 81.4M 4s
177250K .......... .......... .......... .......... .......... 66% 157M 4s
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178150K .......... .......... .......... .......... .......... 67% 84.5M 4s
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185100K .......... .......... .......... .......... .......... 69% 99.9M 4s
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185350K .......... .......... .......... .......... .......... 69% 98.0M 4s
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186250K .......... .......... .......... .......... .......... 70% 228M 4s
186300K .......... .......... .......... .......... .......... 70% 235M 4s
186350K .......... .......... .......... .......... .......... 70% 2.23M 4s
186400K .......... .......... .......... .......... .......... 70% 214M 4s
186450K .......... .......... .......... .......... .......... 70% 200M 4s
186500K .......... .......... .......... .......... .......... 70% 152M 4s
186550K .......... .......... .......... .......... .......... 70% 144M 4s
186600K .......... .......... .......... .......... .......... 70% 161M 4s
186650K .......... .......... .......... .......... .......... 70% 229M 4s
186700K .......... .......... .......... .......... .......... 70% 194M 4s
186750K .......... .......... .......... .......... .......... 70% 165M 4s
186800K .......... .......... .......... .......... .......... 70% 227M 4s
186850K .......... .......... .......... .......... .......... 70% 186M 4s
186900K .......... .......... .......... .......... .......... 70% 234M 4s
186950K .......... .......... .......... .......... .......... 70% 197M 4s
187000K .......... .......... .......... .......... .......... 70% 2.62M 4s
187050K .......... .......... .......... .......... .......... 70% 126M 4s
187100K .......... .......... .......... .......... .......... 70% 201M 4s
187150K .......... .......... .......... .......... .......... 70% 242M 4s
187200K .......... .......... .......... .......... .......... 70% 206M 4s
187250K .......... .......... .......... .......... .......... 70% 209M 4s
187300K .......... .......... .......... .......... .......... 70% 224M 4s
187350K .......... .......... .......... .......... .......... 70% 118M 4s
187400K .......... .......... .......... .......... .......... 70% 189M 4s
187450K .......... .......... .......... .......... .......... 70% 22.4M 4s
187500K .......... .......... .......... .......... .......... 70% 35.7M 4s
187550K .......... .......... .......... .......... .......... 70% 219M 4s
187600K .......... .......... .......... .......... .......... 70% 190M 4s
187650K .......... .......... .......... .......... .......... 70% 227M 4s
187700K .......... .......... .......... .......... .......... 70% 858K 4s
187750K .......... .......... .......... .......... .......... 70% 209M 4s
187800K .......... .......... .......... .......... .......... 70% 227M 4s
187850K .......... .......... .......... .......... .......... 70% 157M 4s
187900K .......... .......... .......... .......... .......... 70% 229M 4s
187950K .......... .......... .......... .......... .......... 70% 194M 4s
188000K .......... .......... .......... .......... .......... 70% 226M 4s
188050K .......... .......... .......... .......... .......... 70% 215M 4s
188100K .......... .......... .......... .......... .......... 70% 186M 4s
188150K .......... .......... .......... .......... .......... 70% 222M 4s
188200K .......... .......... .......... .......... .......... 70% 193M 4s
188250K .......... .......... .......... .......... .......... 70% 223M 4s
188300K .......... .......... .......... .......... .......... 70% 225M 4s
188350K .......... .......... .......... .......... .......... 70% 2.48M 4s
188400K .......... .......... .......... .......... .......... 70% 131M 4s
188450K .......... .......... .......... .......... .......... 70% 186M 4s
188500K .......... .......... .......... .......... .......... 70% 223M 4s
188550K .......... .......... .......... .......... .......... 70% 227M 4s
188600K .......... .......... .......... .......... .......... 70% 198M 4s
188650K .......... .......... .......... .......... .......... 71% 236M 4s
188700K .......... .......... .......... .......... .......... 71% 203M 4s
188750K .......... .......... .......... .......... .......... 71% 202M 4s
188800K .......... .......... .......... .......... .......... 71% 213M 4s
188850K .......... .......... .......... .......... .......... 71% 198M 4s
188900K .......... .......... .......... .......... .......... 71% 227M 4s
188950K .......... .......... .......... .......... .......... 71% 195M 4s
189000K .......... .......... .......... .......... .......... 71% 203M 4s
189050K .......... .......... .......... .......... .......... 71% 2.41M 4s
189100K .......... .......... .......... .......... .......... 71% 92.8M 4s
189150K .......... .......... .......... .......... .......... 71% 185M 4s
189200K .......... .......... .......... .......... .......... 71% 135M 4s
189250K .......... .......... .......... .......... .......... 71% 126M 4s
189300K .......... .......... .......... .......... .......... 71% 69.8M 4s
189350K .......... .......... .......... .......... .......... 71% 128M 4s
189400K .......... .......... .......... .......... .......... 71% 34.8M 4s
189450K .......... .......... .......... .......... .......... 71% 152M 4s
189500K .......... .......... .......... .......... .......... 71% 202M 4s
189550K .......... .......... .......... .......... .......... 71% 183M 4s
189600K .......... .......... .......... .......... .......... 71% 116M 4s
189650K .......... .......... .......... .......... .......... 71% 176M 4s
189700K .......... .......... .......... .......... .......... 71% 2.45M 4s
189750K .......... .......... .......... .......... .......... 71% 157M 4s
189800K .......... .......... .......... .......... .......... 71% 223M 4s
189850K .......... .......... .......... .......... .......... 71% 167M 4s
189900K .......... .......... .......... .......... .......... 71% 205M 4s
189950K .......... .......... .......... .......... .......... 71% 159M 4s
190000K .......... .......... .......... .......... .......... 71% 164M 4s
190050K .......... .......... .......... .......... .......... 71% 191M 4s
190100K .......... .......... .......... .......... .......... 71% 129M 4s
190150K .......... .......... .......... .......... .......... 71% 157M 4s
190200K .......... .......... .......... .......... .......... 71% 140M 4s
190250K .......... .......... .......... .......... .......... 71% 160M 3s
190300K .......... .......... .......... .......... .......... 71% 151M 3s
190350K .......... .......... .......... .......... .......... 71% 163M 3s
190400K .......... .......... .......... .......... .......... 71% 1.83M 3s
190450K .......... .......... .......... .......... .......... 71% 105M 3s
190500K .......... .......... .......... .......... .......... 71% 182M 3s
190550K .......... .......... .......... .......... .......... 71% 223M 3s
190600K .......... .......... .......... .......... .......... 71% 189M 3s
190650K .......... .......... .......... .......... .......... 71% 226M 3s
190700K .......... .......... .......... .......... .......... 71% 195M 3s
190750K .......... .......... .......... .......... .......... 71% 168M 3s
190800K .......... .......... .......... .......... .......... 71% 164M 3s
190850K .......... .......... .......... .......... .......... 71% 150M 3s
190900K .......... .......... .......... .......... .......... 71% 177M 3s
190950K .......... .......... .......... .......... .......... 71% 157M 3s
191000K .......... .......... .......... .......... .......... 71% 174M 3s
191050K .......... .......... .......... .......... .......... 71% 2.37M 3s
191100K .......... .......... .......... .......... .......... 71% 148M 3s
191150K .......... .......... .......... .......... .......... 71% 148M 3s
191200K .......... .......... .......... .......... .......... 71% 159M 3s
191250K .......... .......... .......... .......... .......... 71% 171M 3s
191300K .......... .......... .......... .......... .......... 72% 208M 3s
191350K .......... .......... .......... .......... .......... 72% 77.6M 3s
191400K .......... .......... .......... .......... .......... 72% 125M 3s
191450K .......... .......... .......... .......... .......... 72% 111M 3s
191500K .......... .......... .......... .......... .......... 72% 75.8M 3s
191550K .......... .......... .......... .......... .......... 72% 173M 3s
191600K .......... .......... .......... .......... .......... 72% 27.5M 3s
191650K .......... .......... .......... .......... .......... 72% 133M 3s
191700K .......... .......... .......... .......... .......... 72% 25.8M 3s
191750K .......... .......... .......... .......... .......... 72% 2.36M 3s
191800K .......... .......... .......... .......... .......... 72% 210M 3s
191850K .......... .......... .......... .......... .......... 72% 171M 3s
191900K .......... .......... .......... .......... .......... 72% 231M 3s
191950K .......... .......... .......... .......... .......... 72% 150M 3s
192000K .......... .......... .......... .......... .......... 72% 177M 3s
192050K .......... .......... .......... .......... .......... 72% 175M 3s
192100K .......... .......... .......... .......... .......... 72% 160M 3s
192150K .......... .......... .......... .......... .......... 72% 217M 3s
192200K .......... .......... .......... .......... .......... 72% 137M 3s
192250K .......... .......... .......... .......... .......... 72% 99.2M 3s
192300K .......... .......... .......... .......... .......... 72% 173M 3s
192350K .......... .......... .......... .......... .......... 72% 169M 3s
192400K .......... .......... .......... .......... .......... 72% 726K 3s
192450K .......... .......... .......... .......... .......... 72% 181M 3s
192500K .......... .......... .......... .......... .......... 72% 41.1M 3s
192550K .......... .......... .......... .......... .......... 72% 204M 3s
192600K .......... .......... .......... .......... .......... 72% 191M 3s
192650K .......... .......... .......... .......... .......... 72% 219M 3s
192700K .......... .......... .......... .......... .......... 72% 182M 3s
192750K .......... .......... .......... .......... .......... 72% 226M 3s
192800K .......... .......... .......... .......... .......... 72% 229M 3s
192850K .......... .......... .......... .......... .......... 72% 131M 3s
192900K .......... .......... .......... .......... .......... 72% 165M 3s
192950K .......... .......... .......... .......... .......... 72% 168M 3s
193000K .......... .......... .......... .......... .......... 72% 82.6M 3s
193050K .......... .......... .......... .......... .......... 72% 124M 3s
193100K .......... .......... .......... .......... .......... 72% 2.49M 3s
193150K .......... .......... .......... .......... .......... 72% 212M 3s
193200K .......... .......... .......... .......... .......... 72% 191M 3s
193250K .......... .......... .......... .......... .......... 72% 226M 3s
193300K .......... .......... .......... .......... .......... 72% 52.2M 3s
193350K .......... .......... .......... .......... .......... 72% 161M 3s
193400K .......... .......... .......... .......... .......... 72% 193M 3s
193450K .......... .......... .......... .......... .......... 72% 167M 3s
193500K .......... .......... .......... .......... .......... 72% 8.17M 3s
193550K .......... .......... .......... .......... .......... 72% 190M 3s
193600K .......... .......... .......... .......... .......... 72% 119M 3s
193650K .......... .......... .......... .......... .......... 72% 229M 3s
193700K .......... .......... .......... .......... .......... 72% 157M 3s
193750K .......... .......... .......... .......... .......... 72% 71.0M 3s
193800K .......... .......... .......... .......... .......... 72% 197M 3s
193850K .......... .......... .......... .......... .......... 72% 203M 3s
193900K .......... .......... .......... .......... .......... 72% 230M 3s
193950K .......... .......... .......... .......... .......... 73% 2.47M 3s
194000K .......... .......... .......... .......... .......... 73% 183M 3s
194050K .......... .......... .......... .......... .......... 73% 231M 3s
194100K .......... .......... .......... .......... .......... 73% 198M 3s
194150K .......... .......... .......... .......... .......... 73% 226M 3s
194200K .......... .......... .......... .......... .......... 73% 203M 3s
194250K .......... .......... .......... .......... .......... 73% 238M 3s
194300K .......... .......... .......... .......... .......... 73% 234M 3s
194350K .......... .......... .......... .......... .......... 73% 195M 3s
194400K .......... .......... .......... .......... .......... 73% 234M 3s
194450K .......... .......... .......... .......... .......... 73% 198M 3s
194500K .......... .......... .......... .......... .......... 73% 236M 3s
194550K .......... .......... .......... .......... .......... 73% 128M 3s
194600K .......... .......... .......... .......... .......... 73% 195M 3s
194650K .......... .......... .......... .......... .......... 73% 2.44M 3s
194700K .......... .......... .......... .......... .......... 73% 157M 3s
194750K .......... .......... .......... .......... .......... 73% 207M 3s
194800K .......... .......... .......... .......... .......... 73% 121M 3s
194850K .......... .......... .......... .......... .......... 73% 191M 3s
194900K .......... .......... .......... .......... .......... 73% 229M 3s
194950K .......... .......... .......... .......... .......... 73% 167M 3s
195000K .......... .......... .......... .......... .......... 73% 218M 3s
195050K .......... .......... .......... .......... .......... 73% 174M 3s
195100K .......... .......... .......... .......... .......... 73% 194M 3s
195150K .......... .......... .......... .......... .......... 73% 205M 3s
195200K .......... .......... .......... .......... .......... 73% 194M 3s
195250K .......... .......... .......... .......... .......... 73% 226M 3s
195300K .......... .......... .......... .......... .......... 73% 225M 3s
195350K .......... .......... .......... .......... .......... 73% 2.35M 3s
195400K .......... .......... .......... .......... .......... 73% 218M 3s
195450K .......... .......... .......... .......... .......... 73% 58.8M 3s
195500K .......... .......... .......... .......... .......... 73% 215M 3s
195550K .......... .......... .......... .......... .......... 73% 132M 3s
195600K .......... .......... .......... .......... .......... 73% 189M 3s
195650K .......... .......... .......... .......... .......... 73% 221M 3s
195700K .......... .......... .......... .......... .......... 73% 149M 3s
195750K .......... .......... .......... .......... .......... 73% 184M 3s
195800K .......... .......... .......... .......... .......... 73% 225M 3s
195850K .......... .......... .......... .......... .......... 73% 196M 3s
195900K .......... .......... .......... .......... .......... 73% 225M 3s
195950K .......... .......... .......... .......... .......... 73% 180M 3s
196000K .......... .......... .......... .......... .......... 73% 2.40M 3s
196050K .......... .......... .......... .......... .......... 73% 210M 3s
196100K .......... .......... .......... .......... .......... 73% 191M 3s
196150K .......... .......... .......... .......... .......... 73% 215M 3s
196200K .......... .......... .......... .......... .......... 73% 179M 3s
196250K .......... .......... .......... .......... .......... 73% 223M 3s
196300K .......... .......... .......... .......... .......... 73% 225M 3s
196350K .......... .......... .......... .......... .......... 73% 160M 3s
196400K .......... .......... .......... .......... .......... 73% 220M 3s
196450K .......... .......... .......... .......... .......... 73% 185M 3s
196500K .......... .......... .......... .......... .......... 73% 208M 3s
196550K .......... .......... .......... .......... .......... 73% 220M 3s
196600K .......... .......... .......... .......... .......... 74% 107M 3s
196650K .......... .......... .......... .......... .......... 74% 180M 3s
196700K .......... .......... .......... .......... .......... 74% 2.16M 3s
196750K .......... .......... .......... .......... .......... 74% 170M 3s
196800K .......... .......... .......... .......... .......... 74% 210M 3s
196850K .......... .......... .......... .......... .......... 74% 174M 3s
196900K .......... .......... .......... .......... .......... 74% 140M 3s
196950K .......... .......... .......... .......... .......... 74% 153M 3s
197000K .......... .......... .......... .......... .......... 74% 120M 3s
197050K .......... .......... .......... .......... .......... 74% 183M 3s
197100K .......... .......... .......... .......... .......... 74% 170M 3s
197150K .......... .......... .......... .......... .......... 74% 196M 3s
197200K .......... .......... .......... .......... .......... 74% 109M 3s
197250K .......... .......... .......... .......... .......... 74% 89.1M 3s
197300K .......... .......... .......... .......... .......... 74% 203M 3s
197350K .......... .......... .......... .......... .......... 74% 816K 3s
197400K .......... .......... .......... .......... .......... 74% 133M 3s
197450K .......... .......... .......... .......... .......... 74% 175M 3s
197500K .......... .......... .......... .......... .......... 74% 156M 3s
197550K .......... .......... .......... .......... .......... 74% 203M 3s
197600K .......... .......... .......... .......... .......... 74% 91.4M 3s
197650K .......... .......... .......... .......... .......... 74% 144M 3s
197700K .......... .......... .......... .......... .......... 74% 191M 3s
197750K .......... .......... .......... .......... .......... 74% 218M 3s
197800K .......... .......... .......... .......... .......... 74% 205M 3s
197850K .......... .......... .......... .......... .......... 74% 158M 3s
197900K .......... .......... .......... .......... .......... 74% 41.6M 3s
197950K .......... .......... .......... .......... .......... 74% 39.7M 3s
198000K .......... .......... .......... .......... .......... 74% 56.4M 3s
198050K .......... .......... .......... .......... .......... 74% 2.30M 3s
198100K .......... .......... .......... .......... .......... 74% 184M 3s
198150K .......... .......... .......... .......... .......... 74% 161M 3s
198200K .......... .......... .......... .......... .......... 74% 185M 3s
198250K .......... .......... .......... .......... .......... 74% 207M 3s
198300K .......... .......... .......... .......... .......... 74% 229M 3s
198350K .......... .......... .......... .......... .......... 74% 152M 3s
198400K .......... .......... .......... .......... .......... 74% 209M 3s
198450K .......... .......... .......... .......... .......... 74% 140M 3s
198500K .......... .......... .......... .......... .......... 74% 228M 3s
198550K .......... .......... .......... .......... .......... 74% 219M 3s
198600K .......... .......... .......... .......... .......... 74% 92.3M 3s
198650K .......... .......... .......... .......... .......... 74% 43.9M 3s
198700K .......... .......... .......... .......... .......... 74% 174M 3s
198750K .......... .......... .......... .......... .......... 74% 2.53M 3s
198800K .......... .......... .......... .......... .......... 74% 113M 3s
198850K .......... .......... .......... .......... .......... 74% 82.9M 3s
198900K .......... .......... .......... .......... .......... 74% 130M 3s
198950K .......... .......... .......... .......... .......... 74% 124M 3s
199000K .......... .......... .......... .......... .......... 74% 150M 3s
199050K .......... .......... .......... .......... .......... 74% 166M 3s
199100K .......... .......... .......... .......... .......... 74% 136M 3s
199150K .......... .......... .......... .......... .......... 74% 49.4M 3s
199200K .......... .......... .......... .......... .......... 74% 160M 3s
199250K .......... .......... .......... .......... .......... 75% 132M 3s
199300K .......... .......... .......... .......... .......... 75% 140M 3s
199350K .......... .......... .......... .......... .......... 75% 134M 3s
199400K .......... .......... .......... .......... .......... 75% 2.23M 3s
199450K .......... .......... .......... .......... .......... 75% 130M 3s
199500K .......... .......... .......... .......... .......... 75% 206M 3s
199550K .......... .......... .......... .......... .......... 75% 199M 3s
199600K .......... .......... .......... .......... .......... 75% 41.7M 3s
199650K .......... .......... .......... .......... .......... 75% 37.4M 3s
199700K .......... .......... .......... .......... .......... 75% 102M 3s
199750K .......... .......... .......... .......... .......... 75% 158M 3s
199800K .......... .......... .......... .......... .......... 75% 160M 3s
199850K .......... .......... .......... .......... .......... 75% 148M 3s
199900K .......... .......... .......... .......... .......... 75% 158M 3s
199950K .......... .......... .......... .......... .......... 75% 107M 3s
200000K .......... .......... .......... .......... .......... 75% 180M 3s
200050K .......... .......... .......... .......... .......... 75% 182M 3s
200100K .......... .......... .......... .......... .......... 75% 1.10M 3s
200150K .......... .......... .......... .......... .......... 75% 135M 3s
200200K .......... .......... .......... .......... .......... 75% 150M 3s
200250K .......... .......... .......... .......... .......... 75% 186M 3s
200300K .......... .......... .......... .......... .......... 75% 121M 3s
200350K .......... .......... .......... .......... .......... 75% 103M 3s
200400K .......... .......... .......... .......... .......... 75% 164M 3s
200450K .......... .......... .......... .......... .......... 75% 115M 3s
200500K .......... .......... .......... .......... .......... 75% 130M 3s
200550K .......... .......... .......... .......... .......... 75% 195M 3s
200600K .......... .......... .......... .......... .......... 75% 150M 3s
200650K .......... .......... .......... .......... .......... 75% 98.4M 3s
200700K .......... .......... .......... .......... .......... 75% 31.1M 3s
200750K .......... .......... .......... .......... .......... 75% 90.9M 3s
200800K .......... .......... .......... .......... .......... 75% 1.33M 3s
200850K .......... .......... .......... .......... .......... 75% 45.3M 3s
200900K .......... .......... .......... .......... .......... 75% 218M 3s
200950K .......... .......... .......... .......... .......... 75% 40.0M 3s
201000K .......... .......... .......... .......... .......... 75% 212M 3s
201050K .......... .......... .......... .......... .......... 75% 223M 3s
201100K .......... .......... .......... .......... .......... 75% 52.4M 3s
201150K .......... .......... .......... .......... .......... 75% 217M 3s
201200K .......... .......... .......... .......... .......... 75% 194M 3s
201250K .......... .......... .......... .......... .......... 75% 216M 3s
201300K .......... .......... .......... .......... .......... 75% 228M 3s
201350K .......... .......... .......... .......... .......... 75% 201M 3s
201400K .......... .......... .......... .......... .......... 75% 223M 3s
201450K .......... .......... .......... .......... .......... 75% 183M 3s
201500K .......... .......... .......... .......... .......... 75% 1.24M 3s
201550K .......... .......... .......... .......... .......... 75% 224M 3s
201600K .......... .......... .......... .......... .......... 75% 195M 3s
201650K .......... .......... .......... .......... .......... 75% 2.90M 3s
201700K .......... .......... .......... .......... .......... 75% 48.2M 3s
201750K .......... .......... .......... .......... .......... 75% 119M 3s
201800K .......... .......... .......... .......... .......... 75% 116M 3s
201850K .......... .......... .......... .......... .......... 75% 137M 3s
201900K .......... .......... .......... .......... .......... 75% 219M 3s
201950K .......... .......... .......... .......... .......... 76% 186M 3s
202000K .......... .......... .......... .......... .......... 76% 212M 3s
202050K .......... .......... .......... .......... .......... 76% 215M 3s
202100K .......... .......... .......... .......... .......... 76% 176M 3s
202150K .......... .......... .......... .......... .......... 76% 1.79M 3s
202200K .......... .......... .......... .......... .......... 76% 155M 3s
202250K .......... .......... .......... .......... .......... 76% 224M 3s
202300K .......... .......... .......... .......... .......... 76% 222M 3s
202350K .......... .......... .......... .......... .......... 76% 190M 3s
202400K .......... .......... .......... .......... .......... 76% 192M 3s
202450K .......... .......... .......... .......... .......... 76% 194M 3s
202500K .......... .......... .......... .......... .......... 76% 5.86M 3s
202550K .......... .......... .......... .......... .......... 76% 7.59M 3s
202600K .......... .......... .......... .......... .......... 76% 157M 3s
202650K .......... .......... .......... .......... .......... 76% 212M 3s
202700K .......... .......... .......... .......... .......... 76% 192M 3s
202750K .......... .......... .......... .......... .......... 76% 132M 3s
202800K .......... .......... .......... .......... .......... 76% 166M 3s
202850K .......... .......... .......... .......... .......... 76% 2.16M 3s
202900K .......... .......... .......... .......... .......... 76% 212M 3s
202950K .......... .......... .......... .......... .......... 76% 88.6M 3s
203000K .......... .......... .......... .......... .......... 76% 204M 3s
203050K .......... .......... .......... .......... .......... 76% 228M 3s
203100K .......... .......... .......... .......... .......... 76% 79.5M 3s
203150K .......... .......... .......... .......... .......... 76% 112M 3s
203200K .......... .......... .......... .......... .......... 76% 155M 3s
203250K .......... .......... .......... .......... .......... 76% 224M 3s
203300K .......... .......... .......... .......... .......... 76% 226M 3s
203350K .......... .......... .......... .......... .......... 76% 154M 3s
203400K .......... .......... .......... .......... .......... 76% 14.0M 3s
203450K .......... .......... .......... .......... .......... 76% 29.3M 3s
203500K .......... .......... .......... .......... .......... 76% 143M 3s
203550K .......... .......... .......... .......... .......... 76% 2.07M 3s
203600K .......... .......... .......... .......... .......... 76% 150M 3s
203650K .......... .......... .......... .......... .......... 76% 149M 3s
203700K .......... .......... .......... .......... .......... 76% 147M 3s
203750K .......... .......... .......... .......... .......... 76% 60.7M 3s
203800K .......... .......... .......... .......... .......... 76% 74.4M 3s
203850K .......... .......... .......... .......... .......... 76% 6.64M 3s
203900K .......... .......... .......... .......... .......... 76% 59.3M 3s
203950K .......... .......... .......... .......... .......... 76% 182M 3s
204000K .......... .......... .......... .......... .......... 76% 211M 3s
204050K .......... .......... .......... .......... .......... 76% 123M 3s
204100K .......... .......... .......... .......... .......... 76% 120M 3s
204150K .......... .......... .......... .......... .......... 76% 43.3M 3s
204200K .......... .......... .......... .......... .......... 76% 29.2M 3s
204250K .......... .......... .......... .......... .......... 76% 29.8M 3s
204300K .......... .......... .......... .......... .......... 76% 217M 3s
204350K .......... .......... .......... .......... .......... 76% 195M 3s
204400K .......... .......... .......... .......... .......... 76% 215M 3s
204450K .......... .......... .......... .......... .......... 76% 1.68M 3s
204500K .......... .......... .......... .......... .......... 76% 120M 3s
204550K .......... .......... .......... .......... .......... 76% 30.7M 3s
204600K .......... .......... .......... .......... .......... 77% 182M 3s
204650K .......... .......... .......... .......... .......... 77% 221M 3s
204700K .......... .......... .......... .......... .......... 77% 193M 3s
204750K .......... .......... .......... .......... .......... 77% 213M 3s
204800K .......... .......... .......... .......... .......... 77% 119M 3s
204850K .......... .......... .......... .......... .......... 77% 132M 3s
204900K .......... .......... .......... .......... .......... 77% 207M 3s
204950K .......... .......... .......... .......... .......... 77% 80.7M 3s
205000K .......... .......... .......... .......... .......... 77% 167M 3s
205050K .......... .......... .......... .......... .......... 77% 136M 3s
205100K .......... .......... .......... .......... .......... 77% 126M 3s
205150K .......... .......... .......... .......... .......... 77% 1.64M 3s
205200K .......... .......... .......... .......... .......... 77% 196M 3s
205250K .......... .......... .......... .......... .......... 77% 226M 3s
205300K .......... .......... .......... .......... .......... 77% 42.6M 3s
205350K .......... .......... .......... .......... .......... 77% 45.3M 3s
205400K .......... .......... .......... .......... .......... 77% 226M 3s
205450K .......... .......... .......... .......... .......... 77% 103M 3s
205500K .......... .......... .......... .......... .......... 77% 12.9M 3s
205550K .......... .......... .......... .......... .......... 77% 26.1M 3s
205600K .......... .......... .......... .......... .......... 77% 157M 3s
205650K .......... .......... .......... .......... .......... 77% 194M 3s
205700K .......... .......... .......... .......... .......... 77% 49.4M 3s
205750K .......... .......... .......... .......... .......... 77% 221M 3s
205800K .......... .......... .......... .......... .......... 77% 98.8M 3s
205850K .......... .......... .......... .......... .......... 77% 1.83M 3s
205900K .......... .......... .......... .......... .......... 77% 176M 3s
205950K .......... .......... .......... .......... .......... 77% 189M 3s
206000K .......... .......... .......... .......... .......... 77% 229M 3s
206050K .......... .......... .......... .......... .......... 77% 227M 3s
206100K .......... .......... .......... .......... .......... 77% 199M 3s
206150K .......... .......... .......... .......... .......... 77% 225M 3s
206200K .......... .......... .......... .......... .......... 77% 189M 3s
206250K .......... .......... .......... .......... .......... 77% 223M 3s
206300K .......... .......... .......... .......... .......... 77% 225M 3s
206350K .......... .......... .......... .......... .......... 77% 203M 3s
206400K .......... .......... .......... .......... .......... 77% 234M 3s
206450K .......... .......... .......... .......... .......... 77% 197M 3s
206500K .......... .......... .......... .......... .......... 77% 1.17M 3s
206550K .......... .......... .......... .......... .......... 77% 68.6M 3s
206600K .......... .......... .......... .......... .......... 77% 106M 3s
206650K .......... .......... .......... .......... .......... 77% 135M 3s
206700K .......... .......... .......... .......... .......... 77% 152M 3s
206750K .......... .......... .......... .......... .......... 77% 208M 3s
206800K .......... .......... .......... .......... .......... 77% 66.3M 3s
206850K .......... .......... .......... .......... .......... 77% 110M 3s
206900K .......... .......... .......... .......... .......... 77% 187M 3s
206950K .......... .......... .......... .......... .......... 77% 104M 3s
207000K .......... .......... .......... .......... .......... 77% 189M 3s
207050K .......... .......... .......... .......... .......... 77% 193M 3s
207100K .......... .......... .......... .......... .......... 77% 165M 3s
207150K .......... .......... .......... .......... .......... 77% 187M 3s
207200K .......... .......... .......... .......... .......... 77% 2.29M 3s
207250K .......... .......... .......... .......... .......... 78% 215M 3s
207300K .......... .......... .......... .......... .......... 78% 226M 3s
207350K .......... .......... .......... .......... .......... 78% 192M 3s
207400K .......... .......... .......... .......... .......... 78% 164M 3s
207450K .......... .......... .......... .......... .......... 78% 199M 3s
207500K .......... .......... .......... .......... .......... 78% 230M 3s
207550K .......... .......... .......... .......... .......... 78% 236M 3s
207600K .......... .......... .......... .......... .......... 78% 172M 3s
207650K .......... .......... .......... .......... .......... 78% 222M 3s
207700K .......... .......... .......... .......... .......... 78% 86.1M 3s
207750K .......... .......... .......... .......... .......... 78% 138M 3s
207800K .......... .......... .......... .......... .......... 78% 117M 3s
207850K .......... .......... .......... .......... .......... 78% 78.4M 3s
207900K .......... .......... .......... .......... .......... 78% 2.38M 3s
207950K .......... .......... .......... .......... .......... 78% 56.5M 3s
208000K .......... .......... .......... .......... .......... 78% 110M 3s
208050K .......... .......... .......... .......... .......... 78% 196M 3s
208100K .......... .......... .......... .......... .......... 78% 191M 3s
208150K .......... .......... .......... .......... .......... 78% 221M 3s
208200K .......... .......... .......... .......... .......... 78% 109M 3s
208250K .......... .......... .......... .......... .......... 78% 154M 3s
208300K .......... .......... .......... .......... .......... 78% 148M 3s
208350K .......... .......... .......... .......... .......... 78% 169M 3s
208400K .......... .......... .......... .......... .......... 78% 222M 3s
208450K .......... .......... .......... .......... .......... 78% 196M 3s
208500K .......... .......... .......... .......... .......... 78% 227M 3s
208550K .......... .......... .......... .......... .......... 78% 219M 3s
208600K .......... .......... .......... .......... .......... 78% 947K 3s
208650K .......... .......... .......... .......... .......... 78% 215M 3s
208700K .......... .......... .......... .......... .......... 78% 189M 3s
208750K .......... .......... .......... .......... .......... 78% 222M 3s
208800K .......... .......... .......... .......... .......... 78% 226M 3s
208850K .......... .......... .......... .......... .......... 78% 105M 3s
208900K .......... .......... .......... .......... .......... 78% 36.1M 3s
208950K .......... .......... .......... .......... .......... 78% 184M 3s
209000K .......... .......... .......... .......... .......... 78% 217M 3s
209050K .......... .......... .......... .......... .......... 78% 225M 3s
209100K .......... .......... .......... .......... .......... 78% 174M 3s
209150K .......... .......... .......... .......... .......... 78% 223M 3s
209200K .......... .......... .......... .......... .......... 78% 177M 3s
209250K .......... .......... .......... .......... .......... 78% 218M 3s
209300K .......... .......... .......... .......... .......... 78% 1.78M 3s
209350K .......... .......... .......... .......... .......... 78% 133M 3s
209400K .......... .......... .......... .......... .......... 78% 185M 3s
209450K .......... .......... .......... .......... .......... 78% 3.85M 3s
209500K .......... .......... .......... .......... .......... 78% 176M 3s
209550K .......... .......... .......... .......... .......... 78% 24.7M 3s
209600K .......... .......... .......... .......... .......... 78% 82.6M 3s
209650K .......... .......... .......... .......... .......... 78% 136M 3s
209700K .......... .......... .......... .......... .......... 78% 161M 3s
209750K .......... .......... .......... .......... .......... 78% 143M 3s
209800K .......... .......... .......... .......... .......... 78% 96.9M 3s
209850K .......... .......... .......... .......... .......... 78% 153M 3s
209900K .......... .......... .......... .......... .......... 79% 92.1M 3s
209950K .......... .......... .......... .......... .......... 79% 116M 3s
210000K .......... .......... .......... .......... .......... 79% 1.29M 3s
210050K .......... .......... .......... .......... .......... 79% 210M 3s
210100K .......... .......... .......... .......... .......... 79% 142M 3s
210150K .......... .......... .......... .......... .......... 79% 228M 3s
210200K .......... .......... .......... .......... .......... 79% 191M 3s
210250K .......... .......... .......... .......... .......... 79% 80.2M 3s
210300K .......... .......... .......... .......... .......... 79% 145M 3s
210350K .......... .......... .......... .......... .......... 79% 194M 3s
210400K .......... .......... .......... .......... .......... 79% 88.1M 3s
210450K .......... .......... .......... .......... .......... 79% 159M 3s
210500K .......... .......... .......... .......... .......... 79% 124M 3s
210550K .......... .......... .......... .......... .......... 79% 90.8M 3s
210600K .......... .......... .......... .......... .......... 79% 178M 3s
210650K .......... .......... .......... .......... .......... 79% 188M 3s
210700K .......... .......... .......... .......... .......... 79% 2.36M 3s
210750K .......... .......... .......... .......... .......... 79% 224M 3s
210800K .......... .......... .......... .......... .......... 79% 233M 3s
210850K .......... .......... .......... .......... .......... 79% 197M 3s
210900K .......... .......... .......... .......... .......... 79% 124M 3s
210950K .......... .......... .......... .......... .......... 79% 195M 3s
211000K .......... .......... .......... .......... .......... 79% 229M 3s
211050K .......... .......... .......... .......... .......... 79% 224M 3s
211100K .......... .......... .......... .......... .......... 79% 199M 3s
211150K .......... .......... .......... .......... .......... 79% 144M 3s
211200K .......... .......... .......... .......... .......... 79% 184M 3s
211250K .......... .......... .......... .......... .......... 79% 226M 3s
211300K .......... .......... .......... .......... .......... 79% 144M 3s
211350K .......... .......... .......... .......... .......... 79% 180M 3s
211400K .......... .......... .......... .......... .......... 79% 2.41M 3s
211450K .......... .......... .......... .......... .......... 79% 135M 3s
211500K .......... .......... .......... .......... .......... 79% 90.4M 3s
211550K .......... .......... .......... .......... .......... 79% 96.9M 3s
211600K .......... .......... .......... .......... .......... 79% 136M 3s
211650K .......... .......... .......... .......... .......... 79% 133M 3s
211700K .......... .......... .......... .......... .......... 79% 111M 3s
211750K .......... .......... .......... .......... .......... 79% 99.6M 3s
211800K .......... .......... .......... .......... .......... 79% 142M 3s
211850K .......... .......... .......... .......... .......... 79% 180M 3s
211900K .......... .......... .......... .......... .......... 79% 163M 3s
211950K .......... .......... .......... .......... .......... 79% 66.5M 3s
212000K .......... .......... .......... .......... .......... 79% 98.2M 3s
212050K .......... .......... .......... .......... .......... 79% 120M 3s
212100K .......... .......... .......... .......... .......... 79% 795K 3s
212150K .......... .......... .......... .......... .......... 79% 12.0M 3s
212200K .......... .......... .......... .......... .......... 79% 100M 3s
212250K .......... .......... .......... .......... .......... 79% 4.67M 3s
212300K .......... .......... .......... .......... .......... 79% 122M 3s
212350K .......... .......... .......... .......... .......... 79% 189M 3s
212400K .......... .......... .......... .......... .......... 79% 210M 3s
212450K .......... .......... .......... .......... .......... 79% 136M 3s
212500K .......... .......... .......... .......... .......... 79% 183M 3s
212550K .......... .......... .......... .......... .......... 80% 226M 3s
212600K .......... .......... .......... .......... .......... 80% 182M 3s
212650K .......... .......... .......... .......... .......... 80% 224M 3s
212700K .......... .......... .......... .......... .......... 80% 202M 2s
212750K .......... .......... .......... .......... .......... 80% 234M 2s
212800K .......... .......... .......... .......... .......... 80% 1.80M 2s
212850K .......... .......... .......... .......... .......... 80% 144M 2s
212900K .......... .......... .......... .......... .......... 80% 171M 2s
212950K .......... .......... .......... .......... .......... 80% 95.0M 2s
213000K .......... .......... .......... .......... .......... 80% 82.2M 2s
213050K .......... .......... .......... .......... .......... 80% 130M 2s
213100K .......... .......... .......... .......... .......... 80% 117M 2s
213150K .......... .......... .......... .......... .......... 80% 131M 2s
213200K .......... .......... .......... .......... .......... 80% 154M 2s
213250K .......... .......... .......... .......... .......... 80% 180M 2s
213300K .......... .......... .......... .......... .......... 80% 190M 2s
213350K .......... .......... .......... .......... .......... 80% 64.0M 2s
213400K .......... .......... .......... .......... .......... 80% 12.3M 2s
213450K .......... .......... .......... .......... .......... 80% 118M 2s
213500K .......... .......... .......... .......... .......... 80% 1.39M 2s
213550K .......... .......... .......... .......... .......... 80% 216M 2s
213600K .......... .......... .......... .......... .......... 80% 171M 2s
213650K .......... .......... .......... .......... .......... 80% 175M 2s
213700K .......... .......... .......... .......... .......... 80% 110M 2s
213750K .......... .......... .......... .......... .......... 80% 203M 2s
213800K .......... .......... .......... .......... .......... 80% 210M 2s
213850K .......... .......... .......... .......... .......... 80% 169M 2s
213900K .......... .......... .......... .......... .......... 80% 182M 2s
213950K .......... .......... .......... .......... .......... 80% 124M 2s
214000K .......... .......... .......... .......... .......... 80% 10.7M 2s
214050K .......... .......... .......... .......... .......... 80% 200M 2s
214100K .......... .......... .......... .......... .......... 80% 15.3M 2s
214150K .......... .......... .......... .......... .......... 80% 28.6M 2s
214200K .......... .......... .......... .......... .......... 80% 2.18M 2s
214250K .......... .......... .......... .......... .......... 80% 161M 2s
214300K .......... .......... .......... .......... .......... 80% 198M 2s
214350K .......... .......... .......... .......... .......... 80% 125M 2s
214400K .......... .......... .......... .......... .......... 80% 173M 2s
214450K .......... .......... .......... .......... .......... 80% 108M 2s
214500K .......... .......... .......... .......... .......... 80% 84.0M 2s
214550K .......... .......... .......... .......... .......... 80% 145M 2s
214600K .......... .......... .......... .......... .......... 80% 7.27M 2s
214650K .......... .......... .......... .......... .......... 80% 220M 2s
214700K .......... .......... .......... .......... .......... 80% 186M 2s
214750K .......... .......... .......... .......... .......... 80% 218M 2s
214800K .......... .......... .......... .......... .......... 80% 15.8M 2s
214850K .......... .......... .......... .......... .......... 80% 192M 2s
214900K .......... .......... .......... .......... .......... 80% 1.74M 2s
214950K .......... .......... .......... .......... .......... 80% 197M 2s
215000K .......... .......... .......... .......... .......... 80% 94.6M 2s
215050K .......... .......... .......... .......... .......... 80% 234M 2s
215100K .......... .......... .......... .......... .......... 80% 208M 2s
215150K .......... .......... .......... .......... .......... 80% 242M 2s
215200K .......... .......... .......... .......... .......... 81% 178M 2s
215250K .......... .......... .......... .......... .......... 81% 227M 2s
215300K .......... .......... .......... .......... .......... 81% 242M 2s
215350K .......... .......... .......... .......... .......... 81% 196M 2s
215400K .......... .......... .......... .......... .......... 81% 211M 2s
215450K .......... .......... .......... .......... .......... 81% 172M 2s
215500K .......... .......... .......... .......... .......... 81% 151M 2s
215550K .......... .......... .......... .......... .......... 81% 166M 2s
215600K .......... .......... .......... .......... .......... 81% 1.32M 2s
215650K .......... .......... .......... .......... .......... 81% 20.2M 2s
215700K .......... .......... .......... .......... .......... 81% 25.8M 2s
215750K .......... .......... .......... .......... .......... 81% 4.85M 2s
215800K .......... .......... .......... .......... .......... 81% 209M 2s
215850K .......... .......... .......... .......... .......... 81% 139M 2s
215900K .......... .......... .......... .......... .......... 81% 203M 2s
215950K .......... .......... .......... .......... .......... 81% 92.5M 2s
216000K .......... .......... .......... .......... .......... 81% 227M 2s
216050K .......... .......... .......... .......... .......... 81% 138M 2s
216100K .......... .......... .......... .......... .......... 81% 195M 2s
216150K .......... .......... .......... .......... .......... 81% 223M 2s
216200K .......... .......... .......... .......... .......... 81% 16.7M 2s
216250K .......... .......... .......... .......... .......... 81% 170M 2s
216300K .......... .......... .......... .......... .......... 81% 2.42M 2s
216350K .......... .......... .......... .......... .......... 81% 79.4M 2s
216400K .......... .......... .......... .......... .......... 81% 219M 2s
216450K .......... .......... .......... .......... .......... 81% 164M 2s
216500K .......... .......... .......... .......... .......... 81% 219M 2s
216550K .......... .......... .......... .......... .......... 81% 234M 2s
216600K .......... .......... .......... .......... .......... 81% 156M 2s
216650K .......... .......... .......... .......... .......... 81% 191M 2s
216700K .......... .......... .......... .......... .......... 81% 85.7M 2s
216750K .......... .......... .......... .......... .......... 81% 231M 2s
216800K .......... .......... .......... .......... .......... 81% 237M 2s
216850K .......... .......... .......... .......... .......... 81% 8.07M 2s
216900K .......... .......... .......... .......... .......... 81% 44.0M 2s
216950K .......... .......... .......... .......... .......... 81% 140M 2s
217000K .......... .......... .......... .......... .......... 81% 1.38M 2s
217050K .......... .......... .......... .......... .......... 81% 83.5M 2s
217100K .......... .......... .......... .......... .......... 81% 112M 2s
217150K .......... .......... .......... .......... .......... 81% 127M 2s
217200K .......... .......... .......... .......... .......... 81% 144M 2s
217250K .......... .......... .......... .......... .......... 81% 163M 2s
217300K .......... .......... .......... .......... .......... 81% 158M 2s
217350K .......... .......... .......... .......... .......... 81% 136M 2s
217400K .......... .......... .......... .......... .......... 81% 128M 2s
217450K .......... .......... .......... .......... .......... 81% 83.5M 2s
217500K .......... .......... .......... .......... .......... 81% 183M 2s
217550K .......... .......... .......... .......... .......... 81% 203M 2s
217600K .......... .......... .......... .......... .......... 81% 185M 2s
217650K .......... .......... .......... .......... .......... 81% 61.8M 2s
217700K .......... .......... .......... .......... .......... 81% 1.72M 2s
217750K .......... .......... .......... .......... .......... 81% 78.5M 2s
217800K .......... .......... .......... .......... .......... 81% 112M 2s
217850K .......... .......... .......... .......... .......... 82% 122M 2s
217900K .......... .......... .......... .......... .......... 82% 152M 2s
217950K .......... .......... .......... .......... .......... 82% 156M 2s
218000K .......... .......... .......... .......... .......... 82% 154M 2s
218050K .......... .......... .......... .......... .......... 82% 157M 2s
218100K .......... .......... .......... .......... .......... 82% 40.5M 2s
218150K .......... .......... .......... .......... .......... 82% 158M 2s
218200K .......... .......... .......... .......... .......... 82% 107M 2s
218250K .......... .......... .......... .......... .......... 82% 161M 2s
218300K .......... .......... .......... .......... .......... 82% 191M 2s
218350K .......... .......... .......... .......... .......... 82% 27.0M 2s
218400K .......... .......... .......... .......... .......... 82% 1.88M 2s
218450K .......... .......... .......... .......... .......... 82% 106M 2s
218500K .......... .......... .......... .......... .......... 82% 160M 2s
218550K .......... .......... .......... .......... .......... 82% 108M 2s
218600K .......... .......... .......... .......... .......... 82% 7.12M 2s
218650K .......... .......... .......... .......... .......... 82% 148M 2s
218700K .......... .......... .......... .......... .......... 82% 68.8M 2s
218750K .......... .......... .......... .......... .......... 82% 206M 2s
218800K .......... .......... .......... .......... .......... 82% 220M 2s
218850K .......... .......... .......... .......... .......... 82% 194M 2s
218900K .......... .......... .......... .......... .......... 82% 25.6M 2s
218950K .......... .......... .......... .......... .......... 82% 10.8M 2s
219000K .......... .......... .......... .......... .......... 82% 87.8M 2s
219050K .......... .......... .......... .......... .......... 82% 208M 2s
219100K .......... .......... .......... .......... .......... 82% 1.86M 2s
219150K .......... .......... .......... .......... .......... 82% 33.8M 2s
219200K .......... .......... .......... .......... .......... 82% 186M 2s
219250K .......... .......... .......... .......... .......... 82% 228M 2s
219300K .......... .......... .......... .......... .......... 82% 219M 2s
219350K .......... .......... .......... .......... .......... 82% 61.7M 2s
219400K .......... .......... .......... .......... .......... 82% 228M 2s
219450K .......... .......... .......... .......... .......... 82% 148M 2s
219500K .......... .......... .......... .......... .......... 82% 217M 2s
219550K .......... .......... .......... .......... .......... 82% 216M 2s
219600K .......... .......... .......... .......... .......... 82% 173M 2s
219650K .......... .......... .......... .......... .......... 82% 233M 2s
219700K .......... .......... .......... .......... .......... 82% 204M 2s
219750K .......... .......... .......... .......... .......... 82% 243M 2s
219800K .......... .......... .......... .......... .......... 82% 2.47M 2s
219850K .......... .......... .......... .......... .......... 82% 28.9M 2s
219900K .......... .......... .......... .......... .......... 82% 218M 2s
219950K .......... .......... .......... .......... .......... 82% 187M 2s
220000K .......... .......... .......... .......... .......... 82% 204M 2s
220050K .......... .......... .......... .......... .......... 82% 165M 2s
220100K .......... .......... .......... .......... .......... 82% 189M 2s
220150K .......... .......... .......... .......... .......... 82% 118M 2s
220200K .......... .......... .......... .......... .......... 82% 51.2M 2s
220250K .......... .......... .......... .......... .......... 82% 208M 2s
220300K .......... .......... .......... .......... .......... 82% 216M 2s
220350K .......... .......... .......... .......... .......... 82% 193M 2s
220400K .......... .......... .......... .......... .......... 82% 214M 2s
220450K .......... .......... .......... .......... .......... 82% 188M 2s
220500K .......... .......... .......... .......... .......... 82% 1.96M 2s
220550K .......... .......... .......... .......... .......... 83% 140M 2s
220600K .......... .......... .......... .......... .......... 83% 196M 2s
220650K .......... .......... .......... .......... .......... 83% 155M 2s
220700K .......... .......... .......... .......... .......... 83% 138M 2s
220750K .......... .......... .......... .......... .......... 83% 176M 2s
220800K .......... .......... .......... .......... .......... 83% 186M 2s
220850K .......... .......... .......... .......... .......... 83% 73.8M 2s
220900K .......... .......... .......... .......... .......... 83% 213M 2s
220950K .......... .......... .......... .......... .......... 83% 131M 2s
221000K .......... .......... .......... .......... .......... 83% 205M 2s
221050K .......... .......... .......... .......... .......... 83% 222M 2s
221100K .......... .......... .......... .......... .......... 83% 70.9M 2s
221150K .......... .......... .......... .......... .......... 83% 18.0M 2s
221200K .......... .......... .......... .......... .......... 83% 2.38M 2s
221250K .......... .......... .......... .......... .......... 83% 142M 2s
221300K .......... .......... .......... .......... .......... 83% 204M 2s
221350K .......... .......... .......... .......... .......... 83% 142M 2s
221400K .......... .......... .......... .......... .......... 83% 201M 2s
221450K .......... .......... .......... .......... .......... 83% 182M 2s
221500K .......... .......... .......... .......... .......... 83% 212M 2s
221550K .......... .......... .......... .......... .......... 83% 206M 2s
221600K .......... .......... .......... .......... .......... 83% 180M 2s
221650K .......... .......... .......... .......... .......... 83% 155M 2s
221700K .......... .......... .......... .......... .......... 83% 180M 2s
221750K .......... .......... .......... .......... .......... 83% 212M 2s
221800K .......... .......... .......... .......... .......... 83% 204M 2s
221850K .......... .......... .......... .......... .......... 83% 181M 2s
221900K .......... .......... .......... .......... .......... 83% 150M 2s
221950K .......... .......... .......... .......... .......... 83% 2.44M 2s
222000K .......... .......... .......... .......... .......... 83% 214M 2s
222050K .......... .......... .......... .......... .......... 83% 138M 2s
222100K .......... .......... .......... .......... .......... 83% 175M 2s
222150K .......... .......... .......... .......... .......... 83% 221M 2s
222200K .......... .......... .......... .......... .......... 83% 98.8M 2s
222250K .......... .......... .......... .......... .......... 83% 117M 2s
222300K .......... .......... .......... .......... .......... 83% 57.9M 2s
222350K .......... .......... .......... .......... .......... 83% 77.0M 2s
222400K .......... .......... .......... .......... .......... 83% 147M 2s
222450K .......... .......... .......... .......... .......... 83% 166M 2s
222500K .......... .......... .......... .......... .......... 83% 182M 2s
222550K .......... .......... .......... .......... .......... 83% 58.0M 2s
222600K .......... .......... .......... .......... .......... 83% 65.6M 2s
222650K .......... .......... .......... .......... .......... 83% 2.44M 2s
222700K .......... .......... .......... .......... .......... 83% 103M 2s
222750K .......... .......... .......... .......... .......... 83% 145M 2s
222800K .......... .......... .......... .......... .......... 83% 163M 2s
222850K .......... .......... .......... .......... .......... 83% 102M 2s
222900K .......... .......... .......... .......... .......... 83% 171M 2s
222950K .......... .......... .......... .......... .......... 83% 74.2M 2s
223000K .......... .......... .......... .......... .......... 83% 189M 2s
223050K .......... .......... .......... .......... .......... 83% 181M 2s
223100K .......... .......... .......... .......... .......... 83% 166M 2s
223150K .......... .......... .......... .......... .......... 83% 21.6M 2s
223200K .......... .......... .......... .......... .......... 84% 113M 2s
223250K .......... .......... .......... .......... .......... 84% 24.8M 2s
223300K .......... .......... .......... .......... .......... 84% 219M 2s
223350K .......... .......... .......... .......... .......... 84% 2.34M 2s
223400K .......... .......... .......... .......... .......... 84% 213M 2s
223450K .......... .......... .......... .......... .......... 84% 199M 2s
223500K .......... .......... .......... .......... .......... 84% 89.8M 2s
223550K .......... .......... .......... .......... .......... 84% 227M 2s
223600K .......... .......... .......... .......... .......... 84% 205M 2s
223650K .......... .......... .......... .......... .......... 84% 236M 2s
223700K .......... .......... .......... .......... .......... 84% 206M 2s
223750K .......... .......... .......... .......... .......... 84% 229M 2s
223800K .......... .......... .......... .......... .......... 84% 236M 2s
223850K .......... .......... .......... .......... .......... 84% 203M 2s
223900K .......... .......... .......... .......... .......... 84% 234M 2s
223950K .......... .......... .......... .......... .......... 84% 209M 2s
224000K .......... .......... .......... .......... .......... 84% 241M 2s
224050K .......... .......... .......... .......... .......... 84% 1.71M 2s
224100K .......... .......... .......... .......... .......... 84% 54.9M 2s
224150K .......... .......... .......... .......... .......... 84% 154M 2s
224200K .......... .......... .......... .......... .......... 84% 95.9M 2s
224250K .......... .......... .......... .......... .......... 84% 21.0M 2s
224300K .......... .......... .......... .......... .......... 84% 139M 2s
224350K .......... .......... .......... .......... .......... 84% 189M 2s
224400K .......... .......... .......... .......... .......... 84% 195M 2s
224450K .......... .......... .......... .......... .......... 84% 71.6M 2s
224500K .......... .......... .......... .......... .......... 84% 54.5M 2s
224550K .......... .......... .......... .......... .......... 84% 96.3M 2s
224600K .......... .......... .......... .......... .......... 84% 193M 2s
224650K .......... .......... .......... .......... .......... 84% 209M 2s
224700K .......... .......... .......... .......... .......... 84% 11.1M 2s
224750K .......... .......... .......... .......... .......... 84% 2.38M 2s
224800K .......... .......... .......... .......... .......... 84% 105M 2s
224850K .......... .......... .......... .......... .......... 84% 127M 2s
224900K .......... .......... .......... .......... .......... 84% 74.2M 2s
224950K .......... .......... .......... .......... .......... 84% 56.5M 2s
225000K .......... .......... .......... .......... .......... 84% 35.9M 2s
225050K .......... .......... .......... .......... .......... 84% 39.6M 2s
225100K .......... .......... .......... .......... .......... 84% 182M 2s
225150K .......... .......... .......... .......... .......... 84% 59.0M 2s
225200K .......... .......... .......... .......... .......... 84% 32.0M 2s
225250K .......... .......... .......... .......... .......... 84% 44.8M 2s
225300K .......... .......... .......... .......... .......... 84% 121M 2s
225350K .......... .......... .......... .......... .......... 84% 189M 2s
225400K .......... .......... .......... .......... .......... 84% 214M 2s
225450K .......... .......... .......... .......... .......... 84% 187M 2s
225500K .......... .......... .......... .......... .......... 84% 2.52M 2s
225550K .......... .......... .......... .......... .......... 84% 196M 2s
225600K .......... .......... .......... .......... .......... 84% 188M 2s
225650K .......... .......... .......... .......... .......... 84% 210M 2s
225700K .......... .......... .......... .......... .......... 84% 191M 2s
225750K .......... .......... .......... .......... .......... 84% 214M 2s
225800K .......... .......... .......... .......... .......... 84% 166M 2s
225850K .......... .......... .......... .......... .......... 85% 195M 2s
225900K .......... .......... .......... .......... .......... 85% 234M 2s
225950K .......... .......... .......... .......... .......... 85% 200M 2s
226000K .......... .......... .......... .......... .......... 85% 228M 2s
226050K .......... .......... .......... .......... .......... 85% 236M 2s
226100K .......... .......... .......... .......... .......... 85% 203M 2s
226150K .......... .......... .......... .......... .......... 85% 227M 2s
226200K .......... .......... .......... .......... .......... 85% 2.42M 2s
226250K .......... .......... .......... .......... .......... 85% 199M 2s
226300K .......... .......... .......... .......... .......... 85% 48.0M 2s
226350K .......... .......... .......... .......... .......... 85% 127M 2s
226400K .......... .......... .......... .......... .......... 85% 149M 2s
226450K .......... .......... .......... .......... .......... 85% 105M 2s
226500K .......... .......... .......... .......... .......... 85% 211M 2s
226550K .......... .......... .......... .......... .......... 85% 208M 2s
226600K .......... .......... .......... .......... .......... 85% 138M 2s
226650K .......... .......... .......... .......... .......... 85% 210M 2s
226700K .......... .......... .......... .......... .......... 85% 28.6M 2s
226750K .......... .......... .......... .......... .......... 85% 199M 2s
226800K .......... .......... .......... .......... .......... 85% 228M 2s
226850K .......... .......... .......... .......... .......... 85% 43.6M 2s
226900K .......... .......... .......... .......... .......... 85% 2.33M 2s
226950K .......... .......... .......... .......... .......... 85% 3.68M 2s
227000K .......... .......... .......... .......... .......... 85% 227M 2s
227050K .......... .......... .......... .......... .......... 85% 234M 2s
227100K .......... .......... .......... .......... .......... 85% 197M 2s
227150K .......... .......... .......... .......... .......... 85% 229M 2s
227200K .......... .......... .......... .......... .......... 85% 195M 2s
227250K .......... .......... .......... .......... .......... 85% 230M 2s
227300K .......... .......... .......... .......... .......... 85% 35.6M 2s
227350K .......... .......... .......... .......... .......... 85% 191M 2s
227400K .......... .......... .......... .......... .......... 85% 84.6M 2s
227450K .......... .......... .......... .......... .......... 85% 189M 2s
227500K .......... .......... .......... .......... .......... 85% 226M 2s
227550K .......... .......... .......... .......... .......... 85% 104M 2s
227600K .......... .......... .......... .......... .......... 85% 8.87M 2s
227650K .......... .......... .......... .......... .......... 85% 2.29M 2s
227700K .......... .......... .......... .......... .......... 85% 154M 2s
227750K .......... .......... .......... .......... .......... 85% 212M 2s
227800K .......... .......... .......... .......... .......... 85% 182M 2s
227850K .......... .......... .......... .......... .......... 85% 194M 2s
227900K .......... .......... .......... .......... .......... 85% 228M 2s
227950K .......... .......... .......... .......... .......... 85% 195M 2s
228000K .......... .......... .......... .......... .......... 85% 220M 2s
228050K .......... .......... .......... .......... .......... 85% 125M 2s
228100K .......... .......... .......... .......... .......... 85% 188M 2s
228150K .......... .......... .......... .......... .......... 85% 222M 2s
228200K .......... .......... .......... .......... .......... 85% 198M 2s
228250K .......... .......... .......... .......... .......... 85% 219M 2s
228300K .......... .......... .......... .......... .......... 85% 213M 2s
228350K .......... .......... .......... .......... .......... 85% 1.14M 2s
228400K .......... .......... .......... .......... .......... 85% 76.3M 2s
228450K .......... .......... .......... .......... .......... 85% 182M 2s
228500K .......... .......... .......... .......... .......... 86% 226M 2s
228550K .......... .......... .......... .......... .......... 86% 154M 2s
228600K .......... .......... .......... .......... .......... 86% 1.53M 2s
228650K .......... .......... .......... .......... .......... 86% 207M 2s
228700K .......... .......... .......... .......... .......... 86% 192M 2s
228750K .......... .......... .......... .......... .......... 86% 108M 2s
228800K .......... .......... .......... .......... .......... 86% 222M 2s
228850K .......... .......... .......... .......... .......... 86% 179M 2s
228900K .......... .......... .......... .......... .......... 86% 231M 2s
228950K .......... .......... .......... .......... .......... 86% 200M 2s
229000K .......... .......... .......... .......... .......... 86% 233M 2s
229050K .......... .......... .......... .......... .......... 86% 2.33M 2s
229100K .......... .......... .......... .......... .......... 86% 128M 2s
229150K .......... .......... .......... .......... .......... 86% 27.6M 2s
229200K .......... .......... .......... .......... .......... 86% 153M 2s
229250K .......... .......... .......... .......... .......... 86% 207M 2s
229300K .......... .......... .......... .......... .......... 86% 114M 2s
229350K .......... .......... .......... .......... .......... 86% 98.0M 2s
229400K .......... .......... .......... .......... .......... 86% 195M 2s
229450K .......... .......... .......... .......... .......... 86% 171M 2s
229500K .......... .......... .......... .......... .......... 86% 151M 2s
229550K .......... .......... .......... .......... .......... 86% 208M 2s
229600K .......... .......... .......... .......... .......... 86% 179M 2s
229650K .......... .......... .......... .......... .......... 86% 214M 2s
229700K .......... .......... .......... .......... .......... 86% 191M 2s
229750K .......... .......... .......... .......... .......... 86% 161M 2s
229800K .......... .......... .......... .......... .......... 86% 2.10M 2s
229850K .......... .......... .......... .......... .......... 86% 138M 2s
229900K .......... .......... .......... .......... .......... 86% 102M 2s
229950K .......... .......... .......... .......... .......... 86% 153M 2s
230000K .......... .......... .......... .......... .......... 86% 182M 2s
230050K .......... .......... .......... .......... .......... 86% 185M 2s
230100K .......... .......... .......... .......... .......... 86% 198M 2s
230150K .......... .......... .......... .......... .......... 86% 157M 2s
230200K .......... .......... .......... .......... .......... 86% 158M 2s
230250K .......... .......... .......... .......... .......... 86% 156M 2s
230300K .......... .......... .......... .......... .......... 86% 175M 2s
230350K .......... .......... .......... .......... .......... 86% 159M 2s
230400K .......... .......... .......... .......... .......... 86% 101M 2s
230450K .......... .......... .......... .......... .......... 86% 161M 2s
230500K .......... .......... .......... .......... .......... 86% 2.29M 2s
230550K .......... .......... .......... .......... .......... 86% 188M 2s
230600K .......... .......... .......... .......... .......... 86% 103M 2s
230650K .......... .......... .......... .......... .......... 86% 195M 2s
230700K .......... .......... .......... .......... .......... 86% 166M 2s
230750K .......... .......... .......... .......... .......... 86% 215M 2s
230800K .......... .......... .......... .......... .......... 86% 224M 2s
230850K .......... .......... .......... .......... .......... 86% 4.27M 2s
230900K .......... .......... .......... .......... .......... 86% 148M 2s
230950K .......... .......... .......... .......... .......... 86% 190M 2s
231000K .......... .......... .......... .......... .......... 86% 226M 2s
231050K .......... .......... .......... .......... .......... 86% 228M 2s
231100K .......... .......... .......... .......... .......... 86% 95.9M 2s
231150K .......... .......... .......... .......... .......... 87% 36.6M 2s
231200K .......... .......... .......... .......... .......... 87% 1.13M 2s
231250K .......... .......... .......... .......... .......... 87% 64.0M 2s
231300K .......... .......... .......... .......... .......... 87% 168M 2s
231350K .......... .......... .......... .......... .......... 87% 192M 2s
231400K .......... .......... .......... .......... .......... 87% 99.2M 2s
231450K .......... .......... .......... .......... .......... 87% 28.0M 2s
231500K .......... .......... .......... .......... .......... 87% 211M 2s
231550K .......... .......... .......... .......... .......... 87% 223M 2s
231600K .......... .......... .......... .......... .......... 87% 53.7M 2s
231650K .......... .......... .......... .......... .......... 87% 67.7M 2s
231700K .......... .......... .......... .......... .......... 87% 186M 2s
231750K .......... .......... .......... .......... .......... 87% 221M 2s
231800K .......... .......... .......... .......... .......... 87% 227M 2s
231850K .......... .......... .......... .......... .......... 87% 166M 2s
231900K .......... .......... .......... .......... .......... 87% 53.3M 2s
231950K .......... .......... .......... .......... .......... 87% 393K 2s
232000K .......... .......... .......... .......... .......... 87% 168M 2s
232050K .......... .......... .......... .......... .......... 87% 221M 2s
232100K .......... .......... .......... .......... .......... 87% 186M 2s
232150K .......... .......... .......... .......... .......... 87% 228M 2s
232200K .......... .......... .......... .......... .......... 87% 187M 2s
232250K .......... .......... .......... .......... .......... 87% 217M 2s
232300K .......... .......... .......... .......... .......... 87% 228M 2s
232350K .......... .......... .......... .......... .......... 87% 203M 2s
232400K .......... .......... .......... .......... .......... 87% 229M 2s
232450K .......... .......... .......... .......... .......... 87% 66.5M 2s
232500K .......... .......... .......... .......... .......... 87% 146M 2s
232550K .......... .......... .......... .......... .......... 87% 194M 2s
232600K .......... .......... .......... .......... .......... 87% 65.5M 2s
232650K .......... .......... .......... .......... .......... 87% 1.64M 2s
232700K .......... .......... .......... .......... .......... 87% 190M 2s
232750K .......... .......... .......... .......... .......... 87% 163M 2s
232800K .......... .......... .......... .......... .......... 87% 228M 2s
232850K .......... .......... .......... .......... .......... 87% 198M 2s
232900K .......... .......... .......... .......... .......... 87% 203M 2s
232950K .......... .......... .......... .......... .......... 87% 160M 2s
233000K .......... .......... .......... .......... .......... 87% 175M 2s
233050K .......... .......... .......... .......... .......... 87% 210M 2s
233100K .......... .......... .......... .......... .......... 87% 198M 2s
233150K .......... .......... .......... .......... .......... 87% 227M 2s
233200K .......... .......... .......... .......... .......... 87% 205M 2s
233250K .......... .......... .......... .......... .......... 87% 239M 2s
233300K .......... .......... .......... .......... .......... 87% 225M 2s
233350K .......... .......... .......... .......... .......... 87% 196M 2s
233400K .......... .......... .......... .......... .......... 87% 1.72M 2s
233450K .......... .......... .......... .......... .......... 87% 114M 2s
233500K .......... .......... .......... .......... .......... 87% 190M 2s
233550K .......... .......... .......... .......... .......... 87% 117M 2s
233600K .......... .......... .......... .......... .......... 87% 123M 2s
233650K .......... .......... .......... .......... .......... 87% 128M 2s
233700K .......... .......... .......... .......... .......... 87% 67.0M 2s
233750K .......... .......... .......... .......... .......... 87% 94.3M 2s
233800K .......... .......... .......... .......... .......... 88% 102M 2s
233850K .......... .......... .......... .......... .......... 88% 93.0M 2s
233900K .......... .......... .......... .......... .......... 88% 115M 2s
233950K .......... .......... .......... .......... .......... 88% 147M 2s
234000K .......... .......... .......... .......... .......... 88% 124M 2s
234050K .......... .......... .......... .......... .......... 88% 225M 2s
234100K .......... .......... .......... .......... .......... 88% 2.24M 2s
234150K .......... .......... .......... .......... .......... 88% 163M 2s
234200K .......... .......... .......... .......... .......... 88% 180M 2s
234250K .......... .......... .......... .......... .......... 88% 223M 2s
234300K .......... .......... .......... .......... .......... 88% 229M 2s
234350K .......... .......... .......... .......... .......... 88% 195M 1s
234400K .......... .......... .......... .......... .......... 88% 230M 1s
234450K .......... .......... .......... .......... .......... 88% 109M 1s
234500K .......... .......... .......... .......... .......... 88% 207M 1s
234550K .......... .......... .......... .......... .......... 88% 183M 1s
234600K .......... .......... .......... .......... .......... 88% 112M 1s
234650K .......... .......... .......... .......... .......... 88% 223M 1s
234700K .......... .......... .......... .......... .......... 88% 47.1M 1s
234750K .......... .......... .......... .......... .......... 88% 33.4M 1s
234800K .......... .......... .......... .......... .......... 88% 173M 1s
234850K .......... .......... .......... .......... .......... 88% 2.32M 1s
234900K .......... .......... .......... .......... .......... 88% 167M 1s
234950K .......... .......... .......... .......... .......... 88% 198M 1s
235000K .......... .......... .......... .......... .......... 88% 182M 1s
235050K .......... .......... .......... .......... .......... 88% 233M 1s
235100K .......... .......... .......... .......... .......... 88% 201M 1s
235150K .......... .......... .......... .......... .......... 88% 231M 1s
235200K .......... .......... .......... .......... .......... 88% 155M 1s
235250K .......... .......... .......... .......... .......... 88% 224M 1s
235300K .......... .......... .......... .......... .......... 88% 236M 1s
235350K .......... .......... .......... .......... .......... 88% 203M 1s
235400K .......... .......... .......... .......... .......... 88% 236M 1s
235450K .......... .......... .......... .......... .......... 88% 186M 1s
235500K .......... .......... .......... .......... .......... 88% 92.0M 1s
235550K .......... .......... .......... .......... .......... 88% 2.19M 1s
235600K .......... .......... .......... .......... .......... 88% 148M 1s
235650K .......... .......... .......... .......... .......... 88% 170M 1s
235700K .......... .......... .......... .......... .......... 88% 196M 1s
235750K .......... .......... .......... .......... .......... 88% 198M 1s
235800K .......... .......... .......... .......... .......... 88% 181M 1s
235850K .......... .......... .......... .......... .......... 88% 203M 1s
235900K .......... .......... .......... .......... .......... 88% 229M 1s
235950K .......... .......... .......... .......... .......... 88% 133M 1s
236000K .......... .......... .......... .......... .......... 88% 241M 1s
236050K .......... .......... .......... .......... .......... 88% 238M 1s
236100K .......... .......... .......... .......... .......... 88% 207M 1s
236150K .......... .......... .......... .......... .......... 88% 241M 1s
236200K .......... .......... .......... .......... .......... 88% 151M 1s
236250K .......... .......... .......... .......... .......... 88% 1.71M 1s
236300K .......... .......... .......... .......... .......... 88% 149M 1s
236350K .......... .......... .......... .......... .......... 88% 89.6M 1s
236400K .......... .......... .......... .......... .......... 88% 210M 1s
236450K .......... .......... .......... .......... .......... 89% 67.3M 1s
236500K .......... .......... .......... .......... .......... 89% 4.22M 1s
236550K .......... .......... .......... .......... .......... 89% 191M 1s
236600K .......... .......... .......... .......... .......... 89% 97.9M 1s
236650K .......... .......... .......... .......... .......... 89% 40.5M 1s
236700K .......... .......... .......... .......... .......... 89% 197M 1s
236750K .......... .......... .......... .......... .......... 89% 228M 1s
236800K .......... .......... .......... .......... .......... 89% 233M 1s
236850K .......... .......... .......... .......... .......... 89% 200M 1s
236900K .......... .......... .......... .......... .......... 89% 229M 1s
236950K .......... .......... .......... .......... .......... 89% 156M 1s
237000K .......... .......... .......... .......... .......... 89% 2.30M 1s
237050K .......... .......... .......... .......... .......... 89% 168M 1s
237100K .......... .......... .......... .......... .......... 89% 202M 1s
237150K .......... .......... .......... .......... .......... 89% 236M 1s
237200K .......... .......... .......... .......... .......... 89% 152M 1s
237250K .......... .......... .......... .......... .......... 89% 209M 1s
237300K .......... .......... .......... .......... .......... 89% 229M 1s
237350K .......... .......... .......... .......... .......... 89% 186M 1s
237400K .......... .......... .......... .......... .......... 89% 125M 1s
237450K .......... .......... .......... .......... .......... 89% 172M 1s
237500K .......... .......... .......... .......... .......... 89% 180M 1s
237550K .......... .......... .......... .......... .......... 89% 55.3M 1s
237600K .......... .......... .......... .......... .......... 89% 82.3M 1s
237650K .......... .......... .......... .......... .......... 89% 216M 1s
237700K .......... .......... .......... .......... .......... 89% 2.14M 1s
237750K .......... .......... .......... .......... .......... 89% 174M 1s
237800K .......... .......... .......... .......... .......... 89% 223M 1s
237850K .......... .......... .......... .......... .......... 89% 158M 1s
237900K .......... .......... .......... .......... .......... 89% 224M 1s
237950K .......... .......... .......... .......... .......... 89% 189M 1s
238000K .......... .......... .......... .......... .......... 89% 203M 1s
238050K .......... .......... .......... .......... .......... 89% 237M 1s
238100K .......... .......... .......... .......... .......... 89% 195M 1s
238150K .......... .......... .......... .......... .......... 89% 161M 1s
238200K .......... .......... .......... .......... .......... 89% 190M 1s
238250K .......... .......... .......... .......... .......... 89% 203M 1s
238300K .......... .......... .......... .......... .......... 89% 220M 1s
238350K .......... .......... .......... .......... .......... 89% 186M 1s
238400K .......... .......... .......... .......... .......... 89% 222M 1s
238450K .......... .......... .......... .......... .......... 89% 2.16M 1s
238500K .......... .......... .......... .......... .......... 89% 106M 1s
238550K .......... .......... .......... .......... .......... 89% 538K 1s
238600K .......... .......... .......... .......... .......... 89% 79.3M 1s
238650K .......... .......... .......... .......... .......... 89% 75.1M 1s
238700K .......... .......... .......... .......... .......... 89% 151M 1s
238750K .......... .......... .......... .......... .......... 89% 231M 1s
238800K .......... .......... .......... .......... .......... 89% 100M 1s
238850K .......... .......... .......... .......... .......... 89% 39.0M 1s
238900K .......... .......... .......... .......... .......... 89% 142M 1s
238950K .......... .......... .......... .......... .......... 89% 54.2M 1s
239000K .......... .......... .......... .......... .......... 89% 225M 1s
239050K .......... .......... .......... .......... .......... 89% 231M 1s
239100K .......... .......... .......... .......... .......... 89% 71.7M 1s
239150K .......... .......... .......... .......... .......... 90% 219M 1s
239200K .......... .......... .......... .......... .......... 90% 1.84M 1s
239250K .......... .......... .......... .......... .......... 90% 216M 1s
239300K .......... .......... .......... .......... .......... 90% 81.9M 1s
239350K .......... .......... .......... .......... .......... 90% 195M 1s
239400K .......... .......... .......... .......... .......... 90% 170M 1s
239450K .......... .......... .......... .......... .......... 90% 195M 1s
239500K .......... .......... .......... .......... .......... 90% 225M 1s
239550K .......... .......... .......... .......... .......... 90% 234M 1s
239600K .......... .......... .......... .......... .......... 90% 119M 1s
239650K .......... .......... .......... .......... .......... 90% 150M 1s
239700K .......... .......... .......... .......... .......... 90% 195M 1s
239750K .......... .......... .......... .......... .......... 90% 228M 1s
239800K .......... .......... .......... .......... .......... 90% 236M 1s
239850K .......... .......... .......... .......... .......... 90% 43.8M 1s
239900K .......... .......... .......... .......... .......... 90% 2.27M 1s
239950K .......... .......... .......... .......... .......... 90% 197M 1s
240000K .......... .......... .......... .......... .......... 90% 126M 1s
240050K .......... .......... .......... .......... .......... 90% 211M 1s
240100K .......... .......... .......... .......... .......... 90% 199M 1s
240150K .......... .......... .......... .......... .......... 90% 225M 1s
240200K .......... .......... .......... .......... .......... 90% 198M 1s
240250K .......... .......... .......... .......... .......... 90% 183M 1s
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240350K .......... .......... .......... .......... .......... 90% 196M 1s
240400K .......... .......... .......... .......... .......... 90% 235M 1s
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240600K .......... .......... .......... .......... .......... 90% 2.03M 1s
240650K .......... .......... .......... .......... .......... 90% 2.33M 1s
240700K .......... .......... .......... .......... .......... 90% 187M 1s
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240850K .......... .......... .......... .......... .......... 90% 195M 1s
240900K .......... .......... .......... .......... .......... 90% 225M 1s
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241000K .......... .......... .......... .......... .......... 90% 224M 1s
241050K .......... .......... .......... .......... .......... 90% 223M 1s
241100K .......... .......... .......... .......... .......... 90% 195M 1s
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241200K .......... .......... .......... .......... .......... 90% 194M 1s
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241300K .......... .......... .......... .......... .......... 90% 222M 1s
241350K .......... .......... .......... .......... .......... 90% 1.66M 1s
241400K .......... .......... .......... .......... .......... 90% 29.6M 1s
241450K .......... .......... .......... .......... .......... 90% 184M 1s
241500K .......... .......... .......... .......... .......... 90% 198M 1s
241550K .......... .......... .......... .......... .......... 90% 208M 1s
241600K .......... .......... .......... .......... .......... 90% 98.0M 1s
241650K .......... .......... .......... .......... .......... 90% 123M 1s
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241750K .......... .......... .......... .......... .......... 90% 219M 1s
241800K .......... .......... .......... .......... .......... 91% 215M 1s
241850K .......... .......... .......... .......... .......... 91% 93.0M 1s
241900K .......... .......... .......... .......... .......... 91% 110M 1s
241950K .......... .......... .......... .......... .......... 91% 181M 1s
242000K .......... .......... .......... .......... .......... 91% 211M 1s
242050K .......... .......... .......... .......... .......... 91% 233M 1s
242100K .......... .......... .......... .......... .......... 91% 2.15M 1s
242150K .......... .......... .......... .......... .......... 91% 198M 1s
242200K .......... .......... .......... .......... .......... 91% 59.9M 1s
242250K .......... .......... .......... .......... .......... 91% 22.9M 1s
242300K .......... .......... .......... .......... .......... 91% 220M 1s
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242400K .......... .......... .......... .......... .......... 91% 207M 1s
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242500K .......... .......... .......... .......... .......... 91% 198M 1s
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242800K .......... .......... .......... .......... .......... 91% 686K 1s
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243000K .......... .......... .......... .......... .......... 91% 235M 1s
243050K .......... .......... .......... .......... .......... 91% 239M 1s
243100K .......... .......... .......... .......... .......... 91% 210M 1s
243150K .......... .......... .......... .......... .......... 91% 237M 1s
243200K .......... .......... .......... .......... .......... 91% 209M 1s
243250K .......... .......... .......... .......... .......... 91% 195M 1s
243300K .......... .......... .......... .......... .......... 91% 236M 1s
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243400K .......... .......... .......... .......... .......... 91% 235M 1s
243450K .......... .......... .......... .......... .......... 91% 207M 1s
243500K .......... .......... .......... .......... .......... 91% 205M 1s
243550K .......... .......... .......... .......... .......... 91% 1.10M 1s
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243750K .......... .......... .......... .......... .......... 91% 176M 1s
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243850K .......... .......... .......... .......... .......... 91% 195M 1s
243900K .......... .......... .......... .......... .......... 91% 166M 1s
243950K .......... .......... .......... .......... .......... 91% 191M 1s
244000K .......... .......... .......... .......... .......... 91% 224M 1s
244050K .......... .......... .......... .......... .......... 91% 229M 1s
244100K .......... .......... .......... .......... .......... 91% 190M 1s
244150K .......... .......... .......... .......... .......... 91% 162M 1s
244200K .......... .......... .......... .......... .......... 91% 195M 1s
244250K .......... .......... .......... .......... .......... 91% 211M 1s
244300K .......... .......... .......... .......... .......... 91% 2.31M 1s
244350K .......... .......... .......... .......... .......... 91% 198M 1s
244400K .......... .......... .......... .......... .......... 91% 238M 1s
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244650K .......... .......... .......... .......... .......... 92% 237M 1s
244700K .......... .......... .......... .......... .......... 92% 130M 1s
244750K .......... .......... .......... .......... .......... 92% 81.8M 1s
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244850K .......... .......... .......... .......... .......... 92% 200M 1s
244900K .......... .......... .......... .......... .......... 92% 99.2M 1s
244950K .......... .......... .......... .......... .......... 92% 203M 1s
245000K .......... .......... .......... .......... .......... 92% 2.46M 1s
245050K .......... .......... .......... .......... .......... 92% 84.8M 1s
245100K .......... .......... .......... .......... .......... 92% 180M 1s
245150K .......... .......... .......... .......... .......... 92% 166M 1s
245200K .......... .......... .......... .......... .......... 92% 149M 1s
245250K .......... .......... .......... .......... .......... 92% 192M 1s
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245350K .......... .......... .......... .......... .......... 92% 155M 1s
245400K .......... .......... .......... .......... .......... 92% 89.6M 1s
245450K .......... .......... .......... .......... .......... 92% 111M 1s
245500K .......... .......... .......... .......... .......... 92% 171M 1s
245550K .......... .......... .......... .......... .......... 92% 208M 1s
245600K .......... .......... .......... .......... .......... 92% 189M 1s
245650K .......... .......... .......... .......... .......... 92% 200M 1s
245700K .......... .......... .......... .......... .......... 92% 187M 1s
245750K .......... .......... .......... .......... .......... 92% 2.28M 1s
245800K .......... .......... .......... .......... .......... 92% 66.1M 1s
245850K .......... .......... .......... .......... .......... 92% 180M 1s
245900K .......... .......... .......... .......... .......... 92% 215M 1s
245950K .......... .......... .......... .......... .......... 92% 184M 1s
246000K .......... .......... .......... .......... .......... 92% 218M 1s
246050K .......... .......... .......... .......... .......... 92% 208M 1s
246100K .......... .......... .......... .......... .......... 92% 185M 1s
246150K .......... .......... .......... .......... .......... 92% 218M 1s
246200K .......... .......... .......... .......... .......... 92% 8.12M 1s
246250K .......... .......... .......... .......... .......... 92% 152M 1s
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246350K .......... .......... .......... .......... .......... 92% 195M 1s
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246450K .......... .......... .......... .......... .......... 92% 119M 1s
246500K .......... .......... .......... .......... .......... 92% 2.25M 1s
246550K .......... .......... .......... .......... .......... 92% 223M 1s
246600K .......... .......... .......... .......... .......... 92% 195M 1s
246650K .......... .......... .......... .......... .......... 92% 58.6M 1s
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246750K .......... .......... .......... .......... .......... 92% 63.6M 1s
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246900K .......... .......... .......... .......... .......... 92% 217M 1s
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247000K .......... .......... .......... .......... .......... 92% 242M 1s
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247100K .......... .......... .......... .......... .......... 93% 175M 1s
247150K .......... .......... .......... .......... .......... 93% 229M 1s
247200K .......... .......... .......... .......... .......... 93% 2.28M 1s
247250K .......... .......... .......... .......... .......... 93% 217M 1s
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250000K .......... .......... .......... .......... .......... 94% 137M 1s
250050K .......... .......... .......... .......... .......... 94% 64.8M 1s
250100K .......... .......... .......... .......... .......... 94% 68.7M 1s
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250200K .......... .......... .......... .......... .......... 94% 9.63M 1s
250250K .......... .......... .......... .......... .......... 94% 205M 1s
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251000K .......... .......... .......... .......... .......... 94% 9.56M 1s
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251100K .......... .......... .......... .......... .......... 94% 32.7M 1s
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251800K .......... .......... .......... .......... .......... 94% 68.2M 1s
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252150K .......... .......... .......... .......... .......... 94% 144M 1s
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252250K .......... .......... .......... .......... .......... 94% 173M 1s
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253000K .......... .......... .......... .......... .......... 95% 125M 1s
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253150K .......... .......... .......... .......... .......... 95% 95.7M 1s
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254100K .......... .......... .......... .......... .......... 95% 1.97M 1s
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254550K .......... .......... .......... .......... .......... 95% 29.8M 1s
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2024-05-16 19:55:17 (20.1 MB/s) - ‘ESPbeta.tgz’ saved [272107101/272107101]
+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.5
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/config/
+ ./makeEnv
ESP runtime AutoConfigurator
CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0 with contents:
bin
include
lib
share
Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python found!
Info: Python header /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11/Python.h found!
Info: Python library /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin/libpython3.11.dylib found!
ESP_ARCH = DARWIN64
ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad
EFCOMP = gfortran
CARCH = DARWIN64
CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.7.0
CASARCH = .
CASREV = 7.7
PYTHONINC= /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11
PYTHONLIB= -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.7
++ CASREV=7.7
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11
++ PYTHONINC=/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11
++ export 'PYTHONLIB=-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11'
++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=
++ CAPS_GLYPH=
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESP/ESP.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/ESP/ESP.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/wvClient/wv.html'
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src
+ make
(cd EGADS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64
cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/DARWIN64
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/STANALYZER.make
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads_dot.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egads.inc
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/emp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/prm.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsserver.inc
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/wsss.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsTris.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineFit.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsSplineVels.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egadsf90.inc
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/Surreal/always_inline.h
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsGeom.cpp -o ./egadsGeom.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsHLevel.cpp -o ./egadsHLevel.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsTopo.cpp -o ./egadsTopo.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsCopy.cpp -o ./egadsCopy.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSpline.cpp -o ./egadsSpline.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsIO.cpp -o ./egadsIO.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsSkinning.cpp -o ./egadsSkinning.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include \
-I. egadsTessSens.cpp -o ./egadsTessSens.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsBase.c -o ./egadsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTess.c -o ./egadsTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsTris.c -o ./egadsTris.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsFit.c -o ./egadsFit.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmCfit.c -o ./prmCfit.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmGrid.c -o ./prmGrid.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap prmUV.c -o ./prmUV.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsExport.c -o ./egadsExport.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include ../util/emp.c \
-o ./emp.o
clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \
../util/evaluate.c -o ./evaluate.o
clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I. -I../include \
../util/rational.c -o ./rational.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -I../util \
../util/regQuads.c -o ./regQuads.o
clang++ -g -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1
SurrealD1_test_suite Complete!
clang++ -g -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4
SurrealD4_test_suite Complete!
clang++ -g -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1
SurrealS1_test_suite Complete!
clang++ -g -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
./SurrealS4
SurrealS4_test_suite Complete!
/Library/Developer/CommandLineTools/usr/bin/make -C ../util
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 uvmap/main/uvmap.c -Iuvmap \
-o ./uvmap.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 egadsUVmap.c -Iuvmap \
-o ./egadsUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a
clang -g -o ./uvmap.exe ./uvmap.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib
(cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \
egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -lc++ \
-install_name '@rpath/libegads.dylib' \
-compatibility_version 7.7 \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a
cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a
(cd .; \
ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \
evaluate.o rational.o regQuads.o; )
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsBase.c -o ./fgadsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsMemory.c -o ./fgadsMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsAttrs.c -o ./fgadsAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTess.c -o ./fgadsTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsHLevel.c -o ./fgadsHLevel.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsGeom.c -o ./fgadsGeom.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libfgads.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a emp.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libemp.a
*** EGADS Build Complete! ***
(cd EGADS/lite; make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o ./liteBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o ./liteMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o ./liteGeom.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o ./liteTopo.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o ./liteAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o ./liteImport.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o ./liteString.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o ./liteTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o ./liteTris.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I. -I../src \
../src/egadsQuads.c -o ./liteQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o ./liteTessInp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 ../src/egadsRobust.c \
-o ./egadsRobust.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DDARWIN64 -I../include ../util/emp.c \
-o ./emp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o ./evaLite.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE ../util/rational.c \
-o ./ratLite.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I../util \
../util/regQuads.c -o ./liteRegQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o ./liteEffect.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib
(cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslite.dylib \
liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \
egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \
liteEffect.o liteUVmap.o \
-install_name '@rpath/libegadslite.dylib' \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
liteUVmap.o ; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
(cd wvServer; make)
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 map.cpp -o ./map.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include handshake.c -o ./handshake.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include md5.c -o ./md5.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include parsers.c -o ./parsers.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include extension.c -o ./extension.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include sha-1.c -o ./sha-1.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include server.c -o ./server.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include wv.c -o ./wv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fwv.c -o ./fwv.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
./fwv.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -o ./servertest.o
clang++ -g -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.a \
-lpthread -lz -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib
(cd .; clang++ -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libwsserver.dylib \
base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \
-install_name '@rpath/libwsserver.dylib' \
-compatibility_version 7.7 \
-current_version 1.0.25 )
(cd EGADS/examples; make -f egads2cart.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include egads2cart.c \
-o ./egads2cart.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
(cd EGADS/examples; make -f vCurvature.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vCurvature ./vCurvature.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd EGADS/examples; make -f vGeom.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vGeom.c -o ./vGeom.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd EGADS/examples; make -f vTess.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vTess.c -o ./vTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include ../util/retessFaces.c \
-o ./retessFaces.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet \
-lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
(cd OpenCSM; make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udp.c -o ./udp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib
clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/warp.so ./udpWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads -lm -Wl,-w
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/OpenCSM.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h
cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/common.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h
cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h
cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/esp.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h
cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/tim.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h
cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/egg.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/udpUtilities.c
(cd Slugs; make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Fitter.c \
-o ./Fitter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. RedBlackTree.c \
-o ./RedBlackTree.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. Tessellate.c \
-o ./Tessellate.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lwsserver -legads \
-lpthread -lz -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads \
-lpthread -lz -lm
(cd CAPS; make)
/bin/cp Cart3D/OSX64_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/OSX64_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/DARWIN64/avl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/avl
/bin/cp Executables/DARWIN64/pplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/pplot
/bin/cp Executables/DARWIN64/pxplot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/pxplot
/bin/cp Executables/DARWIN64/xfoil /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/xfoil
/bin/cp Executables/DARWIN64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/DARWIN64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/DARWIN64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/DARWIN64/mses /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mses
/bin/cp Executables/DARWIN64/mset /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include
/bin/cp udunits/DARWIN64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib
/bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libudunits2.dylib
/bin/cp Libraries/DARWIN64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/DARWIN64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/DARWIN64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/aflr4AIM.so
(cd CAPS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/caps.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/capsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimUtil.h
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aimMesh.h
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o ./aimTransferUtil.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../include \
aimMesh.c -o ./aimMesh.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a
ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
./aimTransferUtil.o
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libaimUtil.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib
(cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
-install_name '@rpath/libcaps.dylib' \
-compatibility_version 1.0.25 \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libcapsstatic.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include testingAIM.c \
-o ./testingAIM.o
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so
rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include testingWriter.c \
-o ./testingWriter.o
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so
rm: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include phaseUtil.c \
-o ./phaseUtil.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
(cd ../CAPSexamples; make)
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include avlTest.c -o ./avlTest.o
clang -g -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
clang -g -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
clang -g -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
clang -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
clang -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
clang -g -o ./aeroelasticTest ./aeroelasticTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmTest.c -o ./hsmTest.o
clang -g -o ./hsmTest ./hsmTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o
clang -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o
clang -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o
clang -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include interferenceTest.c \
-o ./interferenceTest.o
clang -g -o ./interferenceTest ./interferenceTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include msesTest.c -o ./msesTest.o
clang -g -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include mystranTest.c -o ./mystranTest.o
clang -g -o ./mystranTest ./mystranTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
clang -g -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
(cd CAPS/aim; make)
/Library/Developer/CommandLineTools/usr/bin/make -C utils
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a
/Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libutils.a(attrUtils.o) has no symbols
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils
cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/aim/utils/vlmUtils.h
/Library/Developer/CommandLineTools/usr/bin/make -C abaqus
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
abaqusAIM.c -o ./abaqusAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
abaqusUtils.c -o ./abaqusUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
-I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -lm -ldl -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin
/Library/Developer/CommandLineTools/usr/bin/make -C aflr2
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr3
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr4
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C astros
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosAIM.c \
-o ./astrosAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosUtils.c \
-o ./astrosUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils astrosCards.c \
-o ./astrosCards.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C avl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C awave
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils awaveAIM.c \
-o ./awaveAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cart3d
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \
cart3dAIM.c -o ./cart3dAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/c3dio \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \
writeTrix.c -o ./writeTrix.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/c3dio \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/libCart3D \
surfTrix.c -o ./surfTrix.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -pedantic -I./xddm -I. \
`xml2-config --cflags` ./xddm/xddm.c \
-o ./xddm.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bodyTess.c -o ./bodyTess.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \
./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/ \
-lc3dio -lCart3D -ldl -lxml2 -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include cart3dTest.c \
-o ./cart3dTest.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I./xddm \
-I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \
./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -locsm -legads \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include/ -lc3dio -lCart3D \
-lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lxml2 -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cbaero
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I. -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
clang -g -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C cgt
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include egads2cgt.c \
-o ./egads2cgt.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include aflr4egads.c \
-o ./aflr4egads.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C custom
make[2]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C delaundo
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils delaundoAIM.c \
-o ./delaundoAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C egadsTess
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils egadsTessAIM.c \
-o ./egadsTessAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C friction
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils frictionAIM.c \
-o ./frictionAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/friction ./friction.o -Wl,-w -static-libgfortran -static-libgcc
/Library/Developer/CommandLineTools/usr/bin/make -C fun3d
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
-I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o ./fun3dUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
-I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -lm -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin
/Library/Developer/CommandLineTools/usr/bin/make -C hsm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmAIM.c \
-o src/hsmAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmUtils.c \
-o src/hsmUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hsmAdj.c \
-o src/hsmAdj.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.7 \
-o src/rcm.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 rcm/genrcmi.cpp -DREVISION=7.7 \
-o src/genrcmi.o
/Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o
/Library/Developer/CommandLineTools/usr/bin/make -C src cross.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o
/Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o
/Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o
/Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/hsmAIM.so \
src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
src/rcm.o src/genrcmi.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lc++ -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C interference
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include interferenceAIM.c \
-o ./interferenceAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. cloudFns.c \
-o ./cloudFns.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/interferenceAIM.so \
./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C masstran
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils masstranAIM.cpp \
-o ./masstranAIM.o
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C meshWriter
/Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bstlWriter.c \
-o ./bstlWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include bvtkWriter.c \
-o ./bvtkWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter
make[3]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C fastWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include fastWriter.c \
-o ./fastWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libmeshbWriter.c \
-o ./libmeshbWriter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C stlWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include stlWriter.c \
-o ./stlWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2Writer
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include su2Writer.c \
-o ./su2Writer.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include tecplotWriter.c \
-o ./tecplotWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include ugridWriter.c \
-o ./ugridWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include vtkWriter.c \
-o ./vtkWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mses
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mystran
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils mystranAIM.c \
-o ./mystranAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils mystranUtils.c \
-o ./mystranUtils.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C nastran
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils nastranAIM.c \
-o ./nastranAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C plato
Not compiling platoAIM: SEACAS must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C pointwise
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils pointwiseAIM.c \
-o ./pointwiseAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils hashElement.c \
-o ./hashElement.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm -lpthread
/Library/Developer/CommandLineTools/usr/bin/make -C refine
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o ./refineAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSD
Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSM
Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C skeleton
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils skeletonAIM.c \
-o ./skeletonAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker
make[2]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C su2
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o ./su2AIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2Utils.c \
-o ./su2Utils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
-o ./su2_4_Cardinal.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_5_Raven.c \
-o ./su2_5_Raven.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_6_Falcon.c \
-o ./su2_6_Falcon.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
-o ./su2_7_Blackbird.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils su2_801_Harrier.c \
-o ./su2_801_Harrier.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tacs
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils tacsAIM.c \
-o ./tacsAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C tetgen
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils tetgenAIM.cpp \
-o ./tetgenAIM.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
./tetgen_Interface.o ./tetgen.o \
./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tsfoil
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
tsfoilAIM.c -o ./tsfoilAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C unitTest
make[2]: Nothing to be done for `all'.
/Library/Developer/CommandLineTools/usr/bin/make -C xfoil
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils \
xfoilAIM.c -o ./xfoilAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C zaero
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
(cd OpenCSM; make -f serveESP.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.7 -I/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/include -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pyscript.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -L/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin
*** Build Completed! ***
+ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin
++ uname -a
+ [[ Darwin macys-VM 20.6.0 Darwin Kernel Version 20.6.0: Thu Sep 29 20:15:11 PDT 2022; root:xnu-7195.141.42~1/RELEASE_X86_64 x86_64 == *\D\a\r\w\i\n* ]]
+ sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==> serveESP completed successfully with no verification data
real 0m0.617s
user 0m0.038s
sys 0m0.015s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.333s
user 0m0.394s
sys 0m0.031s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m3.842s
user 0m4.638s
sys 0m0.356s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.917s
user 0m0.956s
sys 0m0.050s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.700s
user 0m0.863s
sys 0m0.081s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.773s
user 0m1.017s
sys 0m0.043s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m5.132s
user 0m6.907s
sys 0m0.368s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/CAPS/verify_7.7.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m44.798s
user 0m58.120s
sys 0m2.131s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.742s
user 0m0.920s
sys 0m0.038s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 1m2.095s
user 1m37.079s
sys 0m7.284s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
==> serveESP completed successfully with 1 warnings and no verification data
real 0m0.404s
user 0m0.296s
sys 0m0.036s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.546s
user 0m0.785s
sys 0m0.024s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.187s
user 0m0.240s
sys 0m0.023s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/basic/verify_7.7.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data
real 0m0.482s
user 0m0.508s
sys 0m0.030s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.5
python -u -m unittest discover
.................................................... PCurve Map: 48 (alloc 48)!
Surface Map: 12 (alloc 24)!
Curve Map: 28 (alloc 28)!
Writing PCurves...
Writing Curves...
Writing Surfaces...
Writing 16 Nodes...
Writing 28 Edges...
Writing 12 Loops...
Writing 12 Faces...
Writing 1 Shells...
EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 3.714s
OK
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m9.550s
user 0m11.638s
sys 0m0.473s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.5
python -u -m unittest discover
..Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 143
Number of elements = 282
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 282
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 155
Number of elements = 306
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 306
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 298
Combined Number of elements = 588
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 588
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library - d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 209
Number of elements = 414
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 414
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 186
Number of elements = 368
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 368
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 395
Combined Number of elements = 782
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 782
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
----------------------------------------------------------------------
Ran 100 tests in 179.573s
OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.5
python -u -m unittest discover --verbose
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.030 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 = 0.123 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.021 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 = 0.026 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 = 0.079 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.037 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 = 0.129 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 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2224 2224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 446 894
AFLR2 IG : Nodes, Faces = 892 1786
AFLR2 IG : Nodes, Faces = 918 1838
AFLR2 IG : Nodes, Faces = 1033 2068
AFLR2 IG : Nodes, Faces = 1133 2268
AFLR2 IG : Nodes, Faces = 1233 2468
AFLR2 IG : Nodes, Faces = 1333 2668
AFLR2 IG : Nodes, Faces = 1338 2678
AFLR2 IG : Nodes, Faces = 1433 2868
AFLR2 IG : Nodes, Faces = 1533 3068
AFLR2 IG : Nodes, Faces = 1633 3268
AFLR2 IG : Nodes, Faces = 1733 3468
AFLR2 IG : Nodes, Faces = 1784 3570
AFLR2 IG : Nodes, Faces = 1833 3668
AFLR2 IG : Nodes, Faces = 1858 3718
AFLR2 IG : Nodes, Faces = 2224 4450
AFLR2 IG : Nodes, Faces = 2228 4450
AFLR2 IG : Nodes, Faces = 2224 2224
AFLR2 : CPU Time = 0.031 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 = 0.080 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.008 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.027 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 = 0.076 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 48 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 10 22
AFLR2 IG : Nodes, Faces = 20 42
AFLR2 IG : Nodes, Faces = 30 62
AFLR2 IG : Nodes, Faces = 40 82
AFLR2 IG : Nodes, Faces = 45 92
AFLR2 IG : Nodes, Faces = 46 94
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 98
AFLR2 IG : Nodes, Faces = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 48 48
AFLR2 GG : Nodes, Faces = 88 128
AFLR2 GG : Nodes, Faces = 109 170
AFLR2 GG : Nodes, Faces = 124 200
AFLR2 GG : Nodes, Faces = 136 224
AFLR2 GG : Nodes, Faces = 148 248
AFLR2 GG : Nodes, Faces = 161 274
AFLR2 GG : Nodes, Faces = 171 294
AFLR2 GG : Nodes, Faces = 181 314
AFLR2 GG : Nodes, Faces = 187 326
AFLR2 GG : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.001 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 = 0.002 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 = 0.015 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.002 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.003 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 = 0.023 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 = 0.011 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.003 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 = 0.032 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 = 0.010 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1189
Number of elements = 6249
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6237
Number of elements = 34620
Number of triangles = 4438
Number of quadrilatarals = 0
Number of tetrahedrals = 30182
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13613
Number of elements = 76414
Number of triangles = 8142
Number of quadrilatarals = 0
Number of tetrahedrals = 68272
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 41618
Number of elements = 236483
Number of triangles = 19838
Number of quadrilatarals = 0
Number of tetrahedrals = 216645
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4369
Number of elements = 24223
Number of triangles = 3016
Number of quadrilatarals = 0
Number of tetrahedrals = 21207
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 11007
Number of elements = 60837
Number of triangles = 8632
Number of quadrilatarals = 0
Number of tetrahedrals = 52205
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10474
Number of elements = 58678
Number of triangles = 6352
Number of quadrilatarals = 0
Number of tetrahedrals = 52326
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 88507
Number of elements = 497504
Number of triangles = 51750
Number of quadrilatarals = 0
Number of tetrahedrals = 445754
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16456
Number of elements = 93635
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 85709
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2589
Number of elements = 13809
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11051
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3654
Number of elements = 19800
Number of triangles = 3394
Number of quadrilatarals = 0
Number of tetrahedrals = 16406
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5456
Number of elements = 30308
Number of triangles = 3656
Number of quadrilatarals = 0
Number of tetrahedrals = 26652
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4694
Number of elements = 25935
Number of triangles = 3326
Number of quadrilatarals = 0
Number of tetrahedrals = 22609
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5554
Number of elements = 30862
Number of triangles = 3756
Number of quadrilatarals = 0
Number of tetrahedrals = 27106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2260
Number of elements = 12133
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2392
Number of elements = 12577
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3341
Number of elements = 18069
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3606
Number of elements = 18961
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4414
Number of elements = 23974
Number of triangles = 3998
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4811
Number of elements = 25310
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5490
Number of elements = 29891
Number of triangles = 4886
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6019
Number of elements = 31671
Number of triangles = 6666
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6542
Number of elements = 35667
Number of triangles = 5774
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7203
Number of elements = 37891
Number of triangles = 7998
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7601
Number of elements = 41489
Number of triangles = 6662
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8394
Number of elements = 44157
Number of triangles = 9330
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19800
Number of elements = 109798
Number of triangles = 15540
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22741
Number of elements = 119570
Number of triangles = 25312
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1193
Number of elements = 6272
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4940
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1176
Number of elements = 6165
Number of triangles = 1330
Number of quadrilatarals = 0
Number of tetrahedrals = 4835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1203
Number of elements = 6314
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4982
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1198
Number of elements = 6296
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4964
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1223
Number of elements = 6443
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5111
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1184
Number of elements = 6224
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4892
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1195
Number of elements = 6287
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4955
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1197
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1203
Number of elements = 6310
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4978
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1191
Number of elements = 6253
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4921
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8857
Number of elements = 49191
Number of triangles = 6284
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8989
Number of elements = 49635
Number of triangles = 6728
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7796
Number of elements = 43368
Number of triangles = 5396
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6267
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4935
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9944
Number of elements = 55193
Number of triangles = 7174
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10218
Number of elements = 56081
Number of triangles = 8062
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7818
Number of elements = 43469
Number of triangles = 5398
Number of quadrilatarals = 0
Number of tetrahedrals = 38071
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1202
Number of elements = 6320
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4988
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1198
Number of elements = 6292
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4960
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9609
Number of elements = 53228
Number of triangles = 6994
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9829
Number of elements = 53956
Number of triangles = 7722
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7789
Number of elements = 43295
Number of triangles = 5394
Number of quadrilatarals = 0
Number of tetrahedrals = 37901
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1186
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 854
Number of elements = 4431
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3435
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9348
Number of elements = 51734
Number of triangles = 6812
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9531
Number of elements = 52330
Number of triangles = 7408
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7804
Number of elements = 43358
Number of triangles = 5386
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1200
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9183
Number of elements = 50871
Number of triangles = 6632
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9322
Number of elements = 51307
Number of triangles = 7068
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7927
Number of elements = 44116
Number of triangles = 5382
Number of quadrilatarals = 0
Number of tetrahedrals = 38734
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 868
Number of elements = 4530
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3534
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10181
Number of elements = 56797
Number of triangles = 6782
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10671
Number of elements = 58561
Number of triangles = 8546
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7741
Number of elements = 43010
Number of triangles = 5362
Number of quadrilatarals = 0
Number of tetrahedrals = 37648
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2692
Number of elements = 14435
Number of triangles = 2800
Number of quadrilatarals = 0
Number of tetrahedrals = 11635
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 238
Number of elements = 1116
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 732
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1500
Number of elements = 7757
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1564
Number of elements = 7881
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1160
Number of elements = 6087
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4779
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1635
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 159
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 75
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5075
Number of elements = 27761
Number of triangles = 4072
Number of quadrilatarals = 0
Number of tetrahedrals = 23689
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5221
Number of elements = 28313
Number of triangles = 4624
Number of quadrilatarals = 0
Number of tetrahedrals = 23689
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4882
Number of elements = 26790
Number of triangles = 4040
Number of quadrilatarals = 0
Number of tetrahedrals = 22750
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 339
Number of elements = 1523
Number of triangles = 584
Number of quadrilatarals = 0
Number of tetrahedrals = 939
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 32776
Number of elements = 189806
Number of triangles = 8496
Number of quadrilatarals = 0
Number of tetrahedrals = 181310
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36115
Number of elements = 203130
Number of triangles = 21820
Number of quadrilatarals = 0
Number of tetrahedrals = 181310
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28584
Number of elements = 162362
Number of triangles = 15158
Number of quadrilatarals = 0
Number of tetrahedrals = 147204
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1425
Number of elements = 7592
Number of triangles = 1456
Number of quadrilatarals = 0
Number of tetrahedrals = 6136
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4138
Number of elements = 22901
Number of triangles = 2938
Number of quadrilatarals = 0
Number of tetrahedrals = 19963
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 711
Number of elements = 3685
Number of triangles = 844
Number of quadrilatarals = 0
Number of tetrahedrals = 2841
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1257
Number of elements = 6590
Number of triangles = 1424
Number of quadrilatarals = 0
Number of tetrahedrals = 5166
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16639
Number of elements = 94369
Number of triangles = 8800
Number of quadrilatarals = 0
Number of tetrahedrals = 85569
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18563
Number of elements = 101745
Number of triangles = 16176
Number of quadrilatarals = 0
Number of tetrahedrals = 85569
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12009
Number of elements = 67436
Number of triangles = 7140
Number of quadrilatarals = 0
Number of tetrahedrals = 60296
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6554
Number of elements = 34309
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25273
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4989
Number of elements = 27641
Number of triangles = 3462
Number of quadrilatarals = 0
Number of tetrahedrals = 24179
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6401
Number of elements = 35742
Number of triangles = 4048
Number of quadrilatarals = 0
Number of tetrahedrals = 31694
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59702
Number of elements = 348382
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 335454
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 58332
Number of elements = 339688
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 327260
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59702
Number of elements = 347882
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 335454
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 44
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 3
Surface 2: Number of points found for aero-spline = 6
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
8 automatic connections were made for capsConnect Rib_Root (node id 1)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice control surface data
VLM control surface name - Elevator
VLM control surface name - LeftAileron
VLM control surface name - RightAileron
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output (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:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 9
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = nodeBody, index = 8
Name = farfield, index = 9
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
70000D7B6000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000D7B6000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
10E0F0E00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
10E0F0E00 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
10E0F0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
10E0F0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000D7B6000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000D7B6000 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
10E0F0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
10E0F0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000D7B6000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000D7B6000 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
10E0F0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
10E0F0E00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000D7B6000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000D7B6000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
ok
test_nodeBody (test_egadsTess.TestEGADS.test_nodeBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = nodeBody, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_phase (test_egadsTess.TestEGADS.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ok
test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_setInput (test_egadsTess.TestEGADS.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_egadsTess.TestEGADS.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_egadsTess.TestEGADS.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Design_SensFile (test_fun3d.TestFUN3D.test_Design_SensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7820
Number of elements = 15636
Number of triangle elements = 15636
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5889
Number of elements = 11774
Number of triangle elements = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 524
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14233
Total number of elements = 28454
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14233, elements - 28454
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.251562
Creating surface mesh ...
Surface mesh seconds: 0.061263
Recovering boundaries...
Boundary recovery seconds: 0.159357
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.077721
Recovering Delaunayness...
Delaunay recovery seconds: 0.077709
Refining mesh...
18972 insertions, added 13254 points, 701278 tetrahedra in queue.
6317 insertions, added 2883 points, 614952 tetrahedra in queue.
8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds: 3.23264
Smoothing vertices...
Mesh smoothing seconds: 2.73371
Improving mesh...
Mesh improvement seconds: 0.051196
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.017113
Total running seconds: 6.66363
Statistics:
Input points: 14233
Input facets: 28454
Input segments: 42681
Input holes: 2
Input regions: 0
Mesh points: 33078
Mesh tetrahedra: 159812
Mesh faces: 333851
Mesh faces on exterior boundary: 28454
Mesh faces on input facets: 28454
Mesh edges on input segments: 42681
Steiner points inside domain: 18845
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 5
Design Variable name - Mach
Warning: No initial value set for Mach
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 6
Design Variable name - Alpha
Design Variable name - Beta
Warning: No initial value set for Beta
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Overwrite_NML is set to 'True' - a new namelist will be created
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Alpha
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Creating FUN3D directory tree
DesignVariable = Alpha
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Overwrite_NML is set to 'True' - a new namelist will be created
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data
ok
test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 6
Design Variable name - Alpha
Design Variable name - Beta
Warning: No initial value set for Beta
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
ok
test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7820
Number of elements = 15636
Number of triangle elements = 15636
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5889
Number of elements = 11774
Number of triangle elements = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 524
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14233
Total number of elements = 28454
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14233, elements - 28454
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.187559
Creating surface mesh ...
Surface mesh seconds: 0.039899
Recovering boundaries...
Boundary recovery seconds: 0.122933
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.060262
Recovering Delaunayness...
Delaunay recovery seconds: 0.060011
Refining mesh...
18972 insertions, added 13254 points, 701278 tetrahedra in queue.
6317 insertions, added 2883 points, 614952 tetrahedra in queue.
8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds: 2.34378
Smoothing vertices...
Mesh smoothing seconds: 2.26495
Improving mesh...
Mesh improvement seconds: 0.047139
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.018083
Total running seconds: 5.14546
Statistics:
Input points: 14233
Input facets: 28454
Input segments: 42681
Input holes: 2
Input regions: 0
Mesh points: 33078
Mesh tetrahedra: 159812
Mesh faces: 333851
Mesh faces on exterior boundary: 28454
Mesh faces on input facets: 28454
Mesh edges on input segments: 42681
Steiner points inside domain: 18845
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5079, elements - 10146
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5079, elements - 10146
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14233, elements - 28454
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ...
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - alowervar
Design Variable name - auppervar
Design Variable name - classvar
Design Variable name - ztailvar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - avar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 54 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 54 54
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 12 26
AFLR2 IG : Nodes, Faces = 24 50
AFLR2 IG : Nodes, Faces = 36 74
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 106
AFLR2 IG : Nodes, Faces = 53 108
AFLR2 IG : Nodes, Faces = 54 110
AFLR2 IG : Nodes, Faces = 58 110
AFLR2 IG : Nodes, Faces = 54 54
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 54 54
AFLR2 GG : Nodes, Faces = 100 146
AFLR2 GG : Nodes, Faces = 122 190
AFLR2 GG : Nodes, Faces = 138 222
AFLR2 GG : Nodes, Faces = 153 252
AFLR2 GG : Nodes, Faces = 168 282
AFLR2 GG : Nodes, Faces = 180 306
AFLR2 GG : Nodes, Faces = 192 330
AFLR2 GG : Nodes, Faces = 201 348
AFLR2 GG : Nodes, Faces = 210 366
AFLR2 GG : Nodes, Faces = 216 378
AFLR2 GG : Nodes, Faces = 221 388
AFLR2 GG : Nodes, Faces = 224 394
AFLR2 GG : Nodes, Faces = 225 396
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 225 396
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 225
Number of elements = 450
Number of tris = 396
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1602
Number of elements = 8758
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7518
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2600
Number of elements = 13864
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1071
Number of elements = 5705
Number of triangles = 998
Number of quadrilatarals = 0
Number of tetrahedrals = 4707
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 15544
Number of elements = 89331
Number of triangles = 4632
Number of quadrilatarals = 0
Number of tetrahedrals = 84699
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1602
Number of elements = 8758
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7518
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_refine.TestREFINE.test_inputs) ... ok
test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 438
Number of elements = 2179
Number of triangles = 644
Number of quadrilatarals = 0
Number of tetrahedrals = 1535
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 936
Number of elements = 4999
Number of triangles = 758
Number of quadrilatarals = 0
Number of tetrahedrals = 4241
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 3 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 8 Faces
EGADS : Body 0 has 15 Edges
EGADS : Body 0 has 8 Loops
EGADS : Body 0 has 9 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 8 Faces
EGADS : Body 1 has 15 Edges
EGADS : Body 1 has 8 Loops
EGADS : Body 1 has 9 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 2 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 2 Loops
EGADS : Body 2 has 2 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4 5
EGADS : 2 Yes 0 0 1 1 1 1 3 4 6
EGADS : 3 Yes 0 0 1 1 1 1 2 4 7
EGADS : 4 Yes 0 0 1 1 1 1 2 3
EGADS : 5 Yes 0 0 1 1 1 1 6 7 8
EGADS : 6 Yes 0 0 1 1 1 2 5 7 8
EGADS : 7 Yes 0 0 1 1 1 3 5 6 8
EGADS : 8 Yes 0 0 1 1 1 5 6 7
EGADS : 9 Yes 1 0 1 0 10 10 11 12 13
EGADS : 10 Yes 1 0 1 0 10 9 11 12 14
EGADS : 11 Yes 1 0 1 0 10 9 10 12 15
EGADS : 12 Yes 1 0 1 0 10 9 10 11
EGADS : 13 Yes 1 0 1 0 10 9 14 15 16
EGADS : 14 Yes 1 0 1 0 10 10 13 15 16
EGADS : 15 Yes 1 0 1 0 10 11 13 14 16
EGADS : 16 Yes 1 0 1 0 10 13 14 15
EGADS : 17 Yes 2 0 1 NA NA 18
EGADS : 18 Yes 2 0 1 NA NA 17
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 4 -3 -2
EGADS : 2 3 7 -6 -5
EGADS : 3 6 9 -1 -8
EGADS : 4 -4 -9 -7
EGADS : 5 -10 2 11 -12
EGADS : 6 -11 5 13 -14
EGADS : 7 -13 8 10 -15
EGADS : 8 12 14 15
EGADS : 9 16 19 -18 -17
EGADS : 10 18 22 -21 -20
EGADS : 11 21 24 -16 -23
EGADS : 12 -19 -24 -22
EGADS : 13 -25 17 26 -27
EGADS : 14 -26 20 28 -29
EGADS : 15 -28 23 25 -30
EGADS : 16 27 29 30
EGADS : 17 -31 -32 33 34
EGADS : 18 -35 -34 36 32
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 4 -3 -2
EGADS : 2 Yes 3 7 -6 -5
EGADS : 3 Yes 6 9 -1 -8
EGADS : 4 Yes -4 -9 -7
EGADS : 5 Yes -10 2 11 -12
EGADS : 6 Yes -11 5 13 -14
EGADS : 7 Yes -13 8 10 -15
EGADS : 8 Yes 12 14 15
EGADS : 9 Yes 16 19 -18 -17
EGADS : 10 Yes 18 22 -21 -20
EGADS : 11 Yes 21 24 -16 -23
EGADS : 12 Yes -19 -24 -22
EGADS : 13 Yes -25 17 26 -27
EGADS : 14 Yes -26 20 28 -29
EGADS : 15 Yes -28 23 25 -30
EGADS : 16 Yes 27 29 30
EGADS : 17 Yes -31 -32 33 34
EGADS : 18 Yes -35 -34 36 32
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 5
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 5 1 2 6
EGADS : 6 0 Yes 5 6 1 2 3
EGADS : 7 0 Yes 4 6 1 2 4
EGADS : 8 0 Yes 5 1 1 3 7
EGADS : 9 0 Yes 6 2 1 3 4
EGADS : 10 0 Yes 1 7 1 5 7
EGADS : 11 0 Yes 3 8 1 5 6
EGADS : 12 0 Yes 7 8 1 5 8
EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 DEGEN 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 DEGEN 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 DEGEN 19 19 - 18
EGADS : 36 2 DEGEN 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 3.77246052 0 0.00459131419
EGADS : 2 Yes 5.90487498 7.07106781 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.0824829 7.07106781 0.123425948
EGADS : 5 Yes 3.77001182 0 0
EGADS : 6 Yes 5.90282524 7.07106781 0
EGADS : 7 Yes 5.90487498 0 0
EGADS : 8 Yes 4.0824829 0 0.123425948
EGADS : 9 Yes 5.90282524 0 0
EGADS : 10 Yes 11.5089842 0 0.00183652568
EGADS : 11 Yes 12.36195 2.82842712 0
EGADS : 12 Yes 10 0 0
EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791
EGADS : 14 Yes 11.5080047 0 0
EGADS : 15 Yes 12.3611301 2.82842712 0
EGADS : 16 Yes 12.36195 0 0
EGADS : 17 Yes 11.6329932 0 0.0493703791
EGADS : 18 Yes 12.3611301 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 15.6122
AFLR4 : Abs Min Surf Spacing = 0.00222722
AFLR4 : Min Surf Spacing = 0.00445444
AFLR4 : Max Surf Spacing = 0.0890888
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 FARFIELD
AFLR4 : 18 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 12428
AFLR43 : Nodes = 6220
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6220 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 Solid
UG3 : 12 Solid
UG3 : 13 Solid
UG3 : 14 Solid
UG3 : 15 Solid
UG3 : 16 Solid
UG3 : 17 FarField
UG3 : 18 FarField
AFLR3 : CPU Time = 0.012 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6220 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1246 7333
AFLR3 IG : Nodes, Elements = 2492 16261
AFLR3 IG : Nodes, Elements = 3738 25021
AFLR3 IG : Nodes, Elements = 4984 34304
AFLR3 IG : Nodes, Elements = 6227 43518
AFLR3 IG : Nodes, Elements = 6227 43440
AFLR3 IG : Nodes, Elements = 6227 43474
AFLR3 IG : Nodes, Elements = 6227 43437
AFLR3 IG : Nodes, Elements = 6220 26107
AFLR3 IG : Nodes, Elements = 6220 26133
AFLR3 IG : Nodes, Elements = 6220 21538
AFLR3 IG : Nodes, Elements = 6220 19141
AFLR3 : CPU Time = 0.152 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6220 19141
AFLR3 GG : Nodes, Elements = 9092 27970
AFLR3 GG : Nodes, Elements = 9092 39349
AFLR3 GG : Nodes, Elements = 9092 36380
AFLR3 GG : Nodes, Elements = 9092 34923
AFLR3 GG : Nodes, Elements = 11659 42981
AFLR3 GG : Nodes, Elements = 11659 53807
AFLR3 GG : Nodes, Elements = 11659 50702
AFLR3 GG : Nodes, Elements = 11659 49815
AFLR3 GG : Nodes, Elements = 14477 58553
AFLR3 GG : Nodes, Elements = 14477 70855
AFLR3 GG : Nodes, Elements = 14477 67465
AFLR3 GG : Nodes, Elements = 14477 66533
AFLR3 GG : Nodes, Elements = 17443 75634
AFLR3 GG : Nodes, Elements = 17443 88707
AFLR3 GG : Nodes, Elements = 17443 85026
AFLR3 GG : Nodes, Elements = 17443 84166
AFLR3 GG : Nodes, Elements = 20625 93912
AFLR3 GG : Nodes, Elements = 20625 107483
AFLR3 GG : Nodes, Elements = 20625 103837
AFLR3 GG : Nodes, Elements = 20625 103014
AFLR3 GG : Nodes, Elements = 23983 113245
AFLR3 GG : Nodes, Elements = 23983 127691
AFLR3 GG : Nodes, Elements = 23983 123762
AFLR3 GG : Nodes, Elements = 23983 122939
AFLR3 GG : Nodes, Elements = 27471 133562
AFLR3 GG : Nodes, Elements = 27471 148246
AFLR3 GG : Nodes, Elements = 27471 144367
AFLR3 GG : Nodes, Elements = 27471 143483
AFLR3 GG : Nodes, Elements = 31049 154330
AFLR3 GG : Nodes, Elements = 31049 169629
AFLR3 GG : Nodes, Elements = 31049 165573
AFLR3 GG : Nodes, Elements = 31049 164719
AFLR3 GG : Nodes, Elements = 34642 175591
AFLR3 GG : Nodes, Elements = 34642 190772
AFLR3 GG : Nodes, Elements = 34642 186857
AFLR3 GG : Nodes, Elements = 34642 186049
AFLR3 GG : Nodes, Elements = 38204 196811
AFLR3 GG : Nodes, Elements = 38204 211769
AFLR3 GG : Nodes, Elements = 38204 208011
AFLR3 GG : Nodes, Elements = 38204 207203
AFLR3 GG : Nodes, Elements = 41735 217867
AFLR3 GG : Nodes, Elements = 41735 232734
AFLR3 GG : Nodes, Elements = 41735 228893
AFLR3 GG : Nodes, Elements = 41735 228199
AFLR3 GG : Nodes, Elements = 45118 238407
AFLR3 GG : Nodes, Elements = 45118 252771
AFLR3 GG : Nodes, Elements = 45118 249083
AFLR3 GG : Nodes, Elements = 45118 248399
AFLR3 GG : Nodes, Elements = 48432 258383
AFLR3 GG : Nodes, Elements = 48432 272398
AFLR3 GG : Nodes, Elements = 48432 268767
AFLR3 GG : Nodes, Elements = 48432 268040
AFLR3 GG : Nodes, Elements = 51632 277673
AFLR3 GG : Nodes, Elements = 51632 291124
AFLR3 GG : Nodes, Elements = 51632 287737
AFLR3 GG : Nodes, Elements = 51632 287138
AFLR3 GG : Nodes, Elements = 54742 296489
AFLR3 GG : Nodes, Elements = 54742 309545
AFLR3 GG : Nodes, Elements = 54742 306294
AFLR3 GG : Nodes, Elements = 54742 305700
AFLR3 GG : Nodes, Elements = 57753 314750
AFLR3 GG : Nodes, Elements = 57753 327393
AFLR3 GG : Nodes, Elements = 57753 324205
AFLR3 GG : Nodes, Elements = 57753 323671
AFLR3 GG : Nodes, Elements = 60589 332185
AFLR3 GG : Nodes, Elements = 60589 344195
AFLR3 GG : Nodes, Elements = 60589 341132
AFLR3 GG : Nodes, Elements = 60589 340678
AFLR3 GG : Nodes, Elements = 63303 348823
AFLR3 GG : Nodes, Elements = 63303 360078
AFLR3 GG : Nodes, Elements = 63303 357259
AFLR3 GG : Nodes, Elements = 63303 356861
AFLR3 GG : Nodes, Elements = 65821 364418
AFLR3 GG : Nodes, Elements = 65821 375019
AFLR3 GG : Nodes, Elements = 65821 372315
AFLR3 GG : Nodes, Elements = 65821 371973
AFLR3 GG : Nodes, Elements = 68056 378682
AFLR3 GG : Nodes, Elements = 68056 387933
AFLR3 GG : Nodes, Elements = 68056 385584
AFLR3 GG : Nodes, Elements = 68056 385301
AFLR3 GG : Nodes, Elements = 69951 390988
AFLR3 GG : Nodes, Elements = 69951 398948
AFLR3 GG : Nodes, Elements = 69951 396934
AFLR3 GG : Nodes, Elements = 69951 396704
AFLR3 GG : Nodes, Elements = 71446 401190
AFLR3 GG : Nodes, Elements = 71446 407532
AFLR3 GG : Nodes, Elements = 71446 405836
AFLR3 GG : Nodes, Elements = 71446 405665
AFLR3 GG : Nodes, Elements = 72588 409091
AFLR3 GG : Nodes, Elements = 72588 414051
AFLR3 GG : Nodes, Elements = 72588 412698
AFLR3 GG : Nodes, Elements = 72588 412555
AFLR3 GG : Nodes, Elements = 73412 415028
AFLR3 GG : Nodes, Elements = 73412 418465
AFLR3 GG : Nodes, Elements = 73412 417560
AFLR3 GG : Nodes, Elements = 73412 417491
AFLR3 GG : Nodes, Elements = 73970 419165
AFLR3 GG : Nodes, Elements = 73970 421515
AFLR3 GG : Nodes, Elements = 73970 420850
AFLR3 GG : Nodes, Elements = 73970 420801
AFLR3 GG : Nodes, Elements = 74329 421878
AFLR3 GG : Nodes, Elements = 74329 423409
AFLR3 GG : Nodes, Elements = 74329 422967
AFLR3 GG : Nodes, Elements = 74329 422934
AFLR3 GG : Nodes, Elements = 74527 423528
AFLR3 GG : Nodes, Elements = 74527 424406
AFLR3 GG : Nodes, Elements = 74527 424145
AFLR3 GG : Nodes, Elements = 74527 424123
AFLR3 GG : Nodes, Elements = 74619 424399
AFLR3 GG : Nodes, Elements = 74619 424805
AFLR3 GG : Nodes, Elements = 74619 424686
AFLR3 GG : Nodes, Elements = 74619 424681
AFLR3 GG : Nodes, Elements = 74657 424795
AFLR3 GG : Nodes, Elements = 74657 424951
AFLR3 GG : Nodes, Elements = 74657 424897
AFLR3 GG : Nodes, Elements = 74672 424942
AFLR3 GG : Nodes, Elements = 74672 425006
AFLR3 GG : Nodes, Elements = 74672 424985
AFLR3 GG : Nodes, Elements = 74672 424986
AFLR3 GG : Nodes, Elements = 74673 424989
AFLR3 GG : Nodes, Elements = 74673 424992
AFLR3 GG : Nodes, Elements = 74673 424991
AFLR3 GG : Nodes, Elements = 74696 425060
AFLR3 GG : Nodes, Elements = 74696 425133
AFLR3 GG : Nodes, Elements = 74696 425114
AFLR3 GG : Nodes, Elements = 74696 425117
AFLR3 GG : Nodes, Elements = 74700 425129
AFLR3 GG : Nodes, Elements = 74700 425145
AFLR3 GG : Nodes, Elements = 74700 425140
AFLR3 GG : Nodes, Elements = 74702 425146
AFLR3 GG : Nodes, Elements = 74702 425155
AFLR3 GG : Nodes, Elements = 74702 425152
AFLR3 GG : Nodes, Elements = 74702 425150
AFLR3 : CPU Time = 4.521 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 74702 425150
AFLR3 QI : Nodes, Elements = 73200 416638
AFLR3 QI : Nodes, Elements = 72976 415359
AFLR3 QI : Nodes, Elements = 72961 415273
AFLR3 QI : Nodes, Elements = 72960 415266
AFLR3 QI : Nodes, Elements = 72960 419161
AFLR3 QI : Nodes, Elements = 72960 415035
AFLR3 QI : Nodes, Elements = 72960 414621
AFLR3 QI : Nodes, Elements = 72960 415001
AFLR3 QI : Nodes, Elements = 72960 414373
AFLR3 QI : Nodes, Elements = 72960 414178
AFLR3 QI : Nodes, Elements = 72960 414472
AFLR3 QI : Nodes, Elements = 72960 414145
AFLR3 QI : Nodes, Elements = 72960 414045
AFLR3 QI : Nodes, Elements = 72960 414288
AFLR3 QI : Nodes, Elements = 72960 414039
AFLR3 QI : Nodes, Elements = 72960 413980
AFLR3 QI : Nodes, Elements = 72960 414224
AFLR3 QI : Nodes, Elements = 72960 413989
AFLR3 QI : Nodes, Elements = 72960 413938
AFLR3 QI : Nodes, Elements = 72966 413964
AFLR3 QI : Nodes, Elements = 72966 414196
AFLR3 QI : Nodes, Elements = 72966 413985
AFLR3 QI : Nodes, Elements = 72966 413966
AFLR3 QI : Nodes, Elements = 72966 414195
AFLR3 QI : Nodes, Elements = 72966 413976
AFLR3 QI : Nodes, Elements = 72966 413935
AFLR3 : CPU Time = 1.621 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 72966 413935
AFLR3 QRG: Nodes, Elements = 72978 413998
AFLR3 QRG: Nodes, Elements = 72988 414052
AFLR3 QRG: Nodes, Elements = 72990 414061
AFLR3 QRG: Nodes, Elements = 72991 414065
AFLR3 QRG: Nodes, Elements = 72990 414059
AFLR3 QRG: Nodes, Elements = 72998 414101
AFLR3 QRG: Nodes, Elements = 72998 414099
AFLR3 QRG: Nodes, Elements = 73000 414112
AFLR3 QRG: Nodes, Elements = 73007 414152
AFLR3 : CPU Time = 0.042 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Ang = 1.137 170.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 61
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 414152
UG3 : Min Vol = 6.36e-10
UG3 : Average Vol = 5.12
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Q = 0.0734 1
UG3 : Average Q = 0.894
UG3 : No. Q< 0.1 = 29
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 6.791 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Ang = 1.137 170.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 61
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 414152
UG3 : Min Vol = 6.36e-10
UG3 : Average Vol = 5.12
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Q = 0.223 1
UG3 : Average Q = 0.859
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting surface mesh for body 1 (of 7)
Getting surface mesh for body 2 (of 7)
Getting surface mesh for body 3 (of 7)
Getting surface mesh for body 4 (of 7)
Getting surface mesh for body 5 (of 7)
Getting surface mesh for body 6 (of 7)
70000D7B6000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000D7B6000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000D7B6000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000D7B6000 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 = 294
Number of elements = 584
Number of triangle elements = 584
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes = 2048
Number of elements = 4096
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes = 152
Number of elements = 300
Number of triangle elements = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes = 624
Number of elements = 1248
Number of triangle elements = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4192
Total number of elements = 8364
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 294, elements - 584
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 294, elements - 584
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4192, elements - 8364
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 374
Number of elements = 744
Number of triangle elements = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 472
Total number of elements = 936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 386
Number of elements = 768
Number of triangle elements = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 351
Number of elements = 698
Number of triangle elements = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 491
Total number of elements = 970
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 376
Number of elements = 748
Number of triangle elements = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 454
Total number of elements = 896
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 126
Number of elements = 252
Number of triangle elements = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 109
Number of elements = 214
Number of triangle elements = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 48
Number of elements = 96
Number of triangle elements = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 12
Number of elements = 20
Number of triangle elements = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 169
Total number of elements = 330
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 536
Number of elements = 1072
Number of triangle elements = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 544
Number of elements = 1084
Number of triangle elements = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes = 1351
Number of elements = 2682
Number of triangle elements = 2682
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 288
Number of elements = 572
Number of triangle elements = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 174
Number of elements = 344
Number of triangle elements = 344
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 26
Number of elements = 48
Number of triangle elements = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 482
Number of elements = 960
Number of triangle elements = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 174, elements - 344
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1351, elements - 2682
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 174, elements - 344
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 444
Number of elements = 884
Number of triangle elements = 884
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 522
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 966
Total number of elements = 1928
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 444, elements - 884
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 444, elements - 884
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 7173, elements - 14338
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9601
Number of elements = 19194
Number of triangle elements = 19194
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9601
Total number of elements = 19194
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9601, elements - 19194
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1220
Number of elements = 2680
Number of triangle elements = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1221
Total number of elements = 2680
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1220
Number of elements = 2680
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 2680
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 1221
Combined Number of elements = 2681
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 2680
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 1
Material name - madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - Rib_Root
Property name - Rib_Root_Point
Property name - Ribs
Property name - Skin
Property name - Spar1
Property name - Spar2
Done getting FEA properties
Updating mesh element types based on properties input
'Smart_Restart' is ON
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting vortex lattice control surface data
VLM control surface name - CntrlLE
VLM control surface name - CntrlTE
Done getting vortex lattice control surface data
Getting FEA vortex lattice mesh
Getting ZAERO UAIC Configurations.......
Number of UAIC Configurations - 2
UAIC Configuration: climb, id = 1
- Mach Number : 0.200000
- Reduced Freq: [0.020000, ... , 0.250000]
UAIC Configuration: cruise, id = 2
- Mach Number : 0.700000
- Reduced Freq: [0.040000, ... , 0.350000]
Getting ZAERO Analysis Subcases.......
Number of Analysis Subcases - 2
Analysis Subcase: FlutterCruise, id = 1
- Discipline : flutter
- UAIC : cruise
Analysis Subcase: Trim, id = 2
- Discipline : Trim
- UAIC : climb
Getting ZAERO Trim Variables.......
Number of Trim Variables - 2
Trim Variable: ANGLEA
- Label : ALPHA
- Value : free
Trim Variable: URDD3
- Label : NZ
- Value : 1.0
Updating StaticAeroelastic subcase: Trim
- vectorToCG -> [0.345898, 1.652951, -0.041403]
- weight -> 476456.149985
- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523]
ok
----------------------------------------------------------------------
Ran 143 tests in 1359.331s
OK (skipped=15)
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[1]: `avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[1]: `awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[1]: `frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[1]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[1]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[1]: `interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[1]: `msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[1]: `mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[1]: `pointwiseTest' is up to date.
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests
All tests pass!
=================================================
=================================================
(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Using python : /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/ESP_venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
CXtot 0.0006119078685748102
CYtot -6.295467348382128e-15
CZtot -0.3012861394885953
Cltot -4.784258926526785e-14
Cmtot -0.1945055953450382
Cntot -2.338191252215186e-15
Cl'tot -4.787610967125373e-14
Cn'tot -1.502866821492718e-15
CLtot 0.3012509314150635
CDtot 0.004646353488232475
CDvis 0.0
CLff 0.3009503023520388
CYff -7.723329422293541e-15
CDind 0.004646353488232475
CDff 0.004968969500907922
e 0.9669902146157789
StripForces
Wing cl = [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.3101221284189, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422921, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408]
Wing cd = [-0.004234137763162, -0.004494543653192, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946409, 0.000511459807839, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080993, -0.0007386538944077, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653162, -0.004234137764545]
real 0m2.734s
user 0m0.602s
sys 0m0.602s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = [1.05475230553347, 1.36488869373699, 1.5660721427216, 2.03059709348412, 1.97271083121139, 1.87307153172667, 1.7605047576018]
Cd = [0.0131991208677172, 0.0166540240605863, 0.0200551482562954, 0.0458671341943513, 0.07542560093961, 0.099446917447585, 0.127479430989108]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.496044115314418, 0.46137773204142, 0.442376568201556, 0.361251636297643, 0.276104140853528, 0.214381239319783, 0.132988264746104]
real 0m4.022s
user 0m3.620s
sys 0m0.278s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'mses_PyTest.py test;'
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837932402995744
Cd = 0.0077758580442312715
Cm = 0.005262576090327783
real 0m3.384s
user 0m3.005s
sys 0m0.294s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m1.290s
user 0m0.662s
sys 0m0.311s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go. Other input will terminate the job.
Cl = 0.933417
Cd = 0.000284
Cd Wave = 0.0
Cm = -0.203436
Cp _Critcal = -1.303869
real 0m1.083s
user 0m0.553s
sys 0m0.252s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m1.409s
user 0m0.871s
sys 0m0.434s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting mesh sizing parameters
Mesh sizing name - LeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 3793
Number of elements = 4001
Number of triangle elements = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 76
Number of elements = 55
Number of triangle elements = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes = 100
Number of elements = 73
Number of triangle elements = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes = 3970
Total number of elements = 4129
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m12.547s
user 0m18.031s
sys 0m1.911s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.006 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 = 0.003 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.031 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.014 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 0m1.497s
user 0m1.023s
sys 0m0.394s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 150173
Number of elements = 449915
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 214483
Number of pyramids = 425
Number of prisms = 220627
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m23.591s
user 0m18.097s
sys 0m1.303s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3139
Total number of elements = 6266
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.02925
Creating surface mesh ...
Surface mesh seconds: 0.008353
Recovering boundaries...
Boundary recovery seconds: 0.08838
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.012312
Suppressing Steiner points ...
Steiner suppression seconds: 5.9e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.011098
Refining mesh...
4188 insertions, added 2137 points, 127272 tetrahedra in queue.
1394 insertions, added 414 points, 131442 tetrahedra in queue.
1858 insertions, added 464 points, 129858 tetrahedra in queue.
2477 insertions, added 450 points, 111812 tetrahedra in queue.
3302 insertions, added 490 points, 67833 tetrahedra in queue.
4401 insertions, added 401 points, 112 tetrahedra in queue.
Refinement seconds: 0.965578
Smoothing vertices...
Mesh smoothing seconds: 0.574522
Improving mesh...
Mesh improvement seconds: 0.010849
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.00559
Total running seconds: 1.70646
Statistics:
Input points: 3139
Input facets: 6266
Input segments: 9399
Input holes: 2
Input regions: 0
Mesh points: 7895
Mesh tetrahedra: 38676
Mesh faces: 80485
Mesh faces on exterior boundary: 6266
Mesh faces on input facets: 6266
Mesh edges on input segments: 9399
Steiner points inside domain: 4756
Done meshing using TetGen!
Writing Tecplot file ....
Finished writing Tecplot file
real 0m12.739s
user 0m8.691s
sys 0m0.552s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.002 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 = 0.043 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 = 0.016 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| 9.4147e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 9.2230e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.0956e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 8.9772e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 8.9961e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.0681e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.0989e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 8.9175e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 8.7146e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 8.6313e-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 0m3.439s
user 0m2.168s
sys 0m0.654s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = boundary, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = force, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = bar1, index = 1
Name = bar2, index = 2
Name = bar3, index = 3
capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
Removed 0 (out of 4) unused nodes!
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4
Number of elements = 3
Elemental Nodes = 0
Elemental Rods = 3
Elemental Tria3 = 0
Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 3
Property name - bar1
Property name - bar2
Property name - bar3
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - BoundaryCondition
No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedForce
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - SingleLoadCase
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
real 0m1.251s
user 0m0.707s
sys 0m0.433s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 0m2.410s
user 0m1.092s
sys 0m0.633s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Area 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11]
CG [1.222256036874, 0.1634981473778, -4.234574416087e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.454849830627e-06
Iyz 1.707682983295e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06]
II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]]
real 0m11.570s
user 0m11.177s
sys 0m2.563s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m2.456s
user 0m1.108s
sys 0m0.266s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
-21.56250 dimensionless
Variables
---------
x : 1.62500 [-] The X variable
y : 1.37500 [-] The Y variable
Constants
---------
c : 3 [-] A constant
c2 : 2 [-] A constant
Sensitivities
-------------
c : + 0.46957 A constant
c2 : - 0.22338 A constant
Solve Report
------------
Solve Method : Quadratic Program
Classification : Convex
Solver : cvxopt
real 0m33.250s
user 0m2.734s
sys 0m0.468s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
awave
Cart3D
Mystran
=================================================
All tests pass!
=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64
+ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/test/plugs
+ cd /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/test/plugs
+ find /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
data/Plugs/plugs0a.csm
data/Plugs/plugs0b.csm
data/Plugs/plugs0c.csm
data/Plugs/plugs0d.csm
total 51856
-rw-r--r-- 1 jenkins staff 1.2M May 16 20:01 ASTRO.D01
-rw-r--r-- 1 jenkins staff 277K May 16 20:01 ASTRO.IDX
-rwxr-xr-x 1 jenkins staff 131K May 16 20:01 ESPxddm
-rwxr-xr-x 1 jenkins staff 229K May 16 20:01 Slugs
-rwxr-xr-x 1 jenkins staff 102K May 16 20:01 TestFit
-rwxr-xr-x 1 jenkins staff 1.8M May 16 20:01 avl
-rwxr-xr-x 1 jenkins staff 50K May 16 20:01 cart3dTest
-rwxr-xr-x 1 jenkins staff 50K May 16 19:58 egads2cart
-rwxr-xr-x 1 jenkins staff 86K May 16 20:01 egads2cgt
-rwxr-xr-x 1 jenkins staff 383K May 16 20:01 friction
-rwxr-xr-x 1 jenkins staff 8.9M May 16 20:01 mastros.exe
-rwxr-xr-x 1 jenkins staff 2.2M May 16 20:01 mses
-rwxr-xr-x 1 jenkins staff 2.5M May 16 20:01 mset
-rwxr-xr-x 1 jenkins staff 51K May 16 20:01 phaseUtil
-rw-r--r-- 1 jenkins staff 1.6K May 16 20:05 pod.egads
-rw-r--r-- 1 jenkins staff 0B May 16 20:05 port7681.jrnl
-rwxr-xr-x 1 jenkins staff 1.2M May 16 20:01 pplot
-rwxr-xr-x 1 jenkins staff 1.2M May 16 20:01 pxplot
-rwxr-xr-x 1 jenkins staff 84K May 16 20:00 sensCSM
-rwxr-xr-x 1 jenkins staff 224K May 16 19:59 serveCSM
-rwxr-xr-x 1 jenkins staff 192K May 16 19:59 serveESP
-rwxr-xr-x 1 jenkins staff 68K May 16 19:58 vCurvature
-rwxr-xr-x 1 jenkins staff 51K May 16 19:58 vGeom
-rwxr-xr-x 1 jenkins staff 52K May 16 19:58 vTess
-rwxr-xr-x 1 jenkins staff 2.3M May 16 19:58 vTesstatic
-rw-r--r-- 1 jenkins staff 195K May 16 20:05 wingMultiModel.bdf
-rwxr-xr-x 1 jenkins staff 1.8M May 16 20:01 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0a.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0
Starting pass 3 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m17.799s
user 0m12.829s
sys 0m0.958s
++ set +x
data/Plugs/plugs0a passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0b.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0
Starting pass 5 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m12.075s
user 0m12.300s
sys 0m0.142s
++ set +x
data/Plugs/plugs0b passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0c.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m34.386s
user 0m44.733s
sys 0m0.577s
++ set +x
data/Plugs/plugs0c passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/verify_7.7.0/plugs0d.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m30.149s
user 0m40.570s
sys 0m0.372s
++ set +x
data/Plugs/plugs0d passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [macys_VM] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [macys_VM] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.7/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.7,ESP_ARCH=DARWIN64,buildnode=macys_VM #716'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS