Started by upstream project "ESP_Beta" build number 720
originally caused by:
Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on macys_VM in workspace /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-30T12:18:09.796 -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 2501
Checking out a fresh workspace because /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-30T12:18:09.796 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 863
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [macys_VM] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[DARWIN64] $ /bin/bash -ex /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jenkins371694628923047271.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/ESP_Beta.sh
+ source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ macys_VM == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64
++ ESP_BLOC=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]]
+++ . /usr/local/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ macys_VM == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ macys_VM == \m\a\c\y\s* ]]
++ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/intercept-*'
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ ln -s /usr/local/bin/python3 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python
++ ln -s /usr/local/bin/python3-config /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python-config
++ ln -s /usr/local/bin/virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/virtualenv
+++ python-config --includes
++ export 'PYTHONINC=. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11'
++ PYTHONINC='. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11'
+++ python-config --help
++ [[ Usage: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB=-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation'
++ [[ macys_VM == \m\a\c\y\s ]]
++ [[ macys_VM == \v\i\g\g\e\n ]]
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.5
++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/data
+ virtualenv /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv
created virtual environment CPython3.11.5.final.0-64 in 1575ms
creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv)
added seed packages: pip==24.0, setuptools==69.5.1, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/activate
++ '[' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/activate = /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv
++ '[' darwin20 = cygwin ']'
++ '[' darwin20 = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z '' ']'
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl.metadata (61 kB)
Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl (20.6 MB)
Installing collected packages: numpy
Successfully installed numpy-1.26.4
+ pip_install openmdao
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.32.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Requirement already satisfied: numpy<2 in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4)
Collecting packaging (from openmdao)
Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB)
Collecting requests (from openmdao)
Using cached requests-2.32.3-py3-none-any.whl.metadata (4.6 kB)
Collecting scipy (from openmdao)
Using cached scipy-1.13.1-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached packaging-24.0-py3-none-any.whl (53 kB)
Using cached requests-2.32.3-py3-none-any.whl (64 kB)
Using cached scipy-1.13.1-cp311-cp311-macosx_10_9_x86_64.whl (39.3 MB)
Using cached certifi-2024.2.2-py3-none-any.whl (163 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl (121 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.1-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao
Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.32.0 packaging-24.0 requests-2.32.3 scipy-1.13.1 urllib3-2.2.1
+ [[ macys_VM == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl (13.8 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install matplotlib
+ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.9.0-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-4.52.4-cp311-cp311-macosx_10_9_universal2.whl.metadata (161 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-4.52.4-cp311-cp311-macosx_10_9_universal2.whl (2.8 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-4.52.4 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/7.8/DARWIN64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.1)
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
--2024-05-30 12:19:15-- 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: 272121672 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
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4950K .......... .......... .......... .......... .......... 1% 93.0M 11s
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5050K .......... .......... .......... .......... .......... 1% 55.1M 11s
5100K .......... .......... .......... .......... .......... 1% 80.7M 11s
5150K .......... .......... .......... .......... .......... 1% 98.8M 11s
5200K .......... .......... .......... .......... .......... 1% 75.0M 11s
5250K .......... .......... .......... .......... .......... 1% 58.7M 11s
5300K .......... .......... .......... .......... .......... 2% 1.62M 12s
5350K .......... .......... .......... .......... .......... 2% 94.4M 12s
5400K .......... .......... .......... .......... .......... 2% 69.6M 12s
5450K .......... .......... .......... .......... .......... 2% 75.4M 12s
5500K .......... .......... .......... .......... .......... 2% 58.5M 12s
5550K .......... .......... .......... .......... .......... 2% 80.4M 12s
5600K .......... .......... .......... .......... .......... 2% 67.5M 12s
5650K .......... .......... .......... .......... .......... 2% 121M 12s
5700K .......... .......... .......... .......... .......... 2% 83.9M 12s
5750K .......... .......... .......... .......... .......... 2% 62.3M 12s
5800K .......... .......... .......... .......... .......... 2% 95.9M 11s
5850K .......... .......... .......... .......... .......... 2% 77.4M 11s
5900K .......... .......... .......... .......... .......... 2% 106M 11s
5950K .......... .......... .......... .......... .......... 2% 71.7M 11s
6000K .......... .......... .......... .......... .......... 2% 105M 11s
6050K .......... .......... .......... .......... .......... 2% 119M 11s
6100K .......... .......... .......... .......... .......... 2% 57.4M 11s
6150K .......... .......... .......... .......... .......... 2% 97.7M 11s
6200K .......... .......... .......... .......... .......... 2% 65.6M 11s
6250K .......... .......... .......... .......... .......... 2% 87.3M 11s
6300K .......... .......... .......... .......... .......... 2% 83.6M 11s
6350K .......... .......... .......... .......... .......... 2% 43.2M 11s
6400K .......... .......... .......... .......... .......... 2% 79.4M 11s
6450K .......... .......... .......... .......... .......... 2% 64.4M 11s
6500K .......... .......... .......... .......... .......... 2% 82.6M 11s
6550K .......... .......... .......... .......... .......... 2% 68.2M 11s
6600K .......... .......... .......... .......... .......... 2% 61.4M 10s
6650K .......... .......... .......... .......... .......... 2% 99.9M 10s
6700K .......... .......... .......... .......... .......... 2% 60.1M 10s
6750K .......... .......... .......... .......... .......... 2% 75.9M 10s
6800K .......... .......... .......... .......... .......... 2% 77.5M 10s
6850K .......... .......... .......... .......... .......... 2% 2.02M 11s
6900K .......... .......... .......... .......... .......... 2% 78.9M 11s
6950K .......... .......... .......... .......... .......... 2% 78.9M 11s
7000K .......... .......... .......... .......... .......... 2% 69.8M 11s
7050K .......... .......... .......... .......... .......... 2% 85.4M 11s
7100K .......... .......... .......... .......... .......... 2% 91.4M 11s
7150K .......... .......... .......... .......... .......... 2% 107M 11s
7200K .......... .......... .......... .......... .......... 2% 75.2M 11s
7250K .......... .......... .......... .......... .......... 2% 81.9M 11s
7300K .......... .......... .......... .......... .......... 2% 72.3M 11s
7350K .......... .......... .......... .......... .......... 2% 70.4M 11s
7400K .......... .......... .......... .......... .......... 2% 105M 10s
7450K .......... .......... .......... .......... .......... 2% 54.9M 10s
7500K .......... .......... .......... .......... .......... 2% 89.1M 10s
7550K .......... .......... .......... .......... .......... 2% 105M 10s
7600K .......... .......... .......... .......... .......... 2% 87.7M 10s
7650K .......... .......... .......... .......... .......... 2% 79.7M 10s
7700K .......... .......... .......... .......... .......... 2% 78.9M 10s
7750K .......... .......... .......... .......... .......... 2% 75.8M 10s
7800K .......... .......... .......... .......... .......... 2% 2.17M 11s
7850K .......... .......... .......... .......... .......... 2% 36.4M 11s
7900K .......... .......... .......... .......... .......... 2% 121M 11s
7950K .......... .......... .......... .......... .......... 3% 80.4M 11s
8000K .......... .......... .......... .......... .......... 3% 108M 11s
8050K .......... .......... .......... .......... .......... 3% 80.8M 11s
8100K .......... .......... .......... .......... .......... 3% 98.0M 11s
8150K .......... .......... .......... .......... .......... 3% 1.94M 11s
8200K .......... .......... .......... .......... .......... 3% 52.2M 11s
8250K .......... .......... .......... .......... .......... 3% 55.9M 11s
8300K .......... .......... .......... .......... .......... 3% 93.2M 11s
8350K .......... .......... .......... .......... .......... 3% 109M 11s
8400K .......... .......... .......... .......... .......... 3% 99.2M 11s
8450K .......... .......... .......... .......... .......... 3% 50.8M 11s
8500K .......... .......... .......... .......... .......... 3% 98.4M 11s
8550K .......... .......... .......... .......... .......... 3% 91.8M 11s
8600K .......... .......... .......... .......... .......... 3% 72.6M 11s
8650K .......... .......... .......... .......... .......... 3% 107M 11s
8700K .......... .......... .......... .......... .......... 3% 101M 11s
8750K .......... .......... .......... .......... .......... 3% 75.9M 11s
8800K .......... .......... .......... .......... .......... 3% 75.4M 11s
8850K .......... .......... .......... .......... .......... 3% 106M 11s
8900K .......... .......... .......... .......... .......... 3% 107M 11s
8950K .......... .......... .......... .......... .......... 3% 72.8M 10s
9000K .......... .......... .......... .......... .......... 3% 99.6M 10s
9050K .......... .......... .......... .......... .......... 3% 115M 10s
9100K .......... .......... .......... .......... .......... 3% 62.5M 10s
9150K .......... .......... .......... .......... .......... 3% 126M 10s
9200K .......... .......... .......... .......... .......... 3% 9.43M 10s
9250K .......... .......... .......... .......... .......... 3% 129M 10s
9300K .......... .......... .......... .......... .......... 3% 135M 10s
9350K .......... .......... .......... .......... .......... 3% 103M 10s
9400K .......... .......... .......... .......... .......... 3% 72.6M 10s
9450K .......... .......... .......... .......... .......... 3% 87.7M 10s
9500K .......... .......... .......... .......... .......... 3% 60.1M 10s
9550K .......... .......... .......... .......... .......... 3% 88.6M 10s
9600K .......... .......... .......... .......... .......... 3% 84.9M 10s
9650K .......... .......... .......... .......... .......... 3% 95.7M 10s
9700K .......... .......... .......... .......... .......... 3% 53.1M 10s
9750K .......... .......... .......... .......... .......... 3% 88.3M 10s
9800K .......... .......... .......... .......... .......... 3% 1.29M 11s
9850K .......... .......... .......... .......... .......... 3% 3.10M 11s
9900K .......... .......... .......... .......... .......... 3% 46.0M 11s
9950K .......... .......... .......... .......... .......... 3% 90.8M 11s
10000K .......... .......... .......... .......... .......... 3% 95.0M 11s
10050K .......... .......... .......... .......... .......... 3% 95.9M 11s
10100K .......... .......... .......... .......... .......... 3% 95.6M 11s
10150K .......... .......... .......... .......... .......... 3% 124M 11s
10200K .......... .......... .......... .......... .......... 3% 7.82M 11s
10250K .......... .......... .......... .......... .......... 3% 56.7M 11s
10300K .......... .......... .......... .......... .......... 3% 97.3M 11s
10350K .......... .......... .......... .......... .......... 3% 62.8M 11s
10400K .......... .......... .......... .......... .......... 3% 82.9M 11s
10450K .......... .......... .......... .......... .......... 3% 73.6M 11s
10500K .......... .......... .......... .......... .......... 3% 102M 11s
10550K .......... .......... .......... .......... .......... 3% 119M 11s
10600K .......... .......... .......... .......... .......... 4% 55.9M 11s
10650K .......... .......... .......... .......... .......... 4% 78.3M 11s
10700K .......... .......... .......... .......... .......... 4% 78.4M 11s
10750K .......... .......... .......... .......... .......... 4% 123M 11s
10800K .......... .......... .......... .......... .......... 4% 99.0M 11s
10850K .......... .......... .......... .......... .......... 4% 93.7M 11s
10900K .......... .......... .......... .......... .......... 4% 81.9M 11s
10950K .......... .......... .......... .......... .......... 4% 82.2M 11s
11000K .......... .......... .......... .......... .......... 4% 101M 10s
11050K .......... .......... .......... .......... .......... 4% 121M 10s
11100K .......... .......... .......... .......... .......... 4% 83.3M 10s
11150K .......... .......... .......... .......... .......... 4% 114M 10s
11200K .......... .......... .......... .......... .......... 4% 55.4M 10s
11250K .......... .......... .......... .......... .......... 4% 3.38M 11s
11300K .......... .......... .......... .......... .......... 4% 55.9M 11s
11350K .......... .......... .......... .......... .......... 4% 47.2M 11s
11400K .......... .......... .......... .......... .......... 4% 110M 11s
11450K .......... .......... .......... .......... .......... 4% 89.6M 10s
11500K .......... .......... .......... .......... .......... 4% 90.6M 10s
11550K .......... .......... .......... .......... .......... 4% 98.2M 10s
11600K .......... .......... .......... .......... .......... 4% 86.0M 10s
11650K .......... .......... .......... .......... .......... 4% 5.11M 11s
11700K .......... .......... .......... .......... .......... 4% 39.8M 11s
11750K .......... .......... .......... .......... .......... 4% 71.2M 10s
11800K .......... .......... .......... .......... .......... 4% 75.6M 10s
11850K .......... .......... .......... .......... .......... 4% 3.31M 11s
11900K .......... .......... .......... .......... .......... 4% 5.36M 11s
11950K .......... .......... .......... .......... .......... 4% 4.33M 11s
12000K .......... .......... .......... .......... .......... 4% 49.3M 11s
12050K .......... .......... .......... .......... .......... 4% 80.8M 11s
12100K .......... .......... .......... .......... .......... 4% 72.8M 11s
12150K .......... .......... .......... .......... .......... 4% 72.0M 11s
12200K .......... .......... .......... .......... .......... 4% 52.3M 11s
12250K .......... .......... .......... .......... .......... 4% 5.82M 11s
12300K .......... .......... .......... .......... .......... 4% 44.5M 11s
12350K .......... .......... .......... .......... .......... 4% 35.5M 11s
12400K .......... .......... .......... .......... .......... 4% 52.2M 11s
12450K .......... .......... .......... .......... .......... 4% 40.3M 11s
12500K .......... .......... .......... .......... .......... 4% 26.1M 11s
12550K .......... .......... .......... .......... .......... 4% 66.9M 11s
12600K .......... .......... .......... .......... .......... 4% 36.4M 11s
12650K .......... .......... .......... .......... .......... 4% 51.2M 11s
12700K .......... .......... .......... .......... .......... 4% 44.3M 11s
12750K .......... .......... .......... .......... .......... 4% 18.2M 11s
12800K .......... .......... .......... .......... .......... 4% 97.1M 11s
12850K .......... .......... .......... .......... .......... 4% 94.4M 11s
12900K .......... .......... .......... .......... .......... 4% 121M 11s
12950K .......... .......... .......... .......... .......... 4% 13.1M 11s
13000K .......... .......... .......... .......... .......... 4% 2.60M 11s
13050K .......... .......... .......... .......... .......... 4% 52.3M 11s
13100K .......... .......... .......... .......... .......... 4% 42.0M 11s
13150K .......... .......... .......... .......... .......... 4% 40.1M 11s
13200K .......... .......... .......... .......... .......... 4% 31.8M 11s
13250K .......... .......... .......... .......... .......... 5% 41.0M 11s
13300K .......... .......... .......... .......... .......... 5% 6.90M 11s
13350K .......... .......... .......... .......... .......... 5% 3.04M 11s
13400K .......... .......... .......... .......... .......... 5% 49.8M 11s
13450K .......... .......... .......... .......... .......... 5% 39.1M 11s
13500K .......... .......... .......... .......... .......... 5% 41.3M 11s
13550K .......... .......... .......... .......... .......... 5% 39.6M 11s
13600K .......... .......... .......... .......... .......... 5% 33.1M 11s
13650K .......... .......... .......... .......... .......... 5% 22.2M 11s
13700K .......... .......... .......... .......... .......... 5% 3.35M 11s
13750K .......... .......... .......... .......... .......... 5% 74.9M 11s
13800K .......... .......... .......... .......... .......... 5% 68.9M 11s
13850K .......... .......... .......... .......... .......... 5% 78.5M 11s
13900K .......... .......... .......... .......... .......... 5% 116M 11s
13950K .......... .......... .......... .......... .......... 5% 58.1M 11s
14000K .......... .......... .......... .......... .......... 5% 123M 11s
14050K .......... .......... .......... .......... .......... 5% 3.92M 11s
14100K .......... .......... .......... .......... .......... 5% 80.7M 11s
14150K .......... .......... .......... .......... .......... 5% 70.8M 11s
14200K .......... .......... .......... .......... .......... 5% 84.9M 11s
14250K .......... .......... .......... .......... .......... 5% 74.3M 11s
14300K .......... .......... .......... .......... .......... 5% 88.6M 11s
14350K .......... .......... .......... .......... .......... 5% 44.5M 11s
14400K .......... .......... .......... .......... .......... 5% 3.34M 11s
14450K .......... .......... .......... .......... .......... 5% 90.9M 11s
14500K .......... .......... .......... .......... .......... 5% 89.4M 11s
14550K .......... .......... .......... .......... .......... 5% 113M 11s
14600K .......... .......... .......... .......... .......... 5% 61.9M 11s
14650K .......... .......... .......... .......... .......... 5% 110M 11s
14700K .......... .......... .......... .......... .......... 5% 79.7M 11s
14750K .......... .......... .......... .......... .......... 5% 3.12M 11s
14800K .......... .......... .......... .......... .......... 5% 103M 11s
14850K .......... .......... .......... .......... .......... 5% 67.3M 11s
14900K .......... .......... .......... .......... .......... 5% 91.8M 11s
14950K .......... .......... .......... .......... .......... 5% 52.1M 11s
15000K .......... .......... .......... .......... .......... 5% 126M 11s
15050K .......... .......... .......... .......... .......... 5% 87.8M 11s
15100K .......... .......... .......... .......... .......... 5% 3.59M 12s
15150K .......... .......... .......... .......... .......... 5% 68.4M 11s
15200K .......... .......... .......... .......... .......... 5% 50.6M 11s
15250K .......... .......... .......... .......... .......... 5% 59.8M 11s
15300K .......... .......... .......... .......... .......... 5% 116M 11s
15350K .......... .......... .......... .......... .......... 5% 51.9M 11s
15400K .......... .......... .......... .......... .......... 5% 98.4M 11s
15450K .......... .......... .......... .......... .......... 5% 3.07M 12s
15500K .......... .......... .......... .......... .......... 5% 83.9M 12s
15550K .......... .......... .......... .......... .......... 5% 74.5M 11s
15600K .......... .......... .......... .......... .......... 5% 81.2M 11s
15650K .......... .......... .......... .......... .......... 5% 100M 11s
15700K .......... .......... .......... .......... .......... 5% 48.5M 11s
15750K .......... .......... .......... .......... .......... 5% 101M 11s
15800K .......... .......... .......... .......... .......... 5% 3.58M 12s
15850K .......... .......... .......... .......... .......... 5% 89.1M 12s
15900K .......... .......... .......... .......... .......... 6% 104M 11s
15950K .......... .......... .......... .......... .......... 6% 82.1M 11s
16000K .......... .......... .......... .......... .......... 6% 53.9M 11s
16050K .......... .......... .......... .......... .......... 6% 76.3M 11s
16100K .......... .......... .......... .......... .......... 6% 88.3M 11s
16150K .......... .......... .......... .......... .......... 6% 3.66M 12s
16200K .......... .......... .......... .......... .......... 6% 56.9M 12s
16250K .......... .......... .......... .......... .......... 6% 121M 11s
16300K .......... .......... .......... .......... .......... 6% 129M 11s
16350K .......... .......... .......... .......... .......... 6% 75.4M 11s
16400K .......... .......... .......... .......... .......... 6% 54.9M 11s
16450K .......... .......... .......... .......... .......... 6% 81.5M 11s
16500K .......... .......... .......... .......... .......... 6% 3.56M 12s
16550K .......... .......... .......... .......... .......... 6% 78.6M 12s
16600K .......... .......... .......... .......... .......... 6% 79.5M 12s
16650K .......... .......... .......... .......... .......... 6% 90.1M 11s
16700K .......... .......... .......... .......... .......... 6% 51.9M 11s
16750K .......... .......... .......... .......... .......... 6% 58.4M 11s
16800K .......... .......... .......... .......... .......... 6% 91.3M 11s
16850K .......... .......... .......... .......... .......... 6% 3.66M 12s
16900K .......... .......... .......... .......... .......... 6% 118M 12s
16950K .......... .......... .......... .......... .......... 6% 82.1M 12s
17000K .......... .......... .......... .......... .......... 6% 126M 11s
17050K .......... .......... .......... .......... .......... 6% 96.7M 11s
17100K .......... .......... .......... .......... .......... 6% 88.9M 11s
17150K .......... .......... .......... .......... .......... 6% 105M 11s
17200K .......... .......... .......... .......... .......... 6% 3.46M 12s
17250K .......... .......... .......... .......... .......... 6% 68.2M 12s
17300K .......... .......... .......... .......... .......... 6% 123M 11s
17350K .......... .......... .......... .......... .......... 6% 92.7M 11s
17400K .......... .......... .......... .......... .......... 6% 14.3M 11s
17450K .......... .......... .......... .......... .......... 6% 69.7M 11s
17500K .......... .......... .......... .......... .......... 6% 96.1M 11s
17550K .......... .......... .......... .......... .......... 6% 128M 11s
17600K .......... .......... .......... .......... .......... 6% 136M 11s
17650K .......... .......... .......... .......... .......... 6% 6.58M 11s
17700K .......... .......... .......... .......... .......... 6% 92.8M 11s
17750K .......... .......... .......... .......... .......... 6% 108M 11s
17800K .......... .......... .......... .......... .......... 6% 138M 11s
17850K .......... .......... .......... .......... .......... 6% 94.4M 11s
17900K .......... .......... .......... .......... .......... 6% 8.68M 11s
17950K .......... .......... .......... .......... .......... 6% 81.1M 11s
18000K .......... .......... .......... .......... .......... 6% 105M 11s
18050K .......... .......... .......... .......... .......... 6% 17.0M 11s
18100K .......... .......... .......... .......... .......... 6% 6.97M 11s
18150K .......... .......... .......... .......... .......... 6% 58.3M 11s
18200K .......... .......... .......... .......... .......... 6% 78.3M 11s
18250K .......... .......... .......... .......... .......... 6% 97.3M 11s
18300K .......... .......... .......... .......... .......... 6% 26.1M 11s
18350K .......... .......... .......... .......... .......... 6% 3.43M 11s
18400K .......... .......... .......... .......... .......... 6% 8.75M 12s
18450K .......... .......... .......... .......... .......... 6% 62.4M 11s
18500K .......... .......... .......... .......... .......... 6% 89.1M 11s
18550K .......... .......... .......... .......... .......... 6% 133M 11s
18600K .......... .......... .......... .......... .......... 7% 65.5M 11s
18650K .......... .......... .......... .......... .......... 7% 119M 11s
18700K .......... .......... .......... .......... .......... 7% 102M 11s
18750K .......... .......... .......... .......... .......... 7% 101M 11s
18800K .......... .......... .......... .......... .......... 7% 110M 11s
18850K .......... .......... .......... .......... .......... 7% 17.8M 11s
18900K .......... .......... .......... .......... .......... 7% 62.0M 11s
18950K .......... .......... .......... .......... .......... 7% 90.4M 11s
19000K .......... .......... .......... .......... .......... 7% 64.0M 11s
19050K .......... .......... .......... .......... .......... 7% 12.4M 11s
19100K .......... .......... .......... .......... .......... 7% 10.0M 11s
19150K .......... .......... .......... .......... .......... 7% 86.4M 11s
19200K .......... .......... .......... .......... .......... 7% 22.5M 11s
19250K .......... .......... .......... .......... .......... 7% 8.82M 11s
19300K .......... .......... .......... .......... .......... 7% 74.0M 11s
19350K .......... .......... .......... .......... .......... 7% 12.6M 11s
19400K .......... .......... .......... .......... .......... 7% 6.25M 11s
19450K .......... .......... .......... .......... .......... 7% 45.3M 11s
19500K .......... .......... .......... .......... .......... 7% 100M 11s
19550K .......... .......... .......... .......... .......... 7% 5.73M 11s
19600K .......... .......... .......... .......... .......... 7% 69.1M 11s
19650K .......... .......... .......... .......... .......... 7% 79.9M 11s
19700K .......... .......... .......... .......... .......... 7% 61.0M 11s
19750K .......... .......... .......... .......... .......... 7% 5.27M 11s
19800K .......... .......... .......... .......... .......... 7% 84.0M 11s
19850K .......... .......... .......... .......... .......... 7% 57.3M 11s
19900K .......... .......... .......... .......... .......... 7% 5.78M 11s
19950K .......... .......... .......... .......... .......... 7% 75.0M 11s
20000K .......... .......... .......... .......... .......... 7% 113M 11s
20050K .......... .......... .......... .......... .......... 7% 77.4M 11s
20100K .......... .......... .......... .......... .......... 7% 4.58M 11s
20150K .......... .......... .......... .......... .......... 7% 81.1M 11s
20200K .......... .......... .......... .......... .......... 7% 91.8M 11s
20250K .......... .......... .......... .......... .......... 7% 4.16M 12s
20300K .......... .......... .......... .......... .......... 7% 111M 12s
20350K .......... .......... .......... .......... .......... 7% 4.84M 12s
20400K .......... .......... .......... .......... .......... 7% 57.3M 12s
20450K .......... .......... .......... .......... .......... 7% 68.8M 12s
20500K .......... .......... .......... .......... .......... 7% 5.47M 12s
20550K .......... .......... .......... .......... .......... 7% 117M 12s
20600K .......... .......... .......... .......... .......... 7% 121M 12s
20650K .......... .......... .......... .......... .......... 7% 145M 12s
20700K .......... .......... .......... .......... .......... 7% 7.25M 12s
20750K .......... .......... .......... .......... .......... 7% 140M 12s
20800K .......... .......... .......... .......... .......... 7% 7.09M 12s
20850K .......... .......... .......... .......... .......... 7% 55.2M 12s
20900K .......... .......... .......... .......... .......... 7% 138M 12s
20950K .......... .......... .......... .......... .......... 7% 4.42M 12s
21000K .......... .......... .......... .......... .......... 7% 104M 12s
21050K .......... .......... .......... .......... .......... 7% 8.44M 12s
21100K .......... .......... .......... .......... .......... 7% 61.7M 12s
21150K .......... .......... .......... .......... .......... 7% 99.9M 12s
21200K .......... .......... .......... .......... .......... 7% 7.73M 12s
21250K .......... .......... .......... .......... .......... 8% 180M 12s
21300K .......... .......... .......... .......... .......... 8% 9.40M 12s
21350K .......... .......... .......... .......... .......... 8% 113M 12s
21400K .......... .......... .......... .......... .......... 8% 220M 12s
21450K .......... .......... .......... .......... .......... 8% 9.18M 12s
21500K .......... .......... .......... .......... .......... 8% 52.4M 12s
21550K .......... .......... .......... .......... .......... 8% 99.0M 12s
21600K .......... .......... .......... .......... .......... 8% 6.03M 12s
21650K .......... .......... .......... .......... .......... 8% 196M 12s
21700K .......... .......... .......... .......... .......... 8% 7.60M 12s
21750K .......... .......... .......... .......... .......... 8% 150M 12s
21800K .......... .......... .......... .......... .......... 8% 119M 12s
21850K .......... .......... .......... .......... .......... 8% 9.23M 12s
21900K .......... .......... .......... .......... .......... 8% 184M 12s
21950K .......... .......... .......... .......... .......... 8% 8.74M 12s
22000K .......... .......... .......... .......... .......... 8% 174M 12s
22050K .......... .......... .......... .......... .......... 8% 162M 12s
22100K .......... .......... .......... .......... .......... 8% 6.58M 12s
22150K .......... .......... .......... .......... .......... 8% 127M 12s
22200K .......... .......... .......... .......... .......... 8% 81.2M 12s
22250K .......... .......... .......... .......... .......... 8% 6.50M 12s
22300K .......... .......... .......... .......... .......... 8% 126M 12s
22350K .......... .......... .......... .......... .......... 8% 6.45M 12s
22400K .......... .......... .......... .......... .......... 8% 64.0M 12s
22450K .......... .......... .......... .......... .......... 8% 54.7M 12s
22500K .......... .......... .......... .......... .......... 8% 7.76M 12s
22550K .......... .......... .......... .......... .......... 8% 62.6M 12s
22600K .......... .......... .......... .......... .......... 8% 121M 12s
22650K .......... .......... .......... .......... .......... 8% 8.08M 12s
22700K .......... .......... .......... .......... .......... 8% 90.8M 12s
22750K .......... .......... .......... .......... .......... 8% 182M 12s
22800K .......... .......... .......... .......... .......... 8% 8.88M 12s
22850K .......... .......... .......... .......... .......... 8% 9.17M 12s
22900K .......... .......... .......... .......... .......... 8% 9.92M 12s
22950K .......... .......... .......... .......... .......... 8% 133M 12s
23000K .......... .......... .......... .......... .......... 8% 121M 12s
23050K .......... .......... .......... .......... .......... 8% 102M 12s
23100K .......... .......... .......... .......... .......... 8% 8.63M 12s
23150K .......... .......... .......... .......... .......... 8% 203M 12s
23200K .......... .......... .......... .......... .......... 8% 10.3M 12s
23250K .......... .......... .......... .......... .......... 8% 142M 12s
23300K .......... .......... .......... .......... .......... 8% 7.37M 12s
23350K .......... .......... .......... .......... .......... 8% 156M 12s
23400K .......... .......... .......... .......... .......... 8% 7.54M 12s
23450K .......... .......... .......... .......... .......... 8% 6.94M 12s
23500K .......... .......... .......... .......... .......... 8% 93.9M 12s
23550K .......... .......... .......... .......... .......... 8% 61.7M 12s
23600K .......... .......... .......... .......... .......... 8% 6.97M 12s
23650K .......... .......... .......... .......... .......... 8% 6.27M 12s
23700K .......... .......... .......... .......... .......... 8% 105M 12s
23750K .......... .......... .......... .......... .......... 8% 8.45M 12s
23800K .......... .......... .......... .......... .......... 8% 82.3M 12s
23850K .......... .......... .......... .......... .......... 8% 7.89M 12s
23900K .......... .......... .......... .......... .......... 9% 95.2M 12s
23950K .......... .......... .......... .......... .......... 9% 7.27M 12s
24000K .......... .......... .......... .......... .......... 9% 117M 12s
24050K .......... .......... .......... .......... .......... 9% 111M 12s
24100K .......... .......... .......... .......... .......... 9% 7.31M 12s
24150K .......... .......... .......... .......... .......... 9% 96.1M 12s
24200K .......... .......... .......... .......... .......... 9% 6.89M 12s
24250K .......... .......... .......... .......... .......... 9% 149M 12s
24300K .......... .......... .......... .......... .......... 9% 7.07M 12s
24350K .......... .......... .......... .......... .......... 9% 176M 12s
24400K .......... .......... .......... .......... .......... 9% 8.62M 12s
24450K .......... .......... .......... .......... .......... 9% 125M 12s
24500K .......... .......... .......... .......... .......... 9% 8.77M 12s
24550K .......... .......... .......... .......... .......... 9% 865K 12s
24600K .......... .......... .......... .......... .......... 9% 6.65M 13s
24650K .......... .......... .......... .......... .......... 9% 146M 12s
24700K .......... .......... .......... .......... .......... 9% 8.02M 13s
24750K .......... .......... .......... .......... .......... 9% 161M 13s
24800K .......... .......... .......... .......... .......... 9% 5.24M 13s
24850K .......... .......... .......... .......... .......... 9% 132M 13s
24900K .......... .......... .......... .......... .......... 9% 151M 13s
24950K .......... .......... .......... .......... .......... 9% 6.78M 13s
25000K .......... .......... .......... .......... .......... 9% 161M 13s
25050K .......... .......... .......... .......... .......... 9% 7.73M 13s
25100K .......... .......... .......... .......... .......... 9% 98.4M 13s
25150K .......... .......... .......... .......... .......... 9% 6.92M 13s
25200K .......... .......... .......... .......... .......... 9% 98.2M 13s
25250K .......... .......... .......... .......... .......... 9% 7.65M 13s
25300K .......... .......... .......... .......... .......... 9% 194M 13s
25350K .......... .......... .......... .......... .......... 9% 8.05M 13s
25400K .......... .......... .......... .......... .......... 9% 4.67M 13s
25450K .......... .......... .......... .......... .......... 9% 74.2M 13s
25500K .......... .......... .......... .......... .......... 9% 63.7M 13s
25550K .......... .......... .......... .......... .......... 9% 97.1M 13s
25600K .......... .......... .......... .......... .......... 9% 19.1M 13s
25650K .......... .......... .......... .......... .......... 9% 50.6M 13s
25700K .......... .......... .......... .......... .......... 9% 9.75M 13s
25750K .......... .......... .......... .......... .......... 9% 60.3M 13s
25800K .......... .......... .......... .......... .......... 9% 8.51M 13s
25850K .......... .......... .......... .......... .......... 9% 128M 13s
25900K .......... .......... .......... .......... .......... 9% 10.3M 13s
25950K .......... .......... .......... .......... .......... 9% 9.90M 13s
26000K .......... .......... .......... .......... .......... 9% 130M 13s
26050K .......... .......... .......... .......... .......... 9% 8.95M 13s
26100K .......... .......... .......... .......... .......... 9% 111M 13s
26150K .......... .......... .......... .......... .......... 9% 6.19M 13s
26200K .......... .......... .......... .......... .......... 9% 8.65M 13s
26250K .......... .......... .......... .......... .......... 9% 4.55M 13s
26300K .......... .......... .......... .......... .......... 9% 104M 13s
26350K .......... .......... .......... .......... .......... 9% 88.0M 13s
26400K .......... .......... .......... .......... .......... 9% 114M 13s
26450K .......... .......... .......... .......... .......... 9% 14.6M 13s
26500K .......... .......... .......... .......... .......... 9% 8.30M 13s
26550K .......... .......... .......... .......... .......... 10% 11.3M 13s
26600K .......... .......... .......... .......... .......... 10% 9.72M 13s
26650K .......... .......... .......... .......... .......... 10% 108M 13s
26700K .......... .......... .......... .......... .......... 10% 9.12M 13s
26750K .......... .......... .......... .......... .......... 10% 10.9M 13s
26800K .......... .......... .......... .......... .......... 10% 9.71M 13s
26850K .......... .......... .......... .......... .......... 10% 6.84M 13s
26900K .......... .......... .......... .......... .......... 10% 163M 13s
26950K .......... .......... .......... .......... .......... 10% 7.43M 13s
27000K .......... .......... .......... .......... .......... 10% 7.91M 13s
27050K .......... .......... .......... .......... .......... 10% 8.74M 13s
27100K .......... .......... .......... .......... .......... 10% 9.26M 13s
27150K .......... .......... .......... .......... .......... 10% 111M 13s
27200K .......... .......... .......... .......... .......... 10% 5.72M 13s
27250K .......... .......... .......... .......... .......... 10% 8.09M 13s
27300K .......... .......... .......... .......... .......... 10% 121M 13s
27350K .......... .......... .......... .......... .......... 10% 5.20M 13s
27400K .......... .......... .......... .......... .......... 10% 12.0M 13s
27450K .......... .......... .......... .......... .......... 10% 10.6M 13s
27500K .......... .......... .......... .......... .......... 10% 9.99M 13s
27550K .......... .......... .......... .......... .......... 10% 9.80M 13s
27600K .......... .......... .......... .......... .......... 10% 11.5M 13s
27650K .......... .......... .......... .......... .......... 10% 8.87M 13s
27700K .......... .......... .......... .......... .......... 10% 8.82M 13s
27750K .......... .......... .......... .......... .......... 10% 9.09M 13s
27800K .......... .......... .......... .......... .......... 10% 111M 13s
27850K .......... .......... .......... .......... .......... 10% 9.06M 13s
27900K .......... .......... .......... .......... .......... 10% 9.48M 13s
27950K .......... .......... .......... .......... .......... 10% 4.46M 13s
28000K .......... .......... .......... .......... .......... 10% 205M 13s
28050K .......... .......... .......... .......... .......... 10% 5.93M 13s
28100K .......... .......... .......... .......... .......... 10% 9.14M 13s
28150K .......... .......... .......... .......... .......... 10% 8.01M 13s
28200K .......... .......... .......... .......... .......... 10% 9.58M 13s
28250K .......... .......... .......... .......... .......... 10% 2.26M 13s
28300K .......... .......... .......... .......... .......... 10% 12.5M 13s
28350K .......... .......... .......... .......... .......... 10% 14.3M 13s
28400K .......... .......... .......... .......... .......... 10% 13.2M 13s
28450K .......... .......... .......... .......... .......... 10% 16.0M 13s
28500K .......... .......... .......... .......... .......... 10% 12.1M 13s
28550K .......... .......... .......... .......... .......... 10% 12.6M 13s
28600K .......... .......... .......... .......... .......... 10% 12.7M 13s
28650K .......... .......... .......... .......... .......... 10% 12.1M 13s
28700K .......... .......... .......... .......... .......... 10% 4.04M 14s
28750K .......... .......... .......... .......... .......... 10% 187M 13s
28800K .......... .......... .......... .......... .......... 10% 133M 13s
28850K .......... .......... .......... .......... .......... 10% 5.45M 14s
28900K .......... .......... .......... .......... .......... 10% 9.80M 14s
28950K .......... .......... .......... .......... .......... 10% 8.83M 14s
29000K .......... .......... .......... .......... .......... 10% 9.06M 14s
29050K .......... .......... .......... .......... .......... 10% 4.75M 14s
29100K .......... .......... .......... .......... .......... 10% 7.98M 14s
29150K .......... .......... .......... .......... .......... 10% 11.3M 14s
29200K .......... .......... .......... .......... .......... 11% 8.93M 14s
29250K .......... .......... .......... .......... .......... 11% 9.90M 14s
29300K .......... .......... .......... .......... .......... 11% 8.55M 14s
29350K .......... .......... .......... .......... .......... 11% 11.6M 14s
29400K .......... .......... .......... .......... .......... 11% 11.6M 14s
29450K .......... .......... .......... .......... .......... 11% 12.1M 14s
29500K .......... .......... .......... .......... .......... 11% 10.8M 14s
29550K .......... .......... .......... .......... .......... 11% 8.71M 14s
29600K .......... .......... .......... .......... .......... 11% 6.66M 14s
29650K .......... .......... .......... .......... .......... 11% 9.68M 14s
29700K .......... .......... .......... .......... .......... 11% 8.20M 14s
29750K .......... .......... .......... .......... .......... 11% 9.00M 14s
29800K .......... .......... .......... .......... .......... 11% 8.62M 14s
29850K .......... .......... .......... .......... .......... 11% 11.0M 14s
29900K .......... .......... .......... .......... .......... 11% 10.7M 14s
29950K .......... .......... .......... .......... .......... 11% 9.75M 14s
30000K .......... .......... .......... .......... .......... 11% 7.86M 14s
30050K .......... .......... .......... .......... .......... 11% 105M 14s
30100K .......... .......... .......... .......... .......... 11% 10.9M 14s
30150K .......... .......... .......... .......... .......... 11% 12.0M 14s
30200K .......... .......... .......... .......... .......... 11% 11.8M 14s
30250K .......... .......... .......... .......... .......... 11% 10.5M 14s
30300K .......... .......... .......... .......... .......... 11% 6.97M 14s
30350K .......... .......... .......... .......... .......... 11% 7.14M 14s
30400K .......... .......... .......... .......... .......... 11% 87.7M 14s
30450K .......... .......... .......... .......... .......... 11% 9.30M 14s
30500K .......... .......... .......... .......... .......... 11% 7.23M 14s
30550K .......... .......... .......... .......... .......... 11% 8.06M 14s
30600K .......... .......... .......... .......... .......... 11% 8.89M 14s
30650K .......... .......... .......... .......... .......... 11% 109M 14s
30700K .......... .......... .......... .......... .......... 11% 10.2M 14s
30750K .......... .......... .......... .......... .......... 11% 10.3M 14s
30800K .......... .......... .......... .......... .......... 11% 151M 14s
30850K .......... .......... .......... .......... .......... 11% 10.2M 14s
30900K .......... .......... .......... .......... .......... 11% 10.1M 14s
30950K .......... .......... .......... .......... .......... 11% 11.7M 14s
31000K .......... .......... .......... .......... .......... 11% 132M 14s
31050K .......... .......... .......... .......... .......... 11% 9.00M 14s
31100K .......... .......... .......... .......... .......... 11% 7.87M 14s
31150K .......... .......... .......... .......... .......... 11% 184M 14s
31200K .......... .......... .......... .......... .......... 11% 14.6M 14s
31250K .......... .......... .......... .......... .......... 11% 14.5M 14s
31300K .......... .......... .......... .......... .......... 11% 16.8M 14s
31350K .......... .......... .......... .......... .......... 11% 10.6M 14s
31400K .......... .......... .......... .......... .......... 11% 23.3M 14s
31450K .......... .......... .......... .......... .......... 11% 11.8M 14s
31500K .......... .......... .......... .......... .......... 11% 7.42M 14s
31550K .......... .......... .......... .......... .......... 11% 12.6M 14s
31600K .......... .......... .......... .......... .......... 11% 11.0M 14s
31650K .......... .......... .......... .......... .......... 11% 10.1M 14s
31700K .......... .......... .......... .......... .......... 11% 10.6M 14s
31750K .......... .......... .......... .......... .......... 11% 11.9M 14s
31800K .......... .......... .......... .......... .......... 11% 155M 14s
31850K .......... .......... .......... .......... .......... 12% 11.5M 14s
31900K .......... .......... .......... .......... .......... 12% 11.5M 14s
31950K .......... .......... .......... .......... .......... 12% 12.5M 14s
32000K .......... .......... .......... .......... .......... 12% 12.0M 14s
32050K .......... .......... .......... .......... .......... 12% 5.12M 14s
32100K .......... .......... .......... .......... .......... 12% 91.6M 14s
32150K .......... .......... .......... .......... .......... 12% 148M 14s
32200K .......... .......... .......... .......... .......... 12% 8.75M 14s
32250K .......... .......... .......... .......... .......... 12% 13.1M 14s
32300K .......... .......... .......... .......... .......... 12% 15.4M 14s
32350K .......... .......... .......... .......... .......... 12% 7.86M 14s
32400K .......... .......... .......... .......... .......... 12% 13.2M 14s
32450K .......... .......... .......... .......... .......... 12% 12.4M 14s
32500K .......... .......... .......... .......... .......... 12% 13.8M 14s
32550K .......... .......... .......... .......... .......... 12% 13.4M 14s
32600K .......... .......... .......... .......... .......... 12% 5.34M 14s
32650K .......... .......... .......... .......... .......... 12% 17.3M 14s
32700K .......... .......... .......... .......... .......... 12% 10.0M 14s
32750K .......... .......... .......... .......... .......... 12% 11.5M 14s
32800K .......... .......... .......... .......... .......... 12% 11.4M 14s
32850K .......... .......... .......... .......... .......... 12% 11.9M 14s
32900K .......... .......... .......... .......... .......... 12% 11.2M 14s
32950K .......... .......... .......... .......... .......... 12% 11.5M 14s
33000K .......... .......... .......... .......... .......... 12% 14.5M 14s
33050K .......... .......... .......... .......... .......... 12% 9.28M 14s
33100K .......... .......... .......... .......... .......... 12% 13.6M 14s
33150K .......... .......... .......... .......... .......... 12% 12.7M 14s
33200K .......... .......... .......... .......... .......... 12% 12.1M 14s
33250K .......... .......... .......... .......... .......... 12% 12.3M 14s
33300K .......... .......... .......... .......... .......... 12% 13.8M 14s
33350K .......... .......... .......... .......... .......... 12% 14.0M 14s
33400K .......... .......... .......... .......... .......... 12% 13.2M 14s
33450K .......... .......... .......... .......... .......... 12% 10.5M 14s
33500K .......... .......... .......... .......... .......... 12% 171M 14s
33550K .......... .......... .......... .......... .......... 12% 10.0M 14s
33600K .......... .......... .......... .......... .......... 12% 10.9M 14s
33650K .......... .......... .......... .......... .......... 12% 12.3M 14s
33700K .......... .......... .......... .......... .......... 12% 11.3M 14s
33750K .......... .......... .......... .......... .......... 12% 118M 14s
33800K .......... .......... .......... .......... .......... 12% 10.3M 14s
33850K .......... .......... .......... .......... .......... 12% 10.6M 14s
33900K .......... .......... .......... .......... .......... 12% 9.72M 14s
33950K .......... .......... .......... .......... .......... 12% 9.26M 14s
34000K .......... .......... .......... .......... .......... 12% 170M 14s
34050K .......... .......... .......... .......... .......... 12% 11.0M 14s
34100K .......... .......... .......... .......... .......... 12% 10.6M 14s
34150K .......... .......... .......... .......... .......... 12% 9.74M 14s
34200K .......... .......... .......... .......... .......... 12% 8.25M 14s
34250K .......... .......... .......... .......... .......... 12% 70.6M 14s
34300K .......... .......... .......... .......... .......... 12% 11.2M 14s
34350K .......... .......... .......... .......... .......... 12% 10.6M 14s
34400K .......... .......... .......... .......... .......... 12% 10.7M 14s
34450K .......... .......... .......... .......... .......... 12% 71.9M 14s
34500K .......... .......... .......... .......... .......... 13% 8.00M 14s
34550K .......... .......... .......... .......... .......... 13% 8.69M 14s
34600K .......... .......... .......... .......... .......... 13% 81.7M 14s
34650K .......... .......... .......... .......... .......... 13% 10.8M 14s
34700K .......... .......... .......... .......... .......... 13% 11.2M 14s
34750K .......... .......... .......... .......... .......... 13% 137M 14s
34800K .......... .......... .......... .......... .......... 13% 9.71M 14s
34850K .......... .......... .......... .......... .......... 13% 10.2M 14s
34900K .......... .......... .......... .......... .......... 13% 12.3M 14s
34950K .......... .......... .......... .......... .......... 13% 64.6M 14s
35000K .......... .......... .......... .......... .......... 13% 11.6M 14s
35050K .......... .......... .......... .......... .......... 13% 6.84M 14s
35100K .......... .......... .......... .......... .......... 13% 99.0M 14s
35150K .......... .......... .......... .......... .......... 13% 189M 14s
35200K .......... .......... .......... .......... .......... 13% 6.98M 14s
35250K .......... .......... .......... .......... .......... 13% 52.0M 14s
35300K .......... .......... .......... .......... .......... 13% 17.0M 14s
35350K .......... .......... .......... .......... .......... 13% 10.8M 14s
35400K .......... .......... .......... .......... .......... 13% 11.0M 14s
35450K .......... .......... .......... .......... .......... 13% 12.3M 14s
35500K .......... .......... .......... .......... .......... 13% 13.1M 14s
35550K .......... .......... .......... .......... .......... 13% 9.56M 14s
35600K .......... .......... .......... .......... .......... 13% 10.5M 14s
35650K .......... .......... .......... .......... .......... 13% 11.0M 14s
35700K .......... .......... .......... .......... .......... 13% 10.3M 14s
35750K .......... .......... .......... .......... .......... 13% 64.2M 14s
35800K .......... .......... .......... .......... .......... 13% 4.20M 14s
35850K .......... .......... .......... .......... .......... 13% 132M 14s
35900K .......... .......... .......... .......... .......... 13% 136M 14s
35950K .......... .......... .......... .......... .......... 13% 14.7M 14s
36000K .......... .......... .......... .......... .......... 13% 8.00M 14s
36050K .......... .......... .......... .......... .......... 13% 13.7M 14s
36100K .......... .......... .......... .......... .......... 13% 12.5M 14s
36150K .......... .......... .......... .......... .......... 13% 16.2M 14s
36200K .......... .......... .......... .......... .......... 13% 12.6M 14s
36250K .......... .......... .......... .......... .......... 13% 7.80M 14s
36300K .......... .......... .......... .......... .......... 13% 13.1M 14s
36350K .......... .......... .......... .......... .......... 13% 13.3M 14s
36400K .......... .......... .......... .......... .......... 13% 12.1M 14s
36450K .......... .......... .......... .......... .......... 13% 9.66M 14s
36500K .......... .......... .......... .......... .......... 13% 13.2M 14s
36550K .......... .......... .......... .......... .......... 13% 11.1M 14s
36600K .......... .......... .......... .......... .......... 13% 11.9M 14s
36650K .......... .......... .......... .......... .......... 13% 11.3M 14s
36700K .......... .......... .......... .......... .......... 13% 8.79M 14s
36750K .......... .......... .......... .......... .......... 13% 9.59M 14s
36800K .......... .......... .......... .......... .......... 13% 10.3M 14s
36850K .......... .......... .......... .......... .......... 13% 11.3M 14s
36900K .......... .......... .......... .......... .......... 13% 10.6M 14s
36950K .......... .......... .......... .......... .......... 13% 10.4M 14s
37000K .......... .......... .......... .......... .......... 13% 91.4M 14s
37050K .......... .......... .......... .......... .......... 13% 13.9M 14s
37100K .......... .......... .......... .......... .......... 13% 10.3M 14s
37150K .......... .......... .......... .......... .......... 13% 12.0M 14s
37200K .......... .......... .......... .......... .......... 14% 10.3M 14s
37250K .......... .......... .......... .......... .......... 14% 10.7M 14s
37300K .......... .......... .......... .......... .......... 14% 6.55M 14s
37350K .......... .......... .......... .......... .......... 14% 10.8M 14s
37400K .......... .......... .......... .......... .......... 14% 83.0M 14s
37450K .......... .......... .......... .......... .......... 14% 10.5M 14s
37500K .......... .......... .......... .......... .......... 14% 11.1M 14s
37550K .......... .......... .......... .......... .......... 14% 10.7M 14s
37600K .......... .......... .......... .......... .......... 14% 9.69M 14s
37650K .......... .......... .......... .......... .......... 14% 54.6M 14s
37700K .......... .......... .......... .......... .......... 14% 8.87M 14s
37750K .......... .......... .......... .......... .......... 14% 8.88M 14s
37800K .......... .......... .......... .......... .......... 14% 9.16M 14s
37850K .......... .......... .......... .......... .......... 14% 58.1M 14s
37900K .......... .......... .......... .......... .......... 14% 8.69M 14s
37950K .......... .......... .......... .......... .......... 14% 5.70M 14s
38000K .......... .......... .......... .......... .......... 14% 8.65M 14s
38050K .......... .......... .......... .......... .......... 14% 102M 14s
38100K .......... .......... .......... .......... .......... 14% 8.55M 14s
38150K .......... .......... .......... .......... .......... 14% 7.61M 14s
38200K .......... .......... .......... .......... .......... 14% 127M 14s
38250K .......... .......... .......... .......... .......... 14% 8.52M 14s
38300K .......... .......... .......... .......... .......... 14% 9.31M 14s
38350K .......... .......... .......... .......... .......... 14% 47.4M 14s
38400K .......... .......... .......... .......... .......... 14% 7.91M 14s
38450K .......... .......... .......... .......... .......... 14% 5.22M 15s
38500K .......... .......... .......... .......... .......... 14% 6.49M 15s
38550K .......... .......... .......... .......... .......... 14% 40.2M 15s
38600K .......... .......... .......... .......... .......... 14% 6.88M 15s
38650K .......... .......... .......... .......... .......... 14% 126M 15s
38700K .......... .......... .......... .......... .......... 14% 4.89M 15s
38750K .......... .......... .......... .......... .......... 14% 32.6M 15s
38800K .......... .......... .......... .......... .......... 14% 7.72M 15s
38850K .......... .......... .......... .......... .......... 14% 7.22M 15s
38900K .......... .......... .......... .......... .......... 14% 66.3M 15s
38950K .......... .......... .......... .......... .......... 14% 3.67M 15s
39000K .......... .......... .......... .......... .......... 14% 8.92M 15s
39050K .......... .......... .......... .......... .......... 14% 68.8M 15s
39100K .......... .......... .......... .......... .......... 14% 12.6M 15s
39150K .......... .......... .......... .......... .......... 14% 143M 15s
39200K .......... .......... .......... .......... .......... 14% 9.35M 15s
39250K .......... .......... .......... .......... .......... 14% 10.7M 15s
39300K .......... .......... .......... .......... .......... 14% 10.9M 15s
39350K .......... .......... .......... .......... .......... 14% 7.83M 15s
39400K .......... .......... .......... .......... .......... 14% 8.09M 15s
39450K .......... .......... .......... .......... .......... 14% 10.6M 15s
39500K .......... .......... .......... .......... .......... 14% 10.8M 15s
39550K .......... .......... .......... .......... .......... 14% 93.2M 15s
39600K .......... .......... .......... .......... .......... 14% 11.6M 15s
39650K .......... .......... .......... .......... .......... 14% 10.9M 15s
39700K .......... .......... .......... .......... .......... 14% 8.19M 15s
39750K .......... .......... .......... .......... .......... 14% 9.72M 15s
39800K .......... .......... .......... .......... .......... 14% 76.9M 15s
39850K .......... .......... .......... .......... .......... 15% 3.65M 15s
39900K .......... .......... .......... .......... .......... 15% 113M 15s
39950K .......... .......... .......... .......... .......... 15% 13.0M 15s
40000K .......... .......... .......... .......... .......... 15% 12.1M 15s
40050K .......... .......... .......... .......... .......... 15% 17.9M 15s
40100K .......... .......... .......... .......... .......... 15% 13.3M 15s
40150K .......... .......... .......... .......... .......... 15% 12.0M 15s
40200K .......... .......... .......... .......... .......... 15% 13.9M 15s
40250K .......... .......... .......... .......... .......... 15% 13.8M 15s
40300K .......... .......... .......... .......... .......... 15% 14.2M 15s
40350K .......... .......... .......... .......... .......... 15% 6.26M 15s
40400K .......... .......... .......... .......... .......... 15% 13.0M 15s
40450K .......... .......... .......... .......... .......... 15% 11.0M 15s
40500K .......... .......... .......... .......... .......... 15% 10.3M 15s
40550K .......... .......... .......... .......... .......... 15% 11.0M 15s
40600K .......... .......... .......... .......... .......... 15% 8.61M 15s
40650K .......... .......... .......... .......... .......... 15% 11.0M 15s
40700K .......... .......... .......... .......... .......... 15% 9.42M 15s
40750K .......... .......... .......... .......... .......... 15% 12.0M 15s
40800K .......... .......... .......... .......... .......... 15% 10.2M 15s
40850K .......... .......... .......... .......... .......... 15% 9.33M 15s
40900K .......... .......... .......... .......... .......... 15% 122M 15s
40950K .......... .......... .......... .......... .......... 15% 7.38M 15s
41000K .......... .......... .......... .......... .......... 15% 10.3M 15s
41050K .......... .......... .......... .......... .......... 15% 10.4M 15s
41100K .......... .......... .......... .......... .......... 15% 11.6M 15s
41150K .......... .......... .......... .......... .......... 15% 9.84M 15s
41200K .......... .......... .......... .......... .......... 15% 10.9M 15s
41250K .......... .......... .......... .......... .......... 15% 96.7M 15s
41300K .......... .......... .......... .......... .......... 15% 9.80M 15s
41350K .......... .......... .......... .......... .......... 15% 4.13M 15s
41400K .......... .......... .......... .......... .......... 15% 155M 15s
41450K .......... .......... .......... .......... .......... 15% 115M 15s
41500K .......... .......... .......... .......... .......... 15% 14.1M 15s
41550K .......... .......... .......... .......... .......... 15% 14.5M 15s
41600K .......... .......... .......... .......... .......... 15% 13.5M 15s
41650K .......... .......... .......... .......... .......... 15% 14.7M 15s
41700K .......... .......... .......... .......... .......... 15% 7.18M 15s
41750K .......... .......... .......... .......... .......... 15% 8.53M 15s
41800K .......... .......... .......... .......... .......... 15% 13.4M 15s
41850K .......... .......... .......... .......... .......... 15% 12.6M 15s
41900K .......... .......... .......... .......... .......... 15% 12.8M 15s
41950K .......... .......... .......... .......... .......... 15% 7.66M 15s
42000K .......... .......... .......... .......... .......... 15% 9.81M 15s
42050K .......... .......... .......... .......... .......... 15% 11.8M 15s
42100K .......... .......... .......... .......... .......... 15% 12.0M 15s
42150K .......... .......... .......... .......... .......... 15% 11.5M 15s
42200K .......... .......... .......... .......... .......... 15% 9.59M 15s
42250K .......... .......... .......... .......... .......... 15% 11.8M 15s
42300K .......... .......... .......... .......... .......... 15% 10.8M 15s
42350K .......... .......... .......... .......... .......... 15% 6.69M 15s
42400K .......... .......... .......... .......... .......... 15% 98.8M 15s
42450K .......... .......... .......... .......... .......... 15% 9.41M 15s
42500K .......... .......... .......... .......... .......... 16% 11.6M 15s
42550K .......... .......... .......... .......... .......... 16% 9.84M 15s
42600K .......... .......... .......... .......... .......... 16% 10.7M 15s
42650K .......... .......... .......... .......... .......... 16% 10.5M 15s
42700K .......... .......... .......... .......... .......... 16% 10.1M 15s
42750K .......... .......... .......... .......... .......... 16% 120M 15s
42800K .......... .......... .......... .......... .......... 16% 10.2M 15s
42850K .......... .......... .......... .......... .......... 16% 4.39M 15s
42900K .......... .......... .......... .......... .......... 16% 114M 15s
42950K .......... .......... .......... .......... .......... 16% 11.2M 15s
43000K .......... .......... .......... .......... .......... 16% 10.9M 15s
43050K .......... .......... .......... .......... .......... 16% 11.2M 15s
43100K .......... .......... .......... .......... .......... 16% 6.05M 15s
43150K .......... .......... .......... .......... .......... 16% 10.5M 15s
43200K .......... .......... .......... .......... .......... 16% 11.0M 15s
43250K .......... .......... .......... .......... .......... 16% 9.99M 15s
43300K .......... .......... .......... .......... .......... 16% 5.46M 15s
43350K .......... .......... .......... .......... .......... 16% 11.2M 15s
43400K .......... .......... .......... .......... .......... 16% 5.76M 15s
43450K .......... .......... .......... .......... .......... 16% 138M 15s
43500K .......... .......... .......... .......... .......... 16% 7.04M 15s
43550K .......... .......... .......... .......... .......... 16% 13.0M 15s
43600K .......... .......... .......... .......... .......... 16% 6.04M 15s
43650K .......... .......... .......... .......... .......... 16% 11.8M 15s
43700K .......... .......... .......... .......... .......... 16% 12.2M 15s
43750K .......... .......... .......... .......... .......... 16% 7.18M 15s
43800K .......... .......... .......... .......... .......... 16% 8.11M 15s
43850K .......... .......... .......... .......... .......... 16% 10.4M 15s
43900K .......... .......... .......... .......... .......... 16% 13.7M 15s
43950K .......... .......... .......... .......... .......... 16% 10.3M 15s
44000K .......... .......... .......... .......... .......... 16% 8.20M 15s
44050K .......... .......... .......... .......... .......... 16% 5.39M 15s
44100K .......... .......... .......... .......... .......... 16% 11.0M 15s
44150K .......... .......... .......... .......... .......... 16% 10.1M 15s
44200K .......... .......... .......... .......... .......... 16% 9.70M 15s
44250K .......... .......... .......... .......... .......... 16% 9.86M 15s
44300K .......... .......... .......... .......... .......... 16% 10.6M 15s
44350K .......... .......... .......... .......... .......... 16% 10.4M 15s
44400K .......... .......... .......... .......... .......... 16% 7.36M 15s
44450K .......... .......... .......... .......... .......... 16% 7.45M 15s
44500K .......... .......... .......... .......... .......... 16% 10.2M 15s
44550K .......... .......... .......... .......... .......... 16% 9.80M 15s
44600K .......... .......... .......... .......... .......... 16% 6.04M 15s
44650K .......... .......... .......... .......... .......... 16% 8.29M 15s
44700K .......... .......... .......... .......... .......... 16% 9.19M 15s
44750K .......... .......... .......... .......... .......... 16% 83.8M 15s
44800K .......... .......... .......... .......... .......... 16% 9.42M 15s
44850K .......... .......... .......... .......... .......... 16% 8.15M 15s
44900K .......... .......... .......... .......... .......... 16% 9.70M 15s
44950K .......... .......... .......... .......... .......... 16% 9.67M 15s
45000K .......... .......... .......... .......... .......... 16% 10.6M 15s
45050K .......... .......... .......... .......... .......... 16% 2.51M 15s
45100K .......... .......... .......... .......... .......... 16% 7.57M 15s
45150K .......... .......... .......... .......... .......... 17% 86.3M 15s
45200K .......... .......... .......... .......... .......... 17% 5.13M 15s
45250K .......... .......... .......... .......... .......... 17% 5.20M 15s
45300K .......... .......... .......... .......... .......... 17% 7.86M 15s
45350K .......... .......... .......... .......... .......... 17% 7.95M 15s
45400K .......... .......... .......... .......... .......... 17% 168M 15s
45450K .......... .......... .......... .......... .......... 17% 7.48M 15s
45500K .......... .......... .......... .......... .......... 17% 5.51M 15s
45550K .......... .......... .......... .......... .......... 17% 4.37M 15s
45600K .......... .......... .......... .......... .......... 17% 154M 15s
45650K .......... .......... .......... .......... .......... 17% 8.46M 15s
45700K .......... .......... .......... .......... .......... 17% 4.02M 15s
45750K .......... .......... .......... .......... .......... 17% 9.51M 15s
45800K .......... .......... .......... .......... .......... 17% 176M 15s
45850K .......... .......... .......... .......... .......... 17% 3.54M 15s
45900K .......... .......... .......... .......... .......... 17% 7.50M 15s
45950K .......... .......... .......... .......... .......... 17% 7.59M 15s
46000K .......... .......... .......... .......... .......... 17% 138M 15s
46050K .......... .......... .......... .......... .......... 17% 6.56M 15s
46100K .......... .......... .......... .......... .......... 17% 8.44M 15s
46150K .......... .......... .......... .......... .......... 17% 94.6M 15s
46200K .......... .......... .......... .......... .......... 17% 6.02M 15s
46250K .......... .......... .......... .......... .......... 17% 5.17M 15s
46300K .......... .......... .......... .......... .......... 17% 210M 15s
46350K .......... .......... .......... .......... .......... 17% 7.60M 15s
46400K .......... .......... .......... .......... .......... 17% 7.46M 15s
46450K .......... .......... .......... .......... .......... 17% 166M 15s
46500K .......... .......... .......... .......... .......... 17% 5.62M 15s
46550K .......... .......... .......... .......... .......... 17% 5.02M 15s
46600K .......... .......... .......... .......... .......... 17% 145M 15s
46650K .......... .......... .......... .......... .......... 17% 6.98M 15s
46700K .......... .......... .......... .......... .......... 17% 6.37M 15s
46750K .......... .......... .......... .......... .......... 17% 135M 15s
46800K .......... .......... .......... .......... .......... 17% 6.18M 15s
46850K .......... .......... .......... .......... .......... 17% 6.42M 15s
46900K .......... .......... .......... .......... .......... 17% 106M 15s
46950K .......... .......... .......... .......... .......... 17% 5.39M 15s
47000K .......... .......... .......... .......... .......... 17% 186M 15s
47050K .......... .......... .......... .......... .......... 17% 8.13M 15s
47100K .......... .......... .......... .......... .......... 17% 4.28M 15s
47150K .......... .......... .......... .......... .......... 17% 111M 15s
47200K .......... .......... .......... .......... .......... 17% 3.20M 15s
47250K .......... .......... .......... .......... .......... 17% 46.7M 15s
47300K .......... .......... .......... .......... .......... 17% 4.53M 16s
47350K .......... .......... .......... .......... .......... 17% 5.08M 16s
47400K .......... .......... .......... .......... .......... 17% 193M 16s
47450K .......... .......... .......... .......... .......... 17% 5.17M 16s
47500K .......... .......... .......... .......... .......... 17% 180M 16s
47550K .......... .......... .......... .......... .......... 17% 6.72M 16s
47600K .......... .......... .......... .......... .......... 17% 5.27M 16s
47650K .......... .......... .......... .......... .......... 17% 158M 16s
47700K .......... .......... .......... .......... .......... 17% 7.20M 16s
47750K .......... .......... .......... .......... .......... 17% 163M 16s
47800K .......... .......... .......... .......... .......... 18% 7.90M 16s
47850K .......... .......... .......... .......... .......... 18% 93.5M 16s
47900K .......... .......... .......... .......... .......... 18% 5.10M 16s
47950K .......... .......... .......... .......... .......... 18% 7.18M 16s
48000K .......... .......... .......... .......... .......... 18% 178M 16s
48050K .......... .......... .......... .......... .......... 18% 5.14M 16s
48100K .......... .......... .......... .......... .......... 18% 83.5M 16s
48150K .......... .......... .......... .......... .......... 18% 5.13M 16s
48200K .......... .......... .......... .......... .......... 18% 103M 16s
48250K .......... .......... .......... .......... .......... 18% 5.21M 16s
48300K .......... .......... .......... .......... .......... 18% 222M 16s
48350K .......... .......... .......... .......... .......... 18% 8.20M 16s
48400K .......... .......... .......... .......... .......... 18% 5.60M 16s
48450K .......... .......... .......... .......... .......... 18% 95.2M 16s
48500K .......... .......... .......... .......... .......... 18% 4.83M 16s
48550K .......... .......... .......... .......... .......... 18% 154M 16s
48600K .......... .......... .......... .......... .......... 18% 4.73M 16s
48650K .......... .......... .......... .......... .......... 18% 184M 16s
48700K .......... .......... .......... .......... .......... 18% 7.73M 16s
48750K .......... .......... .......... .......... .......... 18% 142M 16s
48800K .......... .......... .......... .......... .......... 18% 4.82M 16s
48850K .......... .......... .......... .......... .......... 18% 128M 16s
48900K .......... .......... .......... .......... .......... 18% 8.13M 16s
48950K .......... .......... .......... .......... .......... 18% 122M 16s
49000K .......... .......... .......... .......... .......... 18% 12.1M 16s
49050K .......... .......... .......... .......... .......... 18% 155M 16s
49100K .......... .......... .......... .......... .......... 18% 10.2M 16s
49150K .......... .......... .......... .......... .......... 18% 103M 16s
49200K .......... .......... .......... .......... .......... 18% 12.2M 16s
49250K .......... .......... .......... .......... .......... 18% 268M 16s
49300K .......... .......... .......... .......... .......... 18% 11.0M 16s
49350K .......... .......... .......... .......... .......... 18% 100M 15s
49400K .......... .......... .......... .......... .......... 18% 11.9M 15s
49450K .......... .......... .......... .......... .......... 18% 137M 15s
49500K .......... .......... .......... .......... .......... 18% 10.3M 15s
49550K .......... .......... .......... .......... .......... 18% 132M 15s
49600K .......... .......... .......... .......... .......... 18% 9.21M 15s
49650K .......... .......... .......... .......... .......... 18% 103M 15s
49700K .......... .......... .......... .......... .......... 18% 9.45M 15s
49750K .......... .......... .......... .......... .......... 18% 153M 15s
49800K .......... .......... .......... .......... .......... 18% 6.77M 15s
49850K .......... .......... .......... .......... .......... 18% 86.7M 15s
49900K .......... .......... .......... .......... .......... 18% 6.59M 15s
49950K .......... .......... .......... .......... .......... 18% 56.8M 15s
50000K .......... .......... .......... .......... .......... 18% 4.07M 15s
50050K .......... .......... .......... .......... .......... 18% 130M 15s
50100K .......... .......... .......... .......... .......... 18% 7.68M 15s
50150K .......... .......... .......... .......... .......... 18% 1.71M 16s
50200K .......... .......... .......... .......... .......... 18% 4.75M 16s
50250K .......... .......... .......... .......... .......... 18% 143M 16s
50300K .......... .......... .......... .......... .......... 18% 4.19M 16s
50350K .......... .......... .......... .......... .......... 18% 150M 16s
50400K .......... .......... .......... .......... .......... 18% 1.86M 16s
50450K .......... .......... .......... .......... .......... 19% 100M 16s
50500K .......... .......... .......... .......... .......... 19% 84.2M 16s
50550K .......... .......... .......... .......... .......... 19% 2.42M 16s
50600K .......... .......... .......... .......... .......... 19% 184M 16s
50650K .......... .......... .......... .......... .......... 19% 3.04M 16s
50700K .......... .......... .......... .......... .......... 19% 146M 16s
50750K .......... .......... .......... .......... .......... 19% 4.12M 16s
50800K .......... .......... .......... .......... .......... 19% 197M 16s
50850K .......... .......... .......... .......... .......... 19% 3.27M 16s
50900K .......... .......... .......... .......... .......... 19% 190M 16s
50950K .......... .......... .......... .......... .......... 19% 4.77M 16s
51000K .......... .......... .......... .......... .......... 19% 198M 16s
51050K .......... .......... .......... .......... .......... 19% 110M 16s
51100K .......... .......... .......... .......... .......... 19% 3.55M 16s
51150K .......... .......... .......... .......... .......... 19% 151M 16s
51200K .......... .......... .......... .......... .......... 19% 2.74M 16s
51250K .......... .......... .......... .......... .......... 19% 22.8M 16s
51300K .......... .......... .......... .......... .......... 19% 2.95M 16s
51350K .......... .......... .......... .......... .......... 19% 55.0M 16s
51400K .......... .......... .......... .......... .......... 19% 3.73M 16s
51450K .......... .......... .......... .......... .......... 19% 87.0M 16s
51500K .......... .......... .......... .......... .......... 19% 124M 16s
51550K .......... .......... .......... .......... .......... 19% 3.01M 16s
51600K .......... .......... .......... .......... .......... 19% 126M 16s
51650K .......... .......... .......... .......... .......... 19% 3.15M 16s
51700K .......... .......... .......... .......... .......... 19% 170M 16s
51750K .......... .......... .......... .......... .......... 19% 3.86M 16s
51800K .......... .......... .......... .......... .......... 19% 113M 16s
51850K .......... .......... .......... .......... .......... 19% 130M 16s
51900K .......... .......... .......... .......... .......... 19% 2.72M 16s
51950K .......... .......... .......... .......... .......... 19% 94.4M 16s
52000K .......... .......... .......... .......... .......... 19% 4.78M 16s
52050K .......... .......... .......... .......... .......... 19% 160M 16s
52100K .......... .......... .......... .......... .......... 19% 135M 16s
52150K .......... .......... .......... .......... .......... 19% 4.26M 16s
52200K .......... .......... .......... .......... .......... 19% 71.8M 16s
52250K .......... .......... .......... .......... .......... 19% 5.86M 16s
52300K .......... .......... .......... .......... .......... 19% 106M 16s
52350K .......... .......... .......... .......... .......... 19% 5.91M 16s
52400K .......... .......... .......... .......... .......... 19% 174M 16s
52450K .......... .......... .......... .......... .......... 19% 74.3M 16s
52500K .......... .......... .......... .......... .......... 19% 5.99M 16s
52550K .......... .......... .......... .......... .......... 19% 214M 16s
52600K .......... .......... .......... .......... .......... 19% 5.52M 16s
52650K .......... .......... .......... .......... .......... 19% 114M 16s
52700K .......... .......... .......... .......... .......... 19% 75.8M 16s
52750K .......... .......... .......... .......... .......... 19% 6.09M 16s
52800K .......... .......... .......... .......... .......... 19% 154M 16s
52850K .......... .......... .......... .......... .......... 19% 5.85M 16s
52900K .......... .......... .......... .......... .......... 19% 194M 16s
52950K .......... .......... .......... .......... .......... 19% 4.25M 16s
53000K .......... .......... .......... .......... .......... 19% 84.0M 16s
53050K .......... .......... .......... .......... .......... 19% 157M 16s
53100K .......... .......... .......... .......... .......... 20% 5.34M 16s
53150K .......... .......... .......... .......... .......... 20% 158M 16s
53200K .......... .......... .......... .......... .......... 20% 3.91M 16s
53250K .......... .......... .......... .......... .......... 20% 86.1M 16s
53300K .......... .......... .......... .......... .......... 20% 70.1M 16s
53350K .......... .......... .......... .......... .......... 20% 4.06M 16s
53400K .......... .......... .......... .......... .......... 20% 214M 16s
53450K .......... .......... .......... .......... .......... 20% 115M 16s
53500K .......... .......... .......... .......... .......... 20% 4.92M 16s
53550K .......... .......... .......... .......... .......... 20% 108M 16s
53600K .......... .......... .......... .......... .......... 20% 4.33M 16s
53650K .......... .......... .......... .......... .......... 20% 111M 16s
53700K .......... .......... .......... .......... .......... 20% 136M 16s
53750K .......... .......... .......... .......... .......... 20% 6.25M 16s
53800K .......... .......... .......... .......... .......... 20% 179M 16s
53850K .......... .......... .......... .......... .......... 20% 6.38M 16s
53900K .......... .......... .......... .......... .......... 20% 45.4M 16s
53950K .......... .......... .......... .......... .......... 20% 105M 16s
54000K .......... .......... .......... .......... .......... 20% 4.04M 16s
54050K .......... .......... .......... .......... .......... 20% 148M 16s
54100K .......... .......... .......... .......... .......... 20% 92.7M 16s
54150K .......... .......... .......... .......... .......... 20% 3.55M 16s
54200K .......... .......... .......... .......... .......... 20% 132M 16s
54250K .......... .......... .......... .......... .......... 20% 5.39M 16s
54300K .......... .......... .......... .......... .......... 20% 75.7M 16s
54350K .......... .......... .......... .......... .......... 20% 88.1M 16s
54400K .......... .......... .......... .......... .......... 20% 4.07M 16s
54450K .......... .......... .......... .......... .......... 20% 109M 16s
54500K .......... .......... .......... .......... .......... 20% 153M 16s
54550K .......... .......... .......... .......... .......... 20% 3.87M 16s
54600K .......... .......... .......... .......... .......... 20% 141M 16s
54650K .......... .......... .......... .......... .......... 20% 1.87M 16s
54700K .......... .......... .......... .......... .......... 20% 129M 16s
54750K .......... .......... .......... .......... .......... 20% 192M 16s
54800K .......... .......... .......... .......... .......... 20% 2.26M 16s
54850K .......... .......... .......... .......... .......... 20% 139M 16s
54900K .......... .......... .......... .......... .......... 20% 186M 16s
54950K .......... .......... .......... .......... .......... 20% 4.11M 16s
55000K .......... .......... .......... .......... .......... 20% 130M 16s
55050K .......... .......... .......... .......... .......... 20% 5.36M 16s
55100K .......... .......... .......... .......... .......... 20% 74.8M 16s
55150K .......... .......... .......... .......... .......... 20% 76.9M 16s
55200K .......... .......... .......... .......... .......... 20% 3.94M 16s
55250K .......... .......... .......... .......... .......... 20% 61.9M 16s
55300K .......... .......... .......... .......... .......... 20% 182M 16s
55350K .......... .......... .......... .......... .......... 20% 3.91M 16s
55400K .......... .......... .......... .......... .......... 20% 194M 16s
55450K .......... .......... .......... .......... .......... 20% 160M 16s
55500K .......... .......... .......... .......... .......... 20% 4.83M 16s
55550K .......... .......... .......... .......... .......... 20% 157M 16s
55600K .......... .......... .......... .......... .......... 20% 3.57M 16s
55650K .......... .......... .......... .......... .......... 20% 132M 16s
55700K .......... .......... .......... .......... .......... 20% 84.8M 16s
55750K .......... .......... .......... .......... .......... 20% 4.05M 16s
55800K .......... .......... .......... .......... .......... 21% 126M 16s
55850K .......... .......... .......... .......... .......... 21% 69.0M 16s
55900K .......... .......... .......... .......... .......... 21% 3.81M 16s
55950K .......... .......... .......... .......... .......... 21% 118M 16s
56000K .......... .......... .......... .......... .......... 21% 145M 16s
56050K .......... .......... .......... .......... .......... 21% 4.99M 16s
56100K .......... .......... .......... .......... .......... 21% 65.3M 16s
56150K .......... .......... .......... .......... .......... 21% 189M 16s
56200K .......... .......... .......... .......... .......... 21% 3.26M 16s
56250K .......... .......... .......... .......... .......... 21% 144M 16s
56300K .......... .......... .......... .......... .......... 21% 8.45M 16s
56350K .......... .......... .......... .......... .......... 21% 4.88M 16s
56400K .......... .......... .......... .......... .......... 21% 147M 16s
56450K .......... .......... .......... .......... .......... 21% 4.92M 16s
56500K .......... .......... .......... .......... .......... 21% 179M 16s
56550K .......... .......... .......... .......... .......... 21% 182M 16s
56600K .......... .......... .......... .......... .......... 21% 3.06M 16s
56650K .......... .......... .......... .......... .......... 21% 184M 16s
56700K .......... .......... .......... .......... .......... 21% 173M 16s
56750K .......... .......... .......... .......... .......... 21% 4.80M 16s
56800K .......... .......... .......... .......... .......... 21% 3.03M 16s
56850K .......... .......... .......... .......... .......... 21% 114M 16s
56900K .......... .......... .......... .......... .......... 21% 197M 16s
56950K .......... .......... .......... .......... .......... 21% 138M 16s
57000K .......... .......... .......... .......... .......... 21% 186M 16s
57050K .......... .......... .......... .......... .......... 21% 5.67M 16s
57100K .......... .......... .......... .......... .......... 21% 170M 16s
57150K .......... .......... .......... .......... .......... 21% 5.10M 16s
57200K .......... .......... .......... .......... .......... 21% 183M 16s
57250K .......... .......... .......... .......... .......... 21% 5.44M 16s
57300K .......... .......... .......... .......... .......... 21% 187M 16s
57350K .......... .......... .......... .......... .......... 21% 3.06M 16s
57400K .......... .......... .......... .......... .......... 21% 221M 16s
57450K .......... .......... .......... .......... .......... 21% 4.38M 16s
57500K .......... .......... .......... .......... .......... 21% 49.9M 16s
57550K .......... .......... .......... .......... .......... 21% 2.64M 16s
57600K .......... .......... .......... .......... .......... 21% 52.4M 16s
57650K .......... .......... .......... .......... .......... 21% 2.55M 16s
57700K .......... .......... .......... .......... .......... 21% 62.4M 16s
57750K .......... .......... .......... .......... .......... 21% 126M 16s
57800K .......... .......... .......... .......... .......... 21% 8.17M 16s
57850K .......... .......... .......... .......... .......... 21% 37.0M 16s
57900K .......... .......... .......... .......... .......... 21% 5.33M 16s
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58000K .......... .......... .......... .......... .......... 21% 5.47M 16s
58050K .......... .......... .......... .......... .......... 21% 3.24M 16s
58100K .......... .......... .......... .......... .......... 21% 143M 16s
58150K .......... .......... .......... .......... .......... 21% 5.49M 16s
58200K .......... .......... .......... .......... .......... 21% 3.75M 16s
58250K .......... .......... .......... .......... .......... 21% 170M 16s
58300K .......... .......... .......... .......... .......... 21% 5.25M 16s
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58400K .......... .......... .......... .......... .......... 21% 102M 16s
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58500K .......... .......... .......... .......... .......... 22% 203M 16s
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58600K .......... .......... .......... .......... .......... 22% 5.00M 16s
58650K .......... .......... .......... .......... .......... 22% 133M 16s
58700K .......... .......... .......... .......... .......... 22% 4.72M 16s
58750K .......... .......... .......... .......... .......... 22% 6.85M 16s
58800K .......... .......... .......... .......... .......... 22% 174M 16s
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58900K .......... .......... .......... .......... .......... 22% 176M 16s
58950K .......... .......... .......... .......... .......... 22% 5.67M 16s
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59050K .......... .......... .......... .......... .......... 22% 124M 16s
59100K .......... .......... .......... .......... .......... 22% 5.00M 16s
59150K .......... .......... .......... .......... .......... 22% 104M 16s
59200K .......... .......... .......... .......... .......... 22% 5.27M 16s
59250K .......... .......... .......... .......... .......... 22% 178M 16s
59300K .......... .......... .......... .......... .......... 22% 5.85M 16s
59350K .......... .......... .......... .......... .......... 22% 6.25M 16s
59400K .......... .......... .......... .......... .......... 22% 76.7M 16s
59450K .......... .......... .......... .......... .......... 22% 3.98M 16s
59500K .......... .......... .......... .......... .......... 22% 167M 16s
59550K .......... .......... .......... .......... .......... 22% 6.21M 16s
59600K .......... .......... .......... .......... .......... 22% 86.0M 16s
59650K .......... .......... .......... .......... .......... 22% 5.29M 16s
59700K .......... .......... .......... .......... .......... 22% 4.56M 16s
59750K .......... .......... .......... .......... .......... 22% 69.8M 16s
59800K .......... .......... .......... .......... .......... 22% 3.81M 16s
59850K .......... .......... .......... .......... .......... 22% 117M 16s
59900K .......... .......... .......... .......... .......... 22% 4.20M 16s
59950K .......... .......... .......... .......... .......... 22% 121M 16s
60000K .......... .......... .......... .......... .......... 22% 7.29M 16s
60050K .......... .......... .......... .......... .......... 22% 83.6M 16s
60100K .......... .......... .......... .......... .......... 22% 6.21M 16s
60150K .......... .......... .......... .......... .......... 22% 73.0M 16s
60200K .......... .......... .......... .......... .......... 22% 4.14M 16s
60250K .......... .......... .......... .......... .......... 22% 115M 16s
60300K .......... .......... .......... .......... .......... 22% 4.94M 16s
60350K .......... .......... .......... .......... .......... 22% 6.01M 16s
60400K .......... .......... .......... .......... .......... 22% 51.8M 16s
60450K .......... .......... .......... .......... .......... 22% 3.27M 16s
60500K .......... .......... .......... .......... .......... 22% 136M 16s
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60600K .......... .......... .......... .......... .......... 22% 35.0M 16s
60650K .......... .......... .......... .......... .......... 22% 3.49M 16s
60700K .......... .......... .......... .......... .......... 22% 82.8M 16s
60750K .......... .......... .......... .......... .......... 22% 5.13M 16s
60800K .......... .......... .......... .......... .......... 22% 82.6M 16s
60850K .......... .......... .......... .......... .......... 22% 3.91M 16s
60900K .......... .......... .......... .......... .......... 22% 103M 16s
60950K .......... .......... .......... .......... .......... 22% 3.54M 16s
61000K .......... .......... .......... .......... .......... 22% 94.4M 16s
61050K .......... .......... .......... .......... .......... 22% 3.45M 16s
61100K .......... .......... .......... .......... .......... 23% 107M 16s
61150K .......... .......... .......... .......... .......... 23% 4.85M 16s
61200K .......... .......... .......... .......... .......... 23% 97.7M 16s
61250K .......... .......... .......... .......... .......... 23% 5.53M 16s
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61400K .......... .......... .......... .......... .......... 23% 87.3M 16s
61450K .......... .......... .......... .......... .......... 23% 54.0M 16s
61500K .......... .......... .......... .......... .......... 23% 9.13M 16s
61550K .......... .......... .......... .......... .......... 23% 101M 16s
61600K .......... .......... .......... .......... .......... 23% 7.33M 16s
61650K .......... .......... .......... .......... .......... 23% 74.1M 16s
61700K .......... .......... .......... .......... .......... 23% 2.91M 16s
61750K .......... .......... .......... .......... .......... 23% 193M 16s
61800K .......... .......... .......... .......... .......... 23% 3.19M 16s
61850K .......... .......... .......... .......... .......... 23% 182M 16s
61900K .......... .......... .......... .......... .......... 23% 3.08M 16s
61950K .......... .......... .......... .......... .......... 23% 126M 16s
62000K .......... .......... .......... .......... .......... 23% 3.37M 16s
62050K .......... .......... .......... .......... .......... 23% 39.8M 16s
62100K .......... .......... .......... .......... .......... 23% 3.23M 16s
62150K .......... .......... .......... .......... .......... 23% 195M 16s
62200K .......... .......... .......... .......... .......... 23% 5.61M 16s
62250K .......... .......... .......... .......... .......... 23% 159M 16s
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62700K .......... .......... .......... .......... .......... 23% 54.0M 16s
62750K .......... .......... .......... .......... .......... 23% 142M 16s
62800K .......... .......... .......... .......... .......... 23% 1.79M 16s
62850K .......... .......... .......... .......... .......... 23% 104M 16s
62900K .......... .......... .......... .......... .......... 23% 3.72M 16s
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63000K .......... .......... .......... .......... .......... 23% 3.83M 16s
63050K .......... .......... .......... .......... .......... 23% 184M 16s
63100K .......... .......... .......... .......... .......... 23% 4.34M 16s
63150K .......... .......... .......... .......... .......... 23% 160M 16s
63200K .......... .......... .......... .......... .......... 23% 66.1M 16s
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63300K .......... .......... .......... .......... .......... 23% 94.1M 16s
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63700K .......... .......... .......... .......... .......... 23% 2.89M 16s
63750K .......... .......... .......... .......... .......... 24% 79.7M 16s
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63900K .......... .......... .......... .......... .......... 24% 94.4M 16s
63950K .......... .......... .......... .......... .......... 24% 2.70M 16s
64000K .......... .......... .......... .......... .......... 24% 193M 16s
64050K .......... .......... .......... .......... .......... 24% 4.05M 16s
64100K .......... .......... .......... .......... .......... 24% 150M 16s
64150K .......... .......... .......... .......... .......... 24% 118M 16s
64200K .......... .......... .......... .......... .......... 24% 2.94M 16s
64250K .......... .......... .......... .......... .......... 24% 171M 16s
64300K .......... .......... .......... .......... .......... 24% 4.35M 16s
64350K .......... .......... .......... .......... .......... 24% 119M 16s
64400K .......... .......... .......... .......... .......... 24% 129M 16s
64450K .......... .......... .......... .......... .......... 24% 3.53M 16s
64500K .......... .......... .......... .......... .......... 24% 86.7M 16s
64550K .......... .......... .......... .......... .......... 24% 4.62M 16s
64600K .......... .......... .......... .......... .......... 24% 132M 16s
64650K .......... .......... .......... .......... .......... 24% 140M 16s
64700K .......... .......... .......... .......... .......... 24% 3.32M 16s
64750K .......... .......... .......... .......... .......... 24% 148M 16s
64800K .......... .......... .......... .......... .......... 24% 3.95M 16s
64850K .......... .......... .......... .......... .......... 24% 176M 16s
64900K .......... .......... .......... .......... .......... 24% 104M 16s
64950K .......... .......... .......... .......... .......... 24% 3.38M 16s
65000K .......... .......... .......... .......... .......... 24% 191M 16s
65050K .......... .......... .......... .......... .......... 24% 3.07M 16s
65100K .......... .......... .......... .......... .......... 24% 62.9M 16s
65150K .......... .......... .......... .......... .......... 24% 48.6M 16s
65200K .......... .......... .......... .......... .......... 24% 3.43M 16s
65250K .......... .......... .......... .......... .......... 24% 174M 16s
65300K .......... .......... .......... .......... .......... 24% 189M 16s
65350K .......... .......... .......... .......... .......... 24% 4.52M 16s
65400K .......... .......... .......... .......... .......... 24% 121M 16s
65450K .......... .......... .......... .......... .......... 24% 3.43M 16s
65500K .......... .......... .......... .......... .......... 24% 8.40M 16s
65550K .......... .......... .......... .......... .......... 24% 117M 16s
65600K .......... .......... .......... .......... .......... 24% 5.21M 16s
65650K .......... .......... .......... .......... .......... 24% 133M 16s
65700K .......... .......... .......... .......... .......... 24% 2.61M 16s
65750K .......... .......... .......... .......... .......... 24% 205M 16s
65800K .......... .......... .......... .......... .......... 24% 102M 16s
65850K .......... .......... .......... .......... .......... 24% 3.34M 16s
65900K .......... .......... .......... .......... .......... 24% 212M 16s
65950K .......... .......... .......... .......... .......... 24% 189M 16s
66000K .......... .......... .......... .......... .......... 24% 3.92M 16s
66050K .......... .......... .......... .......... .......... 24% 132M 16s
66100K .......... .......... .......... .......... .......... 24% 2.76M 16s
66150K .......... .......... .......... .......... .......... 24% 189M 16s
66200K .......... .......... .......... .......... .......... 24% 173M 16s
66250K .......... .......... .......... .......... .......... 24% 3.06M 16s
66300K .......... .......... .......... .......... .......... 24% 67.0M 16s
66350K .......... .......... .......... .......... .......... 24% 131M 16s
66400K .......... .......... .......... .......... .......... 25% 6.32M 16s
66450K .......... .......... .......... .......... .......... 25% 182M 16s
66500K .......... .......... .......... .......... .......... 25% 5.74M 16s
66550K .......... .......... .......... .......... .......... 25% 958K 17s
66600K .......... .......... .......... .......... .......... 25% 7.99M 17s
66650K .......... .......... .......... .......... .......... 25% 127M 17s
66700K .......... .......... .......... .......... .......... 25% 5.25M 17s
66750K .......... .......... .......... .......... .......... 25% 123M 17s
66800K .......... .......... .......... .......... .......... 25% 5.56M 17s
66850K .......... .......... .......... .......... .......... 25% 168M 17s
66900K .......... .......... .......... .......... .......... 25% 5.54M 17s
66950K .......... .......... .......... .......... .......... 25% 173M 17s
67000K .......... .......... .......... .......... .......... 25% 4.51M 17s
67050K .......... .......... .......... .......... .......... 25% 164M 17s
67100K .......... .......... .......... .......... .......... 25% 4.65M 17s
67150K .......... .......... .......... .......... .......... 25% 128M 17s
67200K .......... .......... .......... .......... .......... 25% 3.78M 17s
67250K .......... .......... .......... .......... .......... 25% 142M 17s
67300K .......... .......... .......... .......... .......... 25% 1.72M 17s
67350K .......... .......... .......... .......... .......... 25% 125M 17s
67400K .......... .......... .......... .......... .......... 25% 3.69M 17s
67450K .......... .......... .......... .......... .......... 25% 62.1M 17s
67500K .......... .......... .......... .......... .......... 25% 3.13M 17s
67550K .......... .......... .......... .......... .......... 25% 80.2M 17s
67600K .......... .......... .......... .......... .......... 25% 4.68M 17s
67650K .......... .......... .......... .......... .......... 25% 170M 17s
67700K .......... .......... .......... .......... .......... 25% 4.89M 17s
67750K .......... .......... .......... .......... .......... 25% 104M 17s
67800K .......... .......... .......... .......... .......... 25% 4.44M 17s
67850K .......... .......... .......... .......... .......... 25% 162M 17s
67900K .......... .......... .......... .......... .......... 25% 5.44M 17s
67950K .......... .......... .......... .......... .......... 25% 126M 17s
68000K .......... .......... .......... .......... .......... 25% 4.80M 17s
68050K .......... .......... .......... .......... .......... 25% 178M 17s
68100K .......... .......... .......... .......... .......... 25% 4.08M 17s
68150K .......... .......... .......... .......... .......... 25% 220M 17s
68200K .......... .......... .......... .......... .......... 25% 5.07M 17s
68250K .......... .......... .......... .......... .......... 25% 198M 17s
68300K .......... .......... .......... .......... .......... 25% 4.61M 17s
68350K .......... .......... .......... .......... .......... 25% 159M 17s
68400K .......... .......... .......... .......... .......... 25% 4.22M 17s
68450K .......... .......... .......... .......... .......... 25% 140M 17s
68500K .......... .......... .......... .......... .......... 25% 2.84M 17s
68550K .......... .......... .......... .......... .......... 25% 121M 17s
68600K .......... .......... .......... .......... .......... 25% 59.4M 17s
68650K .......... .......... .......... .......... .......... 25% 3.83M 17s
68700K .......... .......... .......... .......... .......... 25% 168M 17s
68750K .......... .......... .......... .......... .......... 25% 4.74M 17s
68800K .......... .......... .......... .......... .......... 25% 143M 17s
68850K .......... .......... .......... .......... .......... 25% 4.61M 17s
68900K .......... .......... .......... .......... .......... 25% 99.2M 17s
68950K .......... .......... .......... .......... .......... 25% 3.30M 17s
69000K .......... .......... .......... .......... .......... 25% 63.2M 17s
69050K .......... .......... .......... .......... .......... 26% 3.28M 17s
69100K .......... .......... .......... .......... .......... 26% 77.9M 17s
69150K .......... .......... .......... .......... .......... 26% 207M 17s
69200K .......... .......... .......... .......... .......... 26% 4.98M 17s
69250K .......... .......... .......... .......... .......... 26% 131M 17s
69300K .......... .......... .......... .......... .......... 26% 4.50M 17s
69350K .......... .......... .......... .......... .......... 26% 187M 17s
69400K .......... .......... .......... .......... .......... 26% 3.19M 17s
69450K .......... .......... .......... .......... .......... 26% 119M 17s
69500K .......... .......... .......... .......... .......... 26% 8.69M 17s
69550K .......... .......... .......... .......... .......... 26% 165M 17s
69600K .......... .......... .......... .......... .......... 26% 102M 17s
69650K .......... .......... .......... .......... .......... 26% 9.71M 17s
69700K .......... .......... .......... .......... .......... 26% 132M 17s
69750K .......... .......... .......... .......... .......... 26% 8.62M 17s
69800K .......... .......... .......... .......... .......... 26% 111M 17s
69850K .......... .......... .......... .......... .......... 26% 7.33M 17s
69900K .......... .......... .......... .......... .......... 26% 157M 17s
69950K .......... .......... .......... .......... .......... 26% 3.16M 17s
70000K .......... .......... .......... .......... .......... 26% 139M 17s
70050K .......... .......... .......... .......... .......... 26% 154M 17s
70100K .......... .......... .......... .......... .......... 26% 3.53M 17s
70150K .......... .......... .......... .......... .......... 26% 166M 17s
70200K .......... .......... .......... .......... .......... 26% 3.43M 17s
70250K .......... .......... .......... .......... .......... 26% 121M 17s
70300K .......... .......... .......... .......... .......... 26% 122M 17s
70350K .......... .......... .......... .......... .......... 26% 4.65M 17s
70400K .......... .......... .......... .......... .......... 26% 101M 17s
70450K .......... .......... .......... .......... .......... 26% 4.57M 17s
70500K .......... .......... .......... .......... .......... 26% 187M 17s
70550K .......... .......... .......... .......... .......... 26% 3.94M 17s
70600K .......... .......... .......... .......... .......... 26% 133M 17s
70650K .......... .......... .......... .......... .......... 26% 8.31M 17s
70700K .......... .......... .......... .......... .......... 26% 3.90M 17s
70750K .......... .......... .......... .......... .......... 26% 157M 17s
70800K .......... .......... .......... .......... .......... 26% 3.93M 17s
70850K .......... .......... .......... .......... .......... 26% 89.3M 17s
70900K .......... .......... .......... .......... .......... 26% 121M 17s
70950K .......... .......... .......... .......... .......... 26% 3.61M 17s
71000K .......... .......... .......... .......... .......... 26% 120M 17s
71050K .......... .......... .......... .......... .......... 26% 4.51M 17s
71100K .......... .......... .......... .......... .......... 26% 79.3M 17s
71150K .......... .......... .......... .......... .......... 26% 133M 17s
71200K .......... .......... .......... .......... .......... 26% 3.38M 17s
71250K .......... .......... .......... .......... .......... 26% 107M 17s
71300K .......... .......... .......... .......... .......... 26% 4.94M 17s
71350K .......... .......... .......... .......... .......... 26% 97.1M 17s
71400K .......... .......... .......... .......... .......... 26% 82.8M 17s
71450K .......... .......... .......... .......... .......... 26% 3.38M 17s
71500K .......... .......... .......... .......... .......... 26% 189M 17s
71550K .......... .......... .......... .......... .......... 26% 3.93M 17s
71600K .......... .......... .......... .......... .......... 26% 109M 17s
71650K .......... .......... .......... .......... .......... 26% 681K 17s
71700K .......... .......... .......... .......... .......... 26% 162M 17s
71750K .......... .......... .......... .......... .......... 27% 2.66M 17s
71800K .......... .......... .......... .......... .......... 27% 131M 17s
71850K .......... .......... .......... .......... .......... 27% 174M 17s
71900K .......... .......... .......... .......... .......... 27% 4.62M 17s
71950K .......... .......... .......... .......... .......... 27% 154M 17s
72000K .......... .......... .......... .......... .......... 27% 3.50M 17s
72050K .......... .......... .......... .......... .......... 27% 167M 17s
72100K .......... .......... .......... .......... .......... 27% 180M 17s
72150K .......... .......... .......... .......... .......... 27% 3.27M 17s
72200K .......... .......... .......... .......... .......... 27% 113M 17s
72250K .......... .......... .......... .......... .......... 27% 110M 17s
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72400K .......... .......... .......... .......... .......... 27% 4.01M 17s
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72600K .......... .......... .......... .......... .......... 27% 88.6M 17s
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72700K .......... .......... .......... .......... .......... 27% 84.6M 17s
72750K .......... .......... .......... .......... .......... 27% 77.4M 17s
72800K .......... .......... .......... .......... .......... 27% 3.92M 17s
72850K .......... .......... .......... .......... .......... 27% 89.9M 17s
72900K .......... .......... .......... .......... .......... 27% 120M 17s
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73000K .......... .......... .......... .......... .......... 27% 141M 17s
73050K .......... .......... .......... .......... .......... 27% 97.7M 17s
73100K .......... .......... .......... .......... .......... 27% 4.47M 17s
73150K .......... .......... .......... .......... .......... 27% 43.8M 17s
73200K .......... .......... .......... .......... .......... 27% 4.88M 17s
73250K .......... .......... .......... .......... .......... 27% 164M 17s
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73400K .......... .......... .......... .......... .......... 27% 105M 17s
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73500K .......... .......... .......... .......... .......... 27% 4.76M 17s
73550K .......... .......... .......... .......... .......... 27% 113M 17s
73600K .......... .......... .......... .......... .......... 27% 4.43M 17s
73650K .......... .......... .......... .......... .......... 27% 34.9M 17s
73700K .......... .......... .......... .......... .......... 27% 5.38M 17s
73750K .......... .......... .......... .......... .......... 27% 1.96M 17s
73800K .......... .......... .......... .......... .......... 27% 206M 17s
73850K .......... .......... .......... .......... .......... 27% 80.2M 17s
73900K .......... .......... .......... .......... .......... 27% 3.17M 17s
73950K .......... .......... .......... .......... .......... 27% 102M 17s
74000K .......... .......... .......... .......... .......... 27% 78.3M 17s
74050K .......... .......... .......... .......... .......... 27% 3.96M 17s
74100K .......... .......... .......... .......... .......... 27% 95.0M 17s
74150K .......... .......... .......... .......... .......... 27% 105M 17s
74200K .......... .......... .......... .......... .......... 27% 2.92M 17s
74250K .......... .......... .......... .......... .......... 27% 6.35M 17s
74300K .......... .......... .......... .......... .......... 27% 197M 17s
74350K .......... .......... .......... .......... .......... 27% 5.08M 17s
74400K .......... .......... .......... .......... .......... 28% 109M 17s
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74500K .......... .......... .......... .......... .......... 28% 215M 17s
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74850K .......... .......... .......... .......... .......... 28% 8.04M 17s
74900K .......... .......... .......... .......... .......... 28% 72.2M 17s
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75000K .......... .......... .......... .......... .......... 28% 174M 17s
75050K .......... .......... .......... .......... .......... 28% 4.75M 17s
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75150K .......... .......... .......... .......... .......... 28% 7.27M 17s
75200K .......... .......... .......... .......... .......... 28% 164M 17s
75250K .......... .......... .......... .......... .......... 28% 6.33M 17s
75300K .......... .......... .......... .......... .......... 28% 105M 17s
75350K .......... .......... .......... .......... .......... 28% 100M 17s
75400K .......... .......... .......... .......... .......... 28% 3.46M 17s
75450K .......... .......... .......... .......... .......... 28% 89.1M 17s
75500K .......... .......... .......... .......... .......... 28% 3.35M 17s
75550K .......... .......... .......... .......... .......... 28% 46.5M 17s
75600K .......... .......... .......... .......... .......... 28% 4.89M 17s
75650K .......... .......... .......... .......... .......... 28% 134M 17s
75700K .......... .......... .......... .......... .......... 28% 3.34M 17s
75750K .......... .......... .......... .......... .......... 28% 113M 17s
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75850K .......... .......... .......... .......... .......... 28% 62.9M 17s
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75950K .......... .......... .......... .......... .......... 28% 87.2M 17s
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76200K .......... .......... .......... .......... .......... 28% 49.2M 17s
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76300K .......... .......... .......... .......... .......... 28% 119M 17s
76350K .......... .......... .......... .......... .......... 28% 4.94M 17s
76400K .......... .......... .......... .......... .......... 28% 140M 17s
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76500K .......... .......... .......... .......... .......... 28% 130M 17s
76550K .......... .......... .......... .......... .......... 28% 206M 17s
76600K .......... .......... .......... .......... .......... 28% 6.53M 17s
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76700K .......... .......... .......... .......... .......... 28% 4.18M 17s
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76850K .......... .......... .......... .......... .......... 28% 90.3M 17s
76900K .......... .......... .......... .......... .......... 28% 173M 17s
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77000K .......... .......... .......... .......... .......... 28% 53.8M 17s
77050K .......... .......... .......... .......... .......... 29% 3.82M 17s
77100K .......... .......... .......... .......... .......... 29% 63.3M 17s
77150K .......... .......... .......... .......... .......... 29% 5.08M 17s
77200K .......... .......... .......... .......... .......... 29% 181M 17s
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77300K .......... .......... .......... .......... .......... 29% 4.81M 17s
77350K .......... .......... .......... .......... .......... 29% 56.5M 17s
77400K .......... .......... .......... .......... .......... 29% 3.97M 17s
77450K .......... .......... .......... .......... .......... 29% 34.9M 17s
77500K .......... .......... .......... .......... .......... 29% 3.61M 17s
77550K .......... .......... .......... .......... .......... 29% 114M 17s
77600K .......... .......... .......... .......... .......... 29% 61.8M 17s
77650K .......... .......... .......... .......... .......... 29% 3.90M 17s
77700K .......... .......... .......... .......... .......... 29% 93.5M 17s
77750K .......... .......... .......... .......... .......... 29% 5.11M 17s
77800K .......... .......... .......... .......... .......... 29% 126M 17s
77850K .......... .......... .......... .......... .......... 29% 3.61M 17s
77900K .......... .......... .......... .......... .......... 29% 86.6M 17s
77950K .......... .......... .......... .......... .......... 29% 131M 17s
78000K .......... .......... .......... .......... .......... 29% 4.23M 17s
78050K .......... .......... .......... .......... .......... 29% 87.7M 17s
78100K .......... .......... .......... .......... .......... 29% 3.87M 17s
78150K .......... .......... .......... .......... .......... 29% 78.8M 17s
78200K .......... .......... .......... .......... .......... 29% 164M 17s
78250K .......... .......... .......... .......... .......... 29% 5.26M 17s
78300K .......... .......... .......... .......... .......... 29% 184M 17s
78350K .......... .......... .......... .......... .......... 29% 4.83M 17s
78400K .......... .......... .......... .......... .......... 29% 153M 17s
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78500K .......... .......... .......... .......... .......... 29% 3.24M 17s
78550K .......... .......... .......... .......... .......... 29% 74.8M 17s
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78700K .......... .......... .......... .......... .......... 29% 174M 17s
78750K .......... .......... .......... .......... .......... 29% 4.90M 17s
78800K .......... .......... .......... .......... .......... 29% 138M 17s
78850K .......... .......... .......... .......... .......... 29% 82.2M 17s
78900K .......... .......... .......... .......... .......... 29% 4.58M 17s
78950K .......... .......... .......... .......... .......... 29% 167M 17s
79000K .......... .......... .......... .......... .......... 29% 4.36M 17s
79050K .......... .......... .......... .......... .......... 29% 206M 16s
79100K .......... .......... .......... .......... .......... 29% 182M 16s
79150K .......... .......... .......... .......... .......... 29% 4.42M 16s
79200K .......... .......... .......... .......... .......... 29% 173M 16s
79250K .......... .......... .......... .......... .......... 29% 4.45M 16s
79300K .......... .......... .......... .......... .......... 29% 99.6M 16s
79350K .......... .......... .......... .......... .......... 29% 113M 16s
79400K .......... .......... .......... .......... .......... 29% 3.91M 16s
79450K .......... .......... .......... .......... .......... 29% 105M 16s
79500K .......... .......... .......... .......... .......... 29% 128M 16s
79550K .......... .......... .......... .......... .......... 29% 3.36M 16s
79600K .......... .......... .......... .......... .......... 29% 156M 16s
79650K .......... .......... .......... .......... .......... 29% 5.24M 16s
79700K .......... .......... .......... .......... .......... 30% 116M 16s
79750K .......... .......... .......... .......... .......... 30% 100M 16s
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79850K .......... .......... .......... .......... .......... 30% 10.0M 16s
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80000K .......... .......... .......... .......... .......... 30% 138M 16s
80050K .......... .......... .......... .......... .......... 30% 3.07M 16s
80100K .......... .......... .......... .......... .......... 30% 25.4M 16s
80150K .......... .......... .......... .......... .......... 30% 133M 16s
80200K .......... .......... .......... .......... .......... 30% 3.75M 16s
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80350K .......... .......... .......... .......... .......... 30% 3.00M 16s
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80500K .......... .......... .......... .......... .......... 30% 111M 16s
80550K .......... .......... .......... .......... .......... 30% 69.9M 16s
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80650K .......... .......... .......... .......... .......... 30% 97.9M 16s
80700K .......... .......... .......... .......... .......... 30% 158M 16s
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80800K .......... .......... .......... .......... .......... 30% 188M 16s
80850K .......... .......... .......... .......... .......... 30% 107M 16s
80900K .......... .......... .......... .......... .......... 30% 2.79M 16s
80950K .......... .......... .......... .......... .......... 30% 163M 16s
81000K .......... .......... .......... .......... .......... 30% 202M 16s
81050K .......... .......... .......... .......... .......... 30% 3.99M 16s
81100K .......... .......... .......... .......... .......... 30% 57.7M 16s
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81200K .......... .......... .......... .......... .......... 30% 79.1M 16s
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81300K .......... .......... .......... .......... .......... 30% 2.81M 16s
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81450K .......... .......... .......... .......... .......... 30% 1.98M 16s
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81650K .......... .......... .......... .......... .......... 30% 127M 16s
81700K .......... .......... .......... .......... .......... 30% 135M 16s
81750K .......... .......... .......... .......... .......... 30% 1.93M 16s
81800K .......... .......... .......... .......... .......... 30% 174M 16s
81850K .......... .......... .......... .......... .......... 30% 130M 16s
81900K .......... .......... .......... .......... .......... 30% 2.18M 16s
81950K .......... .......... .......... .......... .......... 30% 112M 16s
82000K .......... .......... .......... .......... .......... 30% 122M 16s
82050K .......... .......... .......... .......... .......... 30% 3.14M 16s
82100K .......... .......... .......... .......... .......... 30% 73.9M 16s
82150K .......... .......... .......... .......... .......... 30% 113M 16s
82200K .......... .......... .......... .......... .......... 30% 1.91M 16s
82250K .......... .......... .......... .......... .......... 30% 201M 16s
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82500K .......... .......... .......... .......... .......... 31% 129M 16s
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82700K .......... .......... .......... .......... .......... 31% 98.4M 16s
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82800K .......... .......... .......... .......... .......... 31% 89.1M 16s
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83000K .......... .......... .......... .......... .......... 31% 148M 16s
83050K .......... .......... .......... .......... .......... 31% 4.48M 16s
83100K .......... .......... .......... .......... .......... 31% 124M 16s
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83200K .......... .......... .......... .......... .......... 31% 5.16M 16s
83250K .......... .......... .......... .......... .......... 31% 103M 16s
83300K .......... .......... .......... .......... .......... 31% 155M 16s
83350K .......... .......... .......... .......... .......... 31% 4.24M 16s
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83500K .......... .......... .......... .......... .......... 31% 4.26M 16s
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83650K .......... .......... .......... .......... .......... 31% 176M 16s
83700K .......... .......... .......... .......... .......... 31% 103M 16s
83750K .......... .......... .......... .......... .......... 31% 126M 16s
83800K .......... .......... .......... .......... .......... 31% 7.06M 16s
83850K .......... .......... .......... .......... .......... 31% 43.6M 16s
83900K .......... .......... .......... .......... .......... 31% 103M 16s
83950K .......... .......... .......... .......... .......... 31% 5.13M 16s
84000K .......... .......... .......... .......... .......... 31% 6.61M 16s
84050K .......... .......... .......... .......... .......... 31% 203M 16s
84100K .......... .......... .......... .......... .......... 31% 2.17M 16s
84150K .......... .......... .......... .......... .......... 31% 132M 16s
84200K .......... .......... .......... .......... .......... 31% 3.13M 16s
84250K .......... .......... .......... .......... .......... 31% 127M 16s
84300K .......... .......... .......... .......... .......... 31% 140M 16s
84350K .......... .......... .......... .......... .......... 31% 5.69M 16s
84400K .......... .......... .......... .......... .......... 31% 197M 16s
84450K .......... .......... .......... .......... .......... 31% 6.32M 16s
84500K .......... .......... .......... .......... .......... 31% 95.9M 16s
84550K .......... .......... .......... .......... .......... 31% 4.89M 16s
84600K .......... .......... .......... .......... .......... 31% 80.3M 16s
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84700K .......... .......... .......... .......... .......... 31% 82.1M 16s
84750K .......... .......... .......... .......... .......... 31% 190M 16s
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85000K .......... .......... .......... .......... .......... 32% 4.45M 16s
85050K .......... .......... .......... .......... .......... 32% 93.7M 16s
85100K .......... .......... .......... .......... .......... 32% 87.2M 16s
85150K .......... .......... .......... .......... .......... 32% 5.95M 16s
85200K .......... .......... .......... .......... .......... 32% 138M 16s
85250K .......... .......... .......... .......... .......... 32% 5.90M 16s
85300K .......... .......... .......... .......... .......... 32% 165M 16s
85350K .......... .......... .......... .......... .......... 32% 6.24M 16s
85400K .......... .......... .......... .......... .......... 32% 56.8M 16s
85450K .......... .......... .......... .......... .......... 32% 109M 16s
85500K .......... .......... .......... .......... .......... 32% 5.70M 16s
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85600K .......... .......... .......... .......... .......... 32% 6.37M 16s
85650K .......... .......... .......... .......... .......... 32% 127M 16s
85700K .......... .......... .......... .......... .......... 32% 5.84M 16s
85750K .......... .......... .......... .......... .......... 32% 153M 16s
85800K .......... .......... .......... .......... .......... 32% 148M 16s
85850K .......... .......... .......... .......... .......... 32% 6.00M 16s
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86000K .......... .......... .......... .......... .......... 32% 89.3M 16s
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86100K .......... .......... .......... .......... .......... 32% 6.11M 16s
86150K .......... .......... .......... .......... .......... 32% 83.0M 16s
86200K .......... .......... .......... .......... .......... 32% 5.79M 16s
86250K .......... .......... .......... .......... .......... 32% 109M 16s
86300K .......... .......... .......... .......... .......... 32% 97.7M 16s
86350K .......... .......... .......... .......... .......... 32% 4.57M 16s
86400K .......... .......... .......... .......... .......... 32% 98.4M 16s
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86600K .......... .......... .......... .......... .......... 32% 82.6M 16s
86650K .......... .......... .......... .......... .......... 32% 98.0M 16s
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87200K .......... .......... .......... .......... .......... 32% 4.12M 16s
87250K .......... .......... .......... .......... .......... 32% 189M 16s
87300K .......... .......... .......... .......... .......... 32% 174M 16s
87350K .......... .......... .......... .......... .......... 32% 3.16M 16s
87400K .......... .......... .......... .......... .......... 32% 142M 16s
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87500K .......... .......... .......... .......... .......... 32% 198M 16s
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87600K .......... .......... .......... .......... .......... 32% 5.31M 16s
87650K .......... .......... .......... .......... .......... 33% 147M 16s
87700K .......... .......... .......... .......... .......... 33% 5.19M 16s
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87850K .......... .......... .......... .......... .......... 33% 5.60M 16s
87900K .......... .......... .......... .......... .......... 33% 92.1M 16s
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88050K .......... .......... .......... .......... .......... 33% 76.9M 16s
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88150K .......... .......... .......... .......... .......... 33% 73.3M 16s
88200K .......... .......... .......... .......... .......... 33% 97.5M 16s
88250K .......... .......... .......... .......... .......... 33% 3.72M 16s
88300K .......... .......... .......... .......... .......... 33% 135M 16s
88350K .......... .......... .......... .......... .......... 33% 83.5M 16s
88400K .......... .......... .......... .......... .......... 33% 4.71M 16s
88450K .......... .......... .......... .......... .......... 33% 93.2M 16s
88500K .......... .......... .......... .......... .......... 33% 190M 16s
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88600K .......... .......... .......... .......... .......... 33% 168M 16s
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88700K .......... .......... .......... .......... .......... 33% 125M 16s
88750K .......... .......... .......... .......... .......... 33% 191M 16s
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88850K .......... .......... .......... .......... .......... 33% 61.3M 16s
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89100K .......... .......... .......... .......... .......... 33% 4.79M 16s
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89200K .......... .......... .......... .......... .......... 33% 6.17M 16s
89250K .......... .......... .......... .......... .......... 33% 97.9M 16s
89300K .......... .......... .......... .......... .......... 33% 109M 16s
89350K .......... .......... .......... .......... .......... 33% 3.56M 16s
89400K .......... .......... .......... .......... .......... 33% 115M 16s
89450K .......... .......... .......... .......... .......... 33% 50.4M 16s
89500K .......... .......... .......... .......... .......... 33% 3.32M 16s
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89600K .......... .......... .......... .......... .......... 33% 60.3M 16s
89650K .......... .......... .......... .......... .......... 33% 3.99M 16s
89700K .......... .......... .......... .......... .......... 33% 175M 16s
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89850K .......... .......... .......... .......... .......... 33% 77.4M 16s
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90700K .......... .......... .......... .......... .......... 34% 64.4M 16s
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90850K .......... .......... .......... .......... .......... 34% 65.0M 16s
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92250K .......... .......... .......... .......... .......... 34% 144M 16s
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92600K .......... .......... .......... .......... .......... 34% 95.2M 15s
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92800K .......... .......... .......... .......... .......... 34% 3.36M 15s
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93200K .......... .......... .......... .......... .......... 35% 74.8M 15s
93250K .......... .......... .......... .......... .......... 35% 2.00M 15s
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93550K .......... .......... .......... .......... .......... 35% 193M 15s
93600K .......... .......... .......... .......... .......... 35% 3.42M 15s
93650K .......... .......... .......... .......... .......... 35% 164M 15s
93700K .......... .......... .......... .......... .......... 35% 122M 15s
93750K .......... .......... .......... .......... .......... 35% 4.27M 15s
93800K .......... .......... .......... .......... .......... 35% 103M 15s
93850K .......... .......... .......... .......... .......... 35% 190M 15s
93900K .......... .......... .......... .......... .......... 35% 4.71M 15s
93950K .......... .......... .......... .......... .......... 35% 153M 15s
94000K .......... .......... .......... .......... .......... 35% 100M 15s
94050K .......... .......... .......... .......... .......... 35% 115M 15s
94100K .......... .......... .......... .......... .......... 35% 4.50M 15s
94150K .......... .......... .......... .......... .......... 35% 176M 15s
94200K .......... .......... .......... .......... .......... 35% 32.6M 15s
94250K .......... .......... .......... .......... .......... 35% 3.39M 15s
94300K .......... .......... .......... .......... .......... 35% 88.6M 15s
94350K .......... .......... .......... .......... .......... 35% 111M 15s
94400K .......... .......... .......... .......... .......... 35% 3.68M 15s
94450K .......... .......... .......... .......... .......... 35% 150M 15s
94500K .......... .......... .......... .......... .......... 35% 75.6M 15s
94550K .......... .......... .......... .......... .......... 35% 132M 15s
94600K .......... .......... .......... .......... .......... 35% 4.05M 15s
94650K .......... .......... .......... .......... .......... 35% 85.7M 15s
94700K .......... .......... .......... .......... .......... 35% 163M 15s
94750K .......... .......... .......... .......... .......... 35% 3.76M 15s
94800K .......... .......... .......... .......... .......... 35% 94.1M 15s
94850K .......... .......... .......... .......... .......... 35% 98.8M 15s
94900K .......... .......... .......... .......... .......... 35% 2.22M 15s
94950K .......... .......... .......... .......... .......... 35% 159M 15s
95000K .......... .......... .......... .......... .......... 35% 127M 15s
95050K .......... .......... .......... .......... .......... 35% 86.1M 15s
95100K .......... .......... .......... .......... .......... 35% 3.03M 15s
95150K .......... .......... .......... .......... .......... 35% 36.8M 15s
95200K .......... .......... .......... .......... .......... 35% 9.66M 15s
95250K .......... .......... .......... .......... .......... 35% 4.01M 15s
95300K .......... .......... .......... .......... .......... 35% 152M 15s
95350K .......... .......... .......... .......... .......... 35% 94.3M 15s
95400K .......... .......... .......... .......... .......... 35% 2.60M 15s
95450K .......... .......... .......... .......... .......... 35% 145M 15s
95500K .......... .......... .......... .......... .......... 35% 223M 15s
95550K .......... .......... .......... .......... .......... 35% 79.1M 15s
95600K .......... .......... .......... .......... .......... 35% 3.03M 15s
95650K .......... .......... .......... .......... .......... 36% 153M 15s
95700K .......... .......... .......... .......... .......... 36% 122M 15s
95750K .......... .......... .......... .......... .......... 36% 3.49M 15s
95800K .......... .......... .......... .......... .......... 36% 146M 15s
95850K .......... .......... .......... .......... .......... 36% 101M 15s
95900K .......... .......... .......... .......... .......... 36% 148M 15s
95950K .......... .......... .......... .......... .......... 36% 3.44M 15s
96000K .......... .......... .......... .......... .......... 36% 186M 15s
96050K .......... .......... .......... .......... .......... 36% 156M 15s
96100K .......... .......... .......... .......... .......... 36% 3.21M 15s
96150K .......... .......... .......... .......... .......... 36% 68.9M 15s
96200K .......... .......... .......... .......... .......... 36% 57.2M 15s
96250K .......... .......... .......... .......... .......... 36% 12.5M 15s
96300K .......... .......... .......... .......... .......... 36% 4.51M 15s
96350K .......... .......... .......... .......... .......... 36% 173M 15s
96400K .......... .......... .......... .......... .......... 36% 173M 15s
96450K .......... .......... .......... .......... .......... 36% 3.89M 15s
96500K .......... .......... .......... .......... .......... 36% 94.1M 15s
96550K .......... .......... .......... .......... .......... 36% 88.0M 15s
96600K .......... .......... .......... .......... .......... 36% 3.98M 15s
96650K .......... .......... .......... .......... .......... 36% 121M 15s
96700K .......... .......... .......... .......... .......... 36% 119M 15s
96750K .......... .......... .......... .......... .......... 36% 81.4M 15s
96800K .......... .......... .......... .......... .......... 36% 3.23M 15s
96850K .......... .......... .......... .......... .......... 36% 136M 15s
96900K .......... .......... .......... .......... .......... 36% 107M 15s
96950K .......... .......... .......... .......... .......... 36% 2.87M 15s
97000K .......... .......... .......... .......... .......... 36% 130M 15s
97050K .......... .......... .......... .......... .......... 36% 168M 15s
97100K .......... .......... .......... .......... .......... 36% 112M 15s
97150K .......... .......... .......... .......... .......... 36% 1.74M 15s
97200K .......... .......... .......... .......... .......... 36% 96.1M 15s
97250K .......... .......... .......... .......... .......... 36% 9.98M 15s
97300K .......... .......... .......... .......... .......... 36% 174M 15s
97350K .......... .......... .......... .......... .......... 36% 4.17M 15s
97400K .......... .......... .......... .......... .......... 36% 110M 15s
97450K .......... .......... .......... .......... .......... 36% 41.1M 15s
97500K .......... .......... .......... .......... .......... 36% 5.96M 15s
97550K .......... .......... .......... .......... .......... 36% 173M 15s
97600K .......... .......... .......... .......... .......... 36% 75.4M 15s
97650K .......... .......... .......... .......... .......... 36% 131M 15s
97700K .......... .......... .......... .......... .......... 36% 3.82M 15s
97750K .......... .......... .......... .......... .......... 36% 126M 15s
97800K .......... .......... .......... .......... .......... 36% 90.1M 15s
97850K .......... .......... .......... .......... .......... 36% 3.67M 15s
97900K .......... .......... .......... .......... .......... 36% 86.4M 15s
97950K .......... .......... .......... .......... .......... 36% 144M 15s
98000K .......... .......... .......... .......... .......... 36% 205M 15s
98050K .......... .......... .......... .......... .......... 36% 4.05M 15s
98100K .......... .......... .......... .......... .......... 36% 128M 15s
98150K .......... .......... .......... .......... .......... 36% 152M 15s
98200K .......... .......... .......... .......... .......... 36% 4.92M 15s
98250K .......... .......... .......... .......... .......... 36% 139M 15s
98300K .......... .......... .......... .......... .......... 37% 44.6M 15s
98350K .......... .......... .......... .......... .......... 37% 126M 15s
98400K .......... .......... .......... .......... .......... 37% 4.67M 15s
98450K .......... .......... .......... .......... .......... 37% 106M 15s
98500K .......... .......... .......... .......... .......... 37% 66.5M 15s
98550K .......... .......... .......... .......... .......... 37% 167M 15s
98600K .......... .......... .......... .......... .......... 37% 3.02M 15s
98650K .......... .......... .......... .......... .......... 37% 81.0M 15s
98700K .......... .......... .......... .......... .......... 37% 90.8M 15s
98750K .......... .......... .......... .......... .......... 37% 127M 15s
98800K .......... .......... .......... .......... .......... 37% 3.90M 15s
98850K .......... .......... .......... .......... .......... 37% 84.9M 15s
98900K .......... .......... .......... .......... .......... 37% 200M 15s
98950K .......... .......... .......... .......... .......... 37% 3.94M 15s
99000K .......... .......... .......... .......... .......... 37% 97.9M 15s
99050K .......... .......... .......... .......... .......... 37% 99.2M 15s
99100K .......... .......... .......... .......... .......... 37% 128M 15s
99150K .......... .......... .......... .......... .......... 37% 4.49M 15s
99200K .......... .......... .......... .......... .......... 37% 50.5M 15s
99250K .......... .......... .......... .......... .......... 37% 117M 15s
99300K .......... .......... .......... .......... .......... 37% 15.6M 15s
99350K .......... .......... .......... .......... .......... 37% 4.64M 15s
99400K .......... .......... .......... .......... .......... 37% 115M 15s
99450K .......... .......... .......... .......... .......... 37% 138M 15s
99500K .......... .......... .......... .......... .......... 37% 4.76M 15s
99550K .......... .......... .......... .......... .......... 37% 157M 15s
99600K .......... .......... .......... .......... .......... 37% 168M 15s
99650K .......... .......... .......... .......... .......... 37% 55.0M 15s
99700K .......... .......... .......... .......... .......... 37% 3.43M 15s
99750K .......... .......... .......... .......... .......... 37% 114M 15s
99800K .......... .......... .......... .......... .......... 37% 192M 15s
99850K .......... .......... .......... .......... .......... 37% 157M 15s
99900K .......... .......... .......... .......... .......... 37% 3.73M 15s
99950K .......... .......... .......... .......... .......... 37% 42.9M 15s
100000K .......... .......... .......... .......... .......... 37% 161M 15s
100050K .......... .......... .......... .......... .......... 37% 150M 15s
100100K .......... .......... .......... .......... .......... 37% 3.83M 15s
100150K .......... .......... .......... .......... .......... 37% 96.3M 15s
100200K .......... .......... .......... .......... .......... 37% 122M 15s
100250K .......... .......... .......... .......... .......... 37% 3.79M 15s
100300K .......... .......... .......... .......... .......... 37% 91.3M 15s
100350K .......... .......... .......... .......... .......... 37% 17.4M 15s
100400K .......... .......... .......... .......... .......... 37% 134M 15s
100450K .......... .......... .......... .......... .......... 37% 3.70M 15s
100500K .......... .......... .......... .......... .......... 37% 98.0M 15s
100550K .......... .......... .......... .......... .......... 37% 109M 15s
100600K .......... .......... .......... .......... .......... 37% 126M 15s
100650K .......... .......... .......... .......... .......... 37% 3.38M 15s
100700K .......... .......... .......... .......... .......... 37% 51.5M 15s
100750K .......... .......... .......... .......... .......... 37% 151M 15s
100800K .......... .......... .......... .......... .......... 37% 182M 15s
100850K .......... .......... .......... .......... .......... 37% 3.01M 15s
100900K .......... .......... .......... .......... .......... 37% 142M 15s
100950K .......... .......... .......... .......... .......... 38% 170M 15s
101000K .......... .......... .......... .......... .......... 38% 99.9M 15s
101050K .......... .......... .......... .......... .......... 38% 3.06M 15s
101100K .......... .......... .......... .......... .......... 38% 92.7M 15s
101150K .......... .......... .......... .......... .......... 38% 147M 15s
101200K .......... .......... .......... .......... .......... 38% 106M 15s
101250K .......... .......... .......... .......... .......... 38% 3.28M 15s
101300K .......... .......... .......... .......... .......... 38% 162M 15s
101350K .......... .......... .......... .......... .......... 38% 39.0M 15s
101400K .......... .......... .......... .......... .......... 38% 60.1M 15s
101450K .......... .......... .......... .......... .......... 38% 3.60M 15s
101500K .......... .......... .......... .......... .......... 38% 79.3M 15s
101550K .......... .......... .......... .......... .......... 38% 197M 15s
101600K .......... .......... .......... .......... .......... 38% 2.55M 15s
101650K .......... .......... .......... .......... .......... 38% 141M 15s
101700K .......... .......... .......... .......... .......... 38% 116M 15s
101750K .......... .......... .......... .......... .......... 38% 129M 15s
101800K .......... .......... .......... .......... .......... 38% 4.12M 15s
101850K .......... .......... .......... .......... .......... 38% 84.0M 15s
101900K .......... .......... .......... .......... .......... 38% 59.8M 15s
101950K .......... .......... .......... .......... .......... 38% 74.9M 15s
102000K .......... .......... .......... .......... .......... 38% 3.09M 15s
102050K .......... .......... .......... .......... .......... 38% 135M 15s
102100K .......... .......... .......... .......... .......... 38% 73.1M 15s
102150K .......... .......... .......... .......... .......... 38% 84.0M 15s
102200K .......... .......... .......... .......... .......... 38% 2.86M 15s
102250K .......... .......... .......... .......... .......... 38% 185M 15s
102300K .......... .......... .......... .......... .......... 38% 200M 15s
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102400K .......... .......... .......... .......... .......... 38% 3.49M 15s
102450K .......... .......... .......... .......... .......... 38% 70.8M 15s
102500K .......... .......... .......... .......... .......... 38% 140M 15s
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102750K .......... .......... .......... .......... .......... 38% 127M 15s
102800K .......... .......... .......... .......... .......... 38% 3.16M 15s
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102950K .......... .......... .......... .......... .......... 38% 71.2M 15s
103000K .......... .......... .......... .......... .......... 38% 4.33M 15s
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103100K .......... .......... .......... .......... .......... 38% 189M 15s
103150K .......... .......... .......... .......... .......... 38% 114M 15s
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103250K .......... .......... .......... .......... .......... 38% 130M 15s
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103350K .......... .......... .......... .......... .......... 38% 115M 14s
103400K .......... .......... .......... .......... .......... 38% 3.29M 15s
103450K .......... .......... .......... .......... .......... 38% 167M 14s
103500K .......... .......... .......... .......... .......... 38% 155M 14s
103550K .......... .......... .......... .......... .......... 38% 53.7M 14s
103600K .......... .......... .......... .......... .......... 39% 5.18M 14s
103650K .......... .......... .......... .......... .......... 39% 101M 14s
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103750K .......... .......... .......... .......... .......... 39% 3.26M 14s
103800K .......... .......... .......... .......... .......... 39% 164M 14s
103850K .......... .......... .......... .......... .......... 39% 99.4M 14s
103900K .......... .......... .......... .......... .......... 39% 97.9M 14s
103950K .......... .......... .......... .......... .......... 39% 4.04M 14s
104000K .......... .......... .......... .......... .......... 39% 105M 14s
104050K .......... .......... .......... .......... .......... 39% 83.2M 14s
104100K .......... .......... .......... .......... .......... 39% 106M 14s
104150K .......... .......... .......... .......... .......... 39% 2.85M 14s
104200K .......... .......... .......... .......... .......... 39% 97.5M 14s
104250K .......... .......... .......... .......... .......... 39% 87.3M 14s
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104350K .......... .......... .......... .......... .......... 39% 2.70M 14s
104400K .......... .......... .......... .......... .......... 39% 121M 14s
104450K .......... .......... .......... .......... .......... 39% 72.9M 14s
104500K .......... .......... .......... .......... .......... 39% 168M 14s
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104600K .......... .......... .......... .......... .......... 39% 3.85M 14s
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104700K .......... .......... .......... .......... .......... 39% 76.5M 14s
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104800K .......... .......... .......... .......... .......... 39% 3.38M 14s
104850K .......... .......... .......... .......... .......... 39% 128M 14s
104900K .......... .......... .......... .......... .......... 39% 164M 14s
104950K .......... .......... .......... .......... .......... 39% 75.0M 14s
105000K .......... .......... .......... .......... .......... 39% 3.50M 14s
105050K .......... .......... .......... .......... .......... 39% 99.4M 14s
105100K .......... .......... .......... .......... .......... 39% 104M 14s
105150K .......... .......... .......... .......... .......... 39% 95.9M 14s
105200K .......... .......... .......... .......... .......... 39% 2.56M 14s
105250K .......... .......... .......... .......... .......... 39% 42.2M 14s
105300K .......... .......... .......... .......... .......... 39% 137M 14s
105350K .......... .......... .......... .......... .......... 39% 108M 14s
105400K .......... .......... .......... .......... .......... 39% 2.77M 14s
105450K .......... .......... .......... .......... .......... 39% 5.87M 14s
105500K .......... .......... .......... .......... .......... 39% 169M 14s
105550K .......... .......... .......... .......... .......... 39% 193M 14s
105600K .......... .......... .......... .......... .......... 39% 3.31M 14s
105650K .......... .......... .......... .......... .......... 39% 191M 14s
105700K .......... .......... .......... .......... .......... 39% 178M 14s
105750K .......... .......... .......... .......... .......... 39% 96.1M 14s
105800K .......... .......... .......... .......... .......... 39% 45.1M 14s
105850K .......... .......... .......... .......... .......... 39% 3.37M 14s
105900K .......... .......... .......... .......... .......... 39% 109M 14s
105950K .......... .......... .......... .......... .......... 39% 49.5M 14s
106000K .......... .......... .......... .......... .......... 39% 105M 14s
106050K .......... .......... .......... .......... .......... 39% 3.31M 14s
106100K .......... .......... .......... .......... .......... 39% 75.6M 14s
106150K .......... .......... .......... .......... .......... 39% 49.5M 14s
106200K .......... .......... .......... .......... .......... 39% 112M 14s
106250K .......... .......... .......... .......... .......... 40% 3.24M 14s
106300K .......... .......... .......... .......... .......... 40% 73.2M 14s
106350K .......... .......... .......... .......... .......... 40% 48.8M 14s
106400K .......... .......... .......... .......... .......... 40% 189M 14s
106450K .......... .......... .......... .......... .......... 40% 3.54M 14s
106500K .......... .......... .......... .......... .......... 40% 56.6M 14s
106550K .......... .......... .......... .......... .......... 40% 119M 14s
106600K .......... .......... .......... .......... .......... 40% 110M 14s
106650K .......... .......... .......... .......... .......... 40% 112M 14s
106700K .......... .......... .......... .......... .......... 40% 3.63M 14s
106750K .......... .......... .......... .......... .......... 40% 81.8M 14s
106800K .......... .......... .......... .......... .......... 40% 96.5M 14s
106850K .......... .......... .......... .......... .......... 40% 105M 14s
106900K .......... .......... .......... .......... .......... 40% 4.05M 14s
106950K .......... .......... .......... .......... .......... 40% 160M 14s
107000K .......... .......... .......... .......... .......... 40% 109M 14s
107050K .......... .......... .......... .......... .......... 40% 170M 14s
107100K .......... .......... .......... .......... .......... 40% 3.90M 14s
107150K .......... .......... .......... .......... .......... 40% 140M 14s
107200K .......... .......... .......... .......... .......... 40% 160M 14s
107250K .......... .......... .......... .......... .......... 40% 180M 14s
107300K .......... .......... .......... .......... .......... 40% 193M 14s
107350K .......... .......... .......... .......... .......... 40% 4.02M 14s
107400K .......... .......... .......... .......... .......... 40% 97.7M 14s
107450K .......... .......... .......... .......... .......... 40% 163M 14s
107500K .......... .......... .......... .......... .......... 40% 16.6M 14s
107550K .......... .......... .......... .......... .......... 40% 5.28M 14s
107600K .......... .......... .......... .......... .......... 40% 120M 14s
107650K .......... .......... .......... .......... .......... 40% 127M 14s
107700K .......... .......... .......... .......... .......... 40% 125M 14s
107750K .......... .......... .......... .......... .......... 40% 4.50M 14s
107800K .......... .......... .......... .......... .......... 40% 209M 14s
107850K .......... .......... .......... .......... .......... 40% 170M 14s
107900K .......... .......... .......... .......... .......... 40% 220M 14s
107950K .......... .......... .......... .......... .......... 40% 4.09M 14s
108000K .......... .......... .......... .......... .......... 40% 99.9M 14s
108050K .......... .......... .......... .......... .......... 40% 65.8M 14s
108100K .......... .......... .......... .......... .......... 40% 120M 14s
108150K .......... .......... .......... .......... .......... 40% 128M 14s
108200K .......... .......... .......... .......... .......... 40% 3.60M 14s
108250K .......... .......... .......... .......... .......... 40% 179M 14s
108300K .......... .......... .......... .......... .......... 40% 124M 14s
108350K .......... .......... .......... .......... .......... 40% 156M 14s
108400K .......... .......... .......... .......... .......... 40% 189M 14s
108450K .......... .......... .......... .......... .......... 40% 128M 14s
108500K .......... .......... .......... .......... .......... 40% 9.56M 14s
108550K .......... .......... .......... .......... .......... 40% 152M 14s
108600K .......... .......... .......... .......... .......... 40% 167M 14s
108650K .......... .......... .......... .......... .......... 40% 188M 14s
108700K .......... .......... .......... .......... .......... 40% 9.53M 14s
108750K .......... .......... .......... .......... .......... 40% 7.17M 14s
108800K .......... .......... .......... .......... .......... 40% 7.98M 14s
108850K .......... .......... .......... .......... .......... 40% 151M 14s
108900K .......... .......... .......... .......... .......... 40% 6.60M 14s
108950K .......... .......... .......... .......... .......... 41% 67.2M 14s
109000K .......... .......... .......... .......... .......... 41% 124M 14s
109050K .......... .......... .......... .......... .......... 41% 4.00M 14s
109100K .......... .......... .......... .......... .......... 41% 100M 14s
109150K .......... .......... .......... .......... .......... 41% 137M 14s
109200K .......... .......... .......... .......... .......... 41% 3.06M 14s
109250K .......... .......... .......... .......... .......... 41% 4.20M 14s
109300K .......... .......... .......... .......... .......... 41% 120M 14s
109350K .......... .......... .......... .......... .......... 41% 110M 14s
109400K .......... .......... .......... .......... .......... 41% 109M 14s
109450K .......... .......... .......... .......... .......... 41% 119M 14s
109500K .......... .......... .......... .......... .......... 41% 107M 14s
109550K .......... .......... .......... .......... .......... 41% 7.78M 14s
109600K .......... .......... .......... .......... .......... 41% 132M 14s
109650K .......... .......... .......... .......... .......... 41% 7.94M 14s
109700K .......... .......... .......... .......... .......... 41% 76.9M 14s
109750K .......... .......... .......... .......... .......... 41% 5.04M 14s
109800K .......... .......... .......... .......... .......... 41% 131M 14s
109850K .......... .......... .......... .......... .......... 41% 6.82M 14s
109900K .......... .......... .......... .......... .......... 41% 125M 14s
109950K .......... .......... .......... .......... .......... 41% 53.1M 14s
110000K .......... .......... .......... .......... .......... 41% 4.34M 14s
110050K .......... .......... .......... .......... .......... 41% 121M 14s
110100K .......... .......... .......... .......... .......... 41% 4.98M 14s
110150K .......... .......... .......... .......... .......... 41% 174M 14s
110200K .......... .......... .......... .......... .......... 41% 4.02M 14s
110250K .......... .......... .......... .......... .......... 41% 141M 14s
110300K .......... .......... .......... .......... .......... 41% 168M 14s
110350K .......... .......... .......... .......... .......... 41% 4.09M 14s
110400K .......... .......... .......... .......... .......... 41% 139M 14s
110450K .......... .......... .......... .......... .......... 41% 3.84M 14s
110500K .......... .......... .......... .......... .......... 41% 107M 14s
110550K .......... .......... .......... .......... .......... 41% 4.65M 14s
110600K .......... .......... .......... .......... .......... 41% 111M 14s
110650K .......... .......... .......... .......... .......... 41% 4.03M 14s
110700K .......... .......... .......... .......... .......... 41% 71.8M 14s
110750K .......... .......... .......... .......... .......... 41% 64.2M 14s
110800K .......... .......... .......... .......... .......... 41% 4.71M 14s
110850K .......... .......... .......... .......... .......... 41% 92.7M 14s
110900K .......... .......... .......... .......... .......... 41% 4.43M 14s
110950K .......... .......... .......... .......... .......... 41% 172M 14s
111000K .......... .......... .......... .......... .......... 41% 7.28M 14s
111050K .......... .......... .......... .......... .......... 41% 121M 14s
111100K .......... .......... .......... .......... .......... 41% 156M 14s
111150K .......... .......... .......... .......... .......... 41% 5.54M 14s
111200K .......... .......... .......... .......... .......... 41% 121M 14s
111250K .......... .......... .......... .......... .......... 41% 3.83M 14s
111300K .......... .......... .......... .......... .......... 41% 184M 14s
111350K .......... .......... .......... .......... .......... 41% 3.68M 14s
111400K .......... .......... .......... .......... .......... 41% 146M 14s
111450K .......... .......... .......... .......... .......... 41% 97.3M 14s
111500K .......... .......... .......... .......... .......... 41% 3.43M 14s
111550K .......... .......... .......... .......... .......... 41% 185M 14s
111600K .......... .......... .......... .......... .......... 42% 4.03M 14s
111650K .......... .......... .......... .......... .......... 42% 44.3M 14s
111700K .......... .......... .......... .......... .......... 42% 71.9M 14s
111750K .......... .......... .......... .......... .......... 42% 4.08M 14s
111800K .......... .......... .......... .......... .......... 42% 127M 14s
111850K .......... .......... .......... .......... .......... 42% 3.67M 14s
111900K .......... .......... .......... .......... .......... 42% 28.8M 14s
111950K .......... .......... .......... .......... .......... 42% 113M 14s
112000K .......... .......... .......... .......... .......... 42% 3.59M 14s
112050K .......... .......... .......... .......... .......... 42% 103M 14s
112100K .......... .......... .......... .......... .......... 42% 3.76M 14s
112150K .......... .......... .......... .......... .......... 42% 195M 14s
112200K .......... .......... .......... .......... .......... 42% 170M 14s
112250K .......... .......... .......... .......... .......... 42% 5.43M 14s
112300K .......... .......... .......... .......... .......... 42% 162M 14s
112350K .......... .......... .......... .......... .......... 42% 3.95M 14s
112400K .......... .......... .......... .......... .......... 42% 173M 14s
112450K .......... .......... .......... .......... .......... 42% 126M 14s
112500K .......... .......... .......... .......... .......... 42% 5.44M 14s
112550K .......... .......... .......... .......... .......... 42% 107M 14s
112600K .......... .......... .......... .......... .......... 42% 3.36M 14s
112650K .......... .......... .......... .......... .......... 42% 142M 14s
112700K .......... .......... .......... .......... .......... 42% 173M 14s
112750K .......... .......... .......... .......... .......... 42% 4.73M 14s
112800K .......... .......... .......... .......... .......... 42% 51.7M 14s
112850K .......... .......... .......... .......... .......... 42% 78.6M 14s
112900K .......... .......... .......... .......... .......... 42% 3.48M 14s
112950K .......... .......... .......... .......... .......... 42% 103M 14s
113000K .......... .......... .......... .......... .......... 42% 4.02M 14s
113050K .......... .......... .......... .......... .......... 42% 155M 14s
113100K .......... .......... .......... .......... .......... 42% 124M 14s
113150K .......... .......... .......... .......... .......... 42% 4.58M 14s
113200K .......... .......... .......... .......... .......... 42% 60.1M 14s
113250K .......... .......... .......... .......... .......... 42% 4.05M 14s
113300K .......... .......... .......... .......... .......... 42% 101M 14s
113350K .......... .......... .......... .......... .......... 42% 166M 14s
113400K .......... .......... .......... .......... .......... 42% 6.27M 14s
113450K .......... .......... .......... .......... .......... 42% 104M 14s
113500K .......... .......... .......... .......... .......... 42% 92.3M 14s
113550K .......... .......... .......... .......... .......... 42% 4.21M 14s
113600K .......... .......... .......... .......... .......... 42% 160M 13s
113650K .......... .......... .......... .......... .......... 42% 2.85M 14s
113700K .......... .......... .......... .......... .......... 42% 90.3M 14s
113750K .......... .......... .......... .......... .......... 42% 192M 13s
113800K .......... .......... .......... .......... .......... 42% 6.06M 13s
113850K .......... .......... .......... .......... .......... 42% 176M 13s
113900K .......... .......... .......... .......... .......... 42% 204M 13s
113950K .......... .......... .......... .......... .......... 42% 5.89M 13s
114000K .......... .......... .......... .......... .......... 42% 163M 13s
114050K .......... .......... .......... .......... .......... 42% 139M 13s
114100K .......... .......... .......... .......... .......... 42% 3.22M 13s
114150K .......... .......... .......... .......... .......... 42% 138M 13s
114200K .......... .......... .......... .......... .......... 42% 4.11M 13s
114250K .......... .......... .......... .......... .......... 43% 156M 13s
114300K .......... .......... .......... .......... .......... 43% 173M 13s
114350K .......... .......... .......... .......... .......... 43% 5.93M 13s
114400K .......... .......... .......... .......... .......... 43% 165M 13s
114450K .......... .......... .......... .......... .......... 43% 102M 13s
114500K .......... .......... .......... .......... .......... 43% 4.72M 13s
114550K .......... .......... .......... .......... .......... 43% 174M 13s
114600K .......... .......... .......... .......... .......... 43% 5.46M 13s
114650K .......... .......... .......... .......... .......... 43% 103M 13s
114700K .......... .......... .......... .......... .......... 43% 162M 13s
114750K .......... .......... .......... .......... .......... 43% 4.57M 13s
114800K .......... .......... .......... .......... .......... 43% 119M 13s
114850K .......... .......... .......... .......... .......... 43% 75.4M 13s
114900K .......... .......... .......... .......... .......... 43% 3.35M 13s
114950K .......... .......... .......... .......... .......... 43% 77.1M 13s
115000K .......... .......... .......... .......... .......... 43% 160M 13s
115050K .......... .......... .......... .......... .......... 43% 4.96M 13s
115100K .......... .......... .......... .......... .......... 43% 36.2M 13s
115150K .......... .......... .......... .......... .......... 43% 71.3M 13s
115200K .......... .......... .......... .......... .......... 43% 4.13M 13s
115250K .......... .......... .......... .......... .......... 43% 156M 13s
115300K .......... .......... .......... .......... .......... 43% 120M 13s
115350K .......... .......... .......... .......... .......... 43% 4.00M 13s
115400K .......... .......... .......... .......... .......... 43% 143M 13s
115450K .......... .......... .......... .......... .......... 43% 3.66M 13s
115500K .......... .......... .......... .......... .......... 43% 31.3M 13s
115550K .......... .......... .......... .......... .......... 43% 44.1M 13s
115600K .......... .......... .......... .......... .......... 43% 3.51M 13s
115650K .......... .......... .......... .......... .......... 43% 137M 13s
115700K .......... .......... .......... .......... .......... 43% 12.1M 13s
115750K .......... .......... .......... .......... .......... 43% 3.46M 13s
115800K .......... .......... .......... .......... .......... 43% 127M 13s
115850K .......... .......... .......... .......... .......... 43% 178M 13s
115900K .......... .......... .......... .......... .......... 43% 4.43M 13s
115950K .......... .......... .......... .......... .......... 43% 166M 13s
116000K .......... .......... .......... .......... .......... 43% 4.98M 13s
116050K .......... .......... .......... .......... .......... 43% 28.7M 13s
116100K .......... .......... .......... .......... .......... 43% 108M 13s
116150K .......... .......... .......... .......... .......... 43% 6.57M 13s
116200K .......... .......... .......... .......... .......... 43% 4.71M 13s
116250K .......... .......... .......... .......... .......... 43% 189M 13s
116300K .......... .......... .......... .......... .......... 43% 71.8M 13s
116350K .......... .......... .......... .......... .......... 43% 3.18M 13s
116400K .......... .......... .......... .......... .......... 43% 102M 13s
116450K .......... .......... .......... .......... .......... 43% 77.6M 13s
116500K .......... .......... .......... .......... .......... 43% 3.10M 13s
116550K .......... .......... .......... .......... .......... 43% 206M 13s
116600K .......... .......... .......... .......... .......... 43% 152M 13s
116650K .......... .......... .......... .......... .......... 43% 2.96M 13s
116700K .......... .......... .......... .......... .......... 43% 70.5M 13s
116750K .......... .......... .......... .......... .......... 43% 95.0M 13s
116800K .......... .......... .......... .......... .......... 43% 4.48M 13s
116850K .......... .......... .......... .......... .......... 43% 56.6M 13s
116900K .......... .......... .......... .......... .......... 44% 109M 13s
116950K .......... .......... .......... .......... .......... 44% 4.26M 13s
117000K .......... .......... .......... .......... .......... 44% 110M 13s
117050K .......... .......... .......... .......... .......... 44% 100M 13s
117100K .......... .......... .......... .......... .......... 44% 4.78M 13s
117150K .......... .......... .......... .......... .......... 44% 159M 13s
117200K .......... .......... .......... .......... .......... 44% 106M 13s
117250K .......... .......... .......... .......... .......... 44% 4.88M 13s
117300K .......... .......... .......... .......... .......... 44% 126M 13s
117350K .......... .......... .......... .......... .......... 44% 6.27M 13s
117400K .......... .......... .......... .......... .......... 44% 8.01M 13s
117450K .......... .......... .......... .......... .......... 44% 6.66M 13s
117500K .......... .......... .......... .......... .......... 44% 99.4M 13s
117550K .......... .......... .......... .......... .......... 44% 7.10M 13s
117600K .......... .......... .......... .......... .......... 44% 86.9M 13s
117650K .......... .......... .......... .......... .......... 44% 156M 13s
117700K .......... .......... .......... .......... .......... 44% 4.27M 13s
117750K .......... .......... .......... .......... .......... 44% 11.7M 13s
117800K .......... .......... .......... .......... .......... 44% 5.98M 13s
117850K .......... .......... .......... .......... .......... 44% 132M 13s
117900K .......... .......... .......... .......... .......... 44% 5.04M 13s
117950K .......... .......... .......... .......... .......... 44% 155M 13s
118000K .......... .......... .......... .......... .......... 44% 4.34M 13s
118050K .......... .......... .......... .......... .......... 44% 162M 13s
118100K .......... .......... .......... .......... .......... 44% 3.94M 13s
118150K .......... .......... .......... .......... .......... 44% 130M 13s
118200K .......... .......... .......... .......... .......... 44% 167M 13s
118250K .......... .......... .......... .......... .......... 44% 6.14M 13s
118300K .......... .......... .......... .......... .......... 44% 119M 13s
118350K .......... .......... .......... .......... .......... 44% 5.46M 13s
118400K .......... .......... .......... .......... .......... 44% 203M 13s
118450K .......... .......... .......... .......... .......... 44% 3.70M 13s
118500K .......... .......... .......... .......... .......... 44% 155M 13s
118550K .......... .......... .......... .......... .......... 44% 3.29M 13s
118600K .......... .......... .......... .......... .......... 44% 70.0M 13s
118650K .......... .......... .......... .......... .......... 44% 73.8M 13s
118700K .......... .......... .......... .......... .......... 44% 3.19M 13s
118750K .......... .......... .......... .......... .......... 44% 104M 13s
118800K .......... .......... .......... .......... .......... 44% 5.22M 13s
118850K .......... .......... .......... .......... .......... 44% 53.4M 13s
118900K .......... .......... .......... .......... .......... 44% 3.72M 13s
118950K .......... .......... .......... .......... .......... 44% 109M 13s
119000K .......... .......... .......... .......... .......... 44% 208M 13s
119050K .......... .......... .......... .......... .......... 44% 5.05M 13s
119100K .......... .......... .......... .......... .......... 44% 92.8M 13s
119150K .......... .......... .......... .......... .......... 44% 4.36M 13s
119200K .......... .......... .......... .......... .......... 44% 64.5M 13s
119250K .......... .......... .......... .......... .......... 44% 4.93M 13s
119300K .......... .......... .......... .......... .......... 44% 115M 13s
119350K .......... .......... .......... .......... .......... 44% 86.3M 13s
119400K .......... .......... .......... .......... .......... 44% 2.14M 13s
119450K .......... .......... .......... .......... .......... 44% 60.1M 13s
119500K .......... .......... .......... .......... .......... 44% 4.04M 13s
119550K .......... .......... .......... .......... .......... 45% 144M 13s
119600K .......... .......... .......... .......... .......... 45% 178M 13s
119650K .......... .......... .......... .......... .......... 45% 3.87M 13s
119700K .......... .......... .......... .......... .......... 45% 173M 13s
119750K .......... .......... .......... .......... .......... 45% 2.49M 13s
119800K .......... .......... .......... .......... .......... 45% 6.61M 13s
119850K .......... .......... .......... .......... .......... 45% 164M 13s
119900K .......... .......... .......... .......... .......... 45% 203M 13s
119950K .......... .......... .......... .......... .......... 45% 180M 13s
120000K .......... .......... .......... .......... .......... 45% 6.62M 13s
120050K .......... .......... .......... .......... .......... 45% 146M 13s
120100K .......... .......... .......... .......... .......... 45% 5.20M 13s
120150K .......... .......... .......... .......... .......... 45% 191M 13s
120200K .......... .......... .......... .......... .......... 45% 6.40M 13s
120250K .......... .......... .......... .......... .......... 45% 4.60M 13s
120300K .......... .......... .......... .......... .......... 45% 143M 13s
120350K .......... .......... .......... .......... .......... 45% 6.06M 13s
120400K .......... .......... .......... .......... .......... 45% 124M 13s
120450K .......... .......... .......... .......... .......... 45% 5.00M 13s
120500K .......... .......... .......... .......... .......... 45% 191M 13s
120550K .......... .......... .......... .......... .......... 45% 4.92M 13s
120600K .......... .......... .......... .......... .......... 45% 3.14M 13s
120650K .......... .......... .......... .......... .......... 45% 92.1M 13s
120700K .......... .......... .......... .......... .......... 45% 3.80M 13s
120750K .......... .......... .......... .......... .......... 45% 212M 13s
120800K .......... .......... .......... .......... .......... 45% 5.93M 13s
120850K .......... .......... .......... .......... .......... 45% 138M 13s
120900K .......... .......... .......... .......... .......... 45% 2.69M 13s
120950K .......... .......... .......... .......... .......... 45% 173M 13s
121000K .......... .......... .......... .......... .......... 45% 4.77M 13s
121050K .......... .......... .......... .......... .......... 45% 4.67M 13s
121100K .......... .......... .......... .......... .......... 45% 59.4M 13s
121150K .......... .......... .......... .......... .......... 45% 5.68M 13s
121200K .......... .......... .......... .......... .......... 45% 171M 13s
121250K .......... .......... .......... .......... .......... 45% 4.14M 13s
121300K .......... .......... .......... .......... .......... 45% 182M 13s
121350K .......... .......... .......... .......... .......... 45% 5.56M 13s
121400K .......... .......... .......... .......... .......... 45% 178M 13s
121450K .......... .......... .......... .......... .......... 45% 2.39M 13s
121500K .......... .......... .......... .......... .......... 45% 147M 13s
121550K .......... .......... .......... .......... .......... 45% 3.96M 13s
121600K .......... .......... .......... .......... .......... 45% 183M 13s
121650K .......... .......... .......... .......... .......... 45% 4.78M 13s
121700K .......... .......... .......... .......... .......... 45% 172M 13s
121750K .......... .......... .......... .......... .......... 45% 3.35M 13s
121800K .......... .......... .......... .......... .......... 45% 144M 13s
121850K .......... .......... .......... .......... .......... 45% 4.68M 13s
121900K .......... .......... .......... .......... .......... 45% 213M 13s
121950K .......... .......... .......... .......... .......... 45% 3.01M 13s
122000K .......... .......... .......... .......... .......... 45% 158M 13s
122050K .......... .......... .......... .......... .......... 45% 2.82M 13s
122100K .......... .......... .......... .......... .......... 45% 125M 13s
122150K .......... .......... .......... .......... .......... 45% 3.36M 13s
122200K .......... .......... .......... .......... .......... 46% 81.1M 13s
122250K .......... .......... .......... .......... .......... 46% 4.96M 13s
122300K .......... .......... .......... .......... .......... 46% 84.3M 13s
122350K .......... .......... .......... .......... .......... 46% 5.03M 13s
122400K .......... .......... .......... .......... .......... 46% 112M 13s
122450K .......... .......... .......... .......... .......... 46% 4.52M 13s
122500K .......... .......... .......... .......... .......... 46% 76.7M 13s
122550K .......... .......... .......... .......... .......... 46% 4.34M 13s
122600K .......... .......... .......... .......... .......... 46% 63.3M 13s
122650K .......... .......... .......... .......... .......... 46% 3.48M 13s
122700K .......... .......... .......... .......... .......... 46% 174M 13s
122750K .......... .......... .......... .......... .......... 46% 6.05M 13s
122800K .......... .......... .......... .......... .......... 46% 81.9M 13s
122850K .......... .......... .......... .......... .......... 46% 3.52M 13s
122900K .......... .......... .......... .......... .......... 46% 105M 13s
122950K .......... .......... .......... .......... .......... 46% 5.20M 13s
123000K .......... .......... .......... .......... .......... 46% 156M 13s
123050K .......... .......... .......... .......... .......... 46% 182M 13s
123100K .......... .......... .......... .......... .......... 46% 3.70M 13s
123150K .......... .......... .......... .......... .......... 46% 135M 13s
123200K .......... .......... .......... .......... .......... 46% 3.76M 13s
123250K .......... .......... .......... .......... .......... 46% 143M 13s
123300K .......... .......... .......... .......... .......... 46% 3.78M 13s
123350K .......... .......... .......... .......... .......... 46% 130M 13s
123400K .......... .......... .......... .......... .......... 46% 4.47M 13s
123450K .......... .......... .......... .......... .......... 46% 92.0M 13s
123500K .......... .......... .......... .......... .......... 46% 4.36M 13s
123550K .......... .......... .......... .......... .......... 46% 91.8M 13s
123600K .......... .......... .......... .......... .......... 46% 98.0M 13s
123650K .......... .......... .......... .......... .......... 46% 3.88M 13s
123700K .......... .......... .......... .......... .......... 46% 187M 13s
123750K .......... .......... .......... .......... .......... 46% 5.83M 13s
123800K .......... .......... .......... .......... .......... 46% 78.9M 13s
123850K .......... .......... .......... .......... .......... 46% 4.77M 13s
123900K .......... .......... .......... .......... .......... 46% 70.1M 13s
123950K .......... .......... .......... .......... .......... 46% 5.36M 13s
124000K .......... .......... .......... .......... .......... 46% 172M 13s
124050K .......... .......... .......... .......... .......... 46% 174M 13s
124100K .......... .......... .......... .......... .......... 46% 4.89M 13s
124150K .......... .......... .......... .......... .......... 46% 101M 13s
124200K .......... .......... .......... .......... .......... 46% 5.84M 13s
124250K .......... .......... .......... .......... .......... 46% 129M 13s
124300K .......... .......... .......... .......... .......... 46% 6.57M 13s
124350K .......... .......... .......... .......... .......... 46% 163M 13s
124400K .......... .......... .......... .......... .......... 46% 115M 13s
124450K .......... .......... .......... .......... .......... 46% 5.38M 13s
124500K .......... .......... .......... .......... .......... 46% 147M 13s
124550K .......... .......... .......... .......... .......... 46% 5.58M 13s
124600K .......... .......... .......... .......... .......... 46% 142M 13s
124650K .......... .......... .......... .......... .......... 46% 2.75M 13s
124700K .......... .......... .......... .......... .......... 46% 171M 13s
124750K .......... .......... .......... .......... .......... 46% 55.5M 13s
124800K .......... .......... .......... .......... .......... 46% 2.66M 13s
124850K .......... .......... .......... .......... .......... 47% 63.4M 13s
124900K .......... .......... .......... .......... .......... 47% 3.92M 13s
124950K .......... .......... .......... .......... .......... 47% 95.7M 13s
125000K .......... .......... .......... .......... .......... 47% 2.86M 13s
125050K .......... .......... .......... .......... .......... 47% 100M 13s
125100K .......... .......... .......... .......... .......... 47% 116M 13s
125150K .......... .......... .......... .......... .......... 47% 2.92M 13s
125200K .......... .......... .......... .......... .......... 47% 55.9M 13s
125250K .......... .......... .......... .......... .......... 47% 3.44M 13s
125300K .......... .......... .......... .......... .......... 47% 80.2M 13s
125350K .......... .......... .......... .......... .......... 47% 55.1M 13s
125400K .......... .......... .......... .......... .......... 47% 2.12M 13s
125450K .......... .......... .......... .......... .......... 47% 120M 13s
125500K .......... .......... .......... .......... .......... 47% 4.88M 13s
125550K .......... .......... .......... .......... .......... 47% 104M 13s
125600K .......... .......... .......... .......... .......... 47% 110M 13s
125650K .......... .......... .......... .......... .......... 47% 4.59M 13s
125700K .......... .......... .......... .......... .......... 47% 89.3M 13s
125750K .......... .......... .......... .......... .......... 47% 3.16M 13s
125800K .......... .......... .......... .......... .......... 47% 185M 13s
125850K .......... .......... .......... .......... .......... 47% 167M 13s
125900K .......... .......... .......... .......... .......... 47% 4.56M 13s
125950K .......... .......... .......... .......... .......... 47% 73.1M 13s
126000K .......... .......... .......... .......... .......... 47% 3.04M 13s
126050K .......... .......... .......... .......... .......... 47% 180M 13s
126100K .......... .......... .......... .......... .......... 47% 182M 13s
126150K .......... .......... .......... .......... .......... 47% 5.01M 13s
126200K .......... .......... .......... .......... .......... 47% 4.23M 13s
126250K .......... .......... .......... .......... .......... 47% 3.79M 13s
126300K .......... .......... .......... .......... .......... 47% 83.8M 13s
126350K .......... .......... .......... .......... .......... 47% 160M 13s
126400K .......... .......... .......... .......... .......... 47% 3.54M 13s
126450K .......... .......... .......... .......... .......... 47% 189M 13s
126500K .......... .......... .......... .......... .......... 47% 5.39M 13s
126550K .......... .......... .......... .......... .......... 47% 147M 13s
126600K .......... .......... .......... .......... .......... 47% 136M 13s
126650K .......... .......... .......... .......... .......... 47% 3.93M 13s
126700K .......... .......... .......... .......... .......... 47% 151M 13s
126750K .......... .......... .......... .......... .......... 47% 44.7M 13s
126800K .......... .......... .......... .......... .......... 47% 3.24M 13s
126850K .......... .......... .......... .......... .......... 47% 170M 13s
126900K .......... .......... .......... .......... .......... 47% 3.12M 13s
126950K .......... .......... .......... .......... .......... 47% 79.4M 13s
127000K .......... .......... .......... .......... .......... 47% 170M 13s
127050K .......... .......... .......... .......... .......... 47% 3.36M 13s
127100K .......... .......... .......... .......... .......... 47% 123M 13s
127150K .......... .......... .......... .......... .......... 47% 204M 13s
127200K .......... .......... .......... .......... .......... 47% 2.63M 13s
127250K .......... .......... .......... .......... .......... 47% 131M 13s
127300K .......... .......... .......... .......... .......... 47% 3.49M 13s
127350K .......... .......... .......... .......... .......... 47% 110M 13s
127400K .......... .......... .......... .......... .......... 47% 38.2M 13s
127450K .......... .......... .......... .......... .......... 47% 4.61M 13s
127500K .......... .......... .......... .......... .......... 47% 135M 13s
127550K .......... .......... .......... .......... .......... 48% 57.1M 13s
127600K .......... .......... .......... .......... .......... 48% 3.84M 13s
127650K .......... .......... .......... .......... .......... 48% 68.0M 13s
127700K .......... .......... .......... .......... .......... 48% 3.14M 13s
127750K .......... .......... .......... .......... .......... 48% 28.8M 13s
127800K .......... .......... .......... .......... .......... 48% 164M 13s
127850K .......... .......... .......... .......... .......... 48% 4.69M 13s
127900K .......... .......... .......... .......... .......... 48% 160M 13s
127950K .......... .......... .......... .......... .......... 48% 185M 13s
128000K .......... .......... .......... .......... .......... 48% 1.58M 13s
128050K .......... .......... .......... .......... .......... 48% 54.1M 13s
128100K .......... .......... .......... .......... .......... 48% 50.8M 13s
128150K .......... .......... .......... .......... .......... 48% 3.13M 13s
128200K .......... .......... .......... .......... .......... 48% 167M 13s
128250K .......... .......... .......... .......... .......... 48% 3.27M 13s
128300K .......... .......... .......... .......... .......... 48% 80.7M 13s
128350K .......... .......... .......... .......... .......... 48% 125M 13s
128400K .......... .......... .......... .......... .......... 48% 3.05M 13s
128450K .......... .......... .......... .......... .......... 48% 55.7M 13s
128500K .......... .......... .......... .......... .......... 48% 120M 13s
128550K .......... .......... .......... .......... .......... 48% 3.08M 13s
128600K .......... .......... .......... .......... .......... 48% 112M 13s
128650K .......... .......... .......... .......... .......... 48% 157M 13s
128700K .......... .......... .......... .......... .......... 48% 3.76M 13s
128750K .......... .......... .......... .......... .......... 48% 201M 13s
128800K .......... .......... .......... .......... .......... 48% 176M 12s
128850K .......... .......... .......... .......... .......... 48% 4.10M 13s
128900K .......... .......... .......... .......... .......... 48% 168M 12s
128950K .......... .......... .......... .......... .......... 48% 3.23M 12s
129000K .......... .......... .......... .......... .......... 48% 70.1M 12s
129050K .......... .......... .......... .......... .......... 48% 101M 12s
129100K .......... .......... .......... .......... .......... 48% 3.95M 12s
129150K .......... .......... .......... .......... .......... 48% 117M 12s
129200K .......... .......... .......... .......... .......... 48% 61.9M 12s
129250K .......... .......... .......... .......... .......... 48% 3.25M 12s
129300K .......... .......... .......... .......... .......... 48% 239M 12s
129350K .......... .......... .......... .......... .......... 48% 172M 12s
129400K .......... .......... .......... .......... .......... 48% 2.94M 12s
129450K .......... .......... .......... .......... .......... 48% 79.3M 12s
129500K .......... .......... .......... .......... .......... 48% 106M 12s
129550K .......... .......... .......... .......... .......... 48% 2.80M 12s
129600K .......... .......... .......... .......... .......... 48% 125M 12s
129650K .......... .......... .......... .......... .......... 48% 173M 12s
129700K .......... .......... .......... .......... .......... 48% 3.22M 12s
129750K .......... .......... .......... .......... .......... 48% 150M 12s
129800K .......... .......... .......... .......... .......... 48% 115M 12s
129850K .......... .......... .......... .......... .......... 48% 4.18M 12s
129900K .......... .......... .......... .......... .......... 48% 174M 12s
129950K .......... .......... .......... .......... .......... 48% 138M 12s
130000K .......... .......... .......... .......... .......... 48% 3.69M 12s
130050K .......... .......... .......... .......... .......... 48% 6.27M 12s
130100K .......... .......... .......... .......... .......... 48% 132M 12s
130150K .......... .......... .......... .......... .......... 48% 4.45M 12s
130200K .......... .......... .......... .......... .......... 49% 76.3M 12s
130250K .......... .......... .......... .......... .......... 49% 90.8M 12s
130300K .......... .......... .......... .......... .......... 49% 2.50M 12s
130350K .......... .......... .......... .......... .......... 49% 93.9M 12s
130400K .......... .......... .......... .......... .......... 49% 243M 12s
130450K .......... .......... .......... .......... .......... 49% 2.97M 12s
130500K .......... .......... .......... .......... .......... 49% 121M 12s
130550K .......... .......... .......... .......... .......... 49% 61.3M 12s
130600K .......... .......... .......... .......... .......... 49% 2.68M 12s
130650K .......... .......... .......... .......... .......... 49% 192M 12s
130700K .......... .......... .......... .......... .......... 49% 171M 12s
130750K .......... .......... .......... .......... .......... 49% 3.22M 12s
130800K .......... .......... .......... .......... .......... 49% 94.1M 12s
130850K .......... .......... .......... .......... .......... 49% 131M 12s
130900K .......... .......... .......... .......... .......... 49% 2.20M 12s
130950K .......... .......... .......... .......... .......... 49% 109M 12s
131000K .......... .......... .......... .......... .......... 49% 52.1M 12s
131050K .......... .......... .......... .......... .......... 49% 2.74M 12s
131100K .......... .......... .......... .......... .......... 49% 81.4M 12s
131150K .......... .......... .......... .......... .......... 49% 159M 12s
131200K .......... .......... .......... .......... .......... 49% 2.56M 12s
131250K .......... .......... .......... .......... .......... 49% 138M 12s
131300K .......... .......... .......... .......... .......... 49% 189M 12s
131350K .......... .......... .......... .......... .......... 49% 3.85M 12s
131400K .......... .......... .......... .......... .......... 49% 205M 12s
131450K .......... .......... .......... .......... .......... 49% 136M 12s
131500K .......... .......... .......... .......... .......... 49% 2.74M 12s
131550K .......... .......... .......... .......... .......... 49% 176M 12s
131600K .......... .......... .......... .......... .......... 49% 52.2M 12s
131650K .......... .......... .......... .......... .......... 49% 4.10M 12s
131700K .......... .......... .......... .......... .......... 49% 28.5M 12s
131750K .......... .......... .......... .......... .......... 49% 195M 12s
131800K .......... .......... .......... .......... .......... 49% 173M 12s
131850K .......... .......... .......... .......... .......... 49% 2.69M 12s
131900K .......... .......... .......... .......... .......... 49% 150M 12s
131950K .......... .......... .......... .......... .......... 49% 160M 12s
132000K .......... .......... .......... .......... .......... 49% 2.73M 12s
132050K .......... .......... .......... .......... .......... 49% 172M 12s
132100K .......... .......... .......... .......... .......... 49% 827K 12s
132150K .......... .......... .......... .......... .......... 49% 2.35M 12s
132200K .......... .......... .......... .......... .......... 49% 127M 12s
132250K .......... .......... .......... .......... .......... 49% 114M 12s
132300K .......... .......... .......... .......... .......... 49% 2.17M 12s
132350K .......... .......... .......... .......... .......... 49% 82.2M 12s
132400K .......... .......... .......... .......... .......... 49% 153M 12s
132450K .......... .......... .......... .......... .......... 49% 2.16M 12s
132500K .......... .......... .......... .......... .......... 49% 118M 12s
132550K .......... .......... .......... .......... .......... 49% 104M 12s
132600K .......... .......... .......... .......... .......... 49% 2.23M 12s
132650K .......... .......... .......... .......... .......... 49% 102M 12s
132700K .......... .......... .......... .......... .......... 49% 126M 12s
132750K .......... .......... .......... .......... .......... 49% 32.4M 12s
132800K .......... .......... .......... .......... .......... 49% 2.45M 12s
132850K .......... .......... .......... .......... .......... 50% 111M 12s
132900K .......... .......... .......... .......... .......... 50% 189M 12s
132950K .......... .......... .......... .......... .......... 50% 3.84M 12s
133000K .......... .......... .......... .......... .......... 50% 129M 12s
133050K .......... .......... .......... .......... .......... 50% 145M 12s
133100K .......... .......... .......... .......... .......... 50% 2.18M 12s
133150K .......... .......... .......... .......... .......... 50% 193M 12s
133200K .......... .......... .......... .......... .......... 50% 95.6M 12s
133250K .......... .......... .......... .......... .......... 50% 3.23M 12s
133300K .......... .......... .......... .......... .......... 50% 92.3M 12s
133350K .......... .......... .......... .......... .......... 50% 176M 12s
133400K .......... .......... .......... .......... .......... 50% 166M 12s
133450K .......... .......... .......... .......... .......... 50% 3.68M 12s
133500K .......... .......... .......... .......... .......... 50% 156M 12s
133550K .......... .......... .......... .......... .......... 50% 115M 12s
133600K .......... .......... .......... .......... .......... 50% 2.37M 12s
133650K .......... .......... .......... .......... .......... 50% 202M 12s
133700K .......... .......... .......... .......... .......... 50% 178M 12s
133750K .......... .......... .......... .......... .......... 50% 3.36M 12s
133800K .......... .......... .......... .......... .......... 50% 103M 12s
133850K .......... .......... .......... .......... .......... 50% 94.1M 12s
133900K .......... .......... .......... .......... .......... 50% 110M 12s
133950K .......... .......... .......... .......... .......... 50% 2.76M 12s
134000K .......... .......... .......... .......... .......... 50% 181M 12s
134050K .......... .......... .......... .......... .......... 50% 47.2M 12s
134100K .......... .......... .......... .......... .......... 50% 3.45M 12s
134150K .......... .......... .......... .......... .......... 50% 51.6M 12s
134200K .......... .......... .......... .......... .......... 50% 110M 12s
134250K .......... .......... .......... .......... .......... 50% 2.17M 12s
134300K .......... .......... .......... .......... .......... 50% 152M 12s
134350K .......... .......... .......... .......... .......... 50% 166M 12s
134400K .......... .......... .......... .......... .......... 50% 193M 12s
134450K .......... .......... .......... .......... .......... 50% 2.52M 12s
134500K .......... .......... .......... .......... .......... 50% 47.5M 12s
134550K .......... .......... .......... .......... .......... 50% 142M 12s
134600K .......... .......... .......... .......... .......... 50% 5.72M 12s
134650K .......... .......... .......... .......... .......... 50% 154M 12s
134700K .......... .......... .......... .......... .......... 50% 3.06M 12s
134750K .......... .......... .......... .......... .......... 50% 110M 12s
134800K .......... .......... .......... .......... .......... 50% 82.8M 12s
134850K .......... .......... .......... .......... .......... 50% 3.10M 12s
134900K .......... .......... .......... .......... .......... 50% 113M 12s
134950K .......... .......... .......... .......... .......... 50% 109M 12s
135000K .......... .......... .......... .......... .......... 50% 2.18M 12s
135050K .......... .......... .......... .......... .......... 50% 96.5M 12s
135100K .......... .......... .......... .......... .......... 50% 137M 12s
135150K .......... .......... .......... .......... .......... 50% 5.36M 12s
135200K .......... .......... .......... .......... .......... 50% 53.2M 12s
135250K .......... .......... .......... .......... .......... 50% 80.0M 12s
135300K .......... .......... .......... .......... .......... 50% 120M 12s
135350K .......... .......... .......... .......... .......... 50% 7.68M 12s
135400K .......... .......... .......... .......... .......... 50% 173M 12s
135450K .......... .......... .......... .......... .......... 50% 6.62M 12s
135500K .......... .......... .......... .......... .......... 51% 5.56M 12s
135550K .......... .......... .......... .......... .......... 51% 117M 12s
135600K .......... .......... .......... .......... .......... 51% 6.68M 12s
135650K .......... .......... .......... .......... .......... 51% 167M 12s
135700K .......... .......... .......... .......... .......... 51% 168M 12s
135750K .......... .......... .......... .......... .......... 51% 3.16M 12s
135800K .......... .......... .......... .......... .......... 51% 195M 12s
135850K .......... .......... .......... .......... .......... 51% 3.13M 12s
135900K .......... .......... .......... .......... .......... 51% 81.9M 12s
135950K .......... .......... .......... .......... .......... 51% 2.87M 12s
136000K .......... .......... .......... .......... .......... 51% 91.6M 12s
136050K .......... .......... .......... .......... .......... 51% 140M 12s
136100K .......... .......... .......... .......... .......... 51% 2.03M 12s
136150K .......... .......... .......... .......... .......... 51% 42.9M 12s
136200K .......... .......... .......... .......... .......... 51% 2.79M 12s
136250K .......... .......... .......... .......... .......... 51% 76.5M 12s
136300K .......... .......... .......... .......... .......... 51% 132M 12s
136350K .......... .......... .......... .......... .......... 51% 2.46M 12s
136400K .......... .......... .......... .......... .......... 51% 82.6M 12s
136450K .......... .......... .......... .......... .......... 51% 2.30M 12s
136500K .......... .......... .......... .......... .......... 51% 83.5M 12s
136550K .......... .......... .......... .......... .......... 51% 98.6M 12s
136600K .......... .......... .......... .......... .......... 51% 2.82M 12s
136650K .......... .......... .......... .......... .......... 51% 133M 12s
136700K .......... .......... .......... .......... .......... 51% 2.92M 12s
136750K .......... .......... .......... .......... .......... 51% 117M 12s
136800K .......... .......... .......... .......... .......... 51% 131M 12s
136850K .......... .......... .......... .......... .......... 51% 2.81M 12s
136900K .......... .......... .......... .......... .......... 51% 132M 12s
136950K .......... .......... .......... .......... .......... 51% 90.3M 12s
137000K .......... .......... .......... .......... .......... 51% 7.37M 12s
137050K .......... .......... .......... .......... .......... 51% 89.6M 12s
137100K .......... .......... .......... .......... .......... 51% 6.90M 12s
137150K .......... .......... .......... .......... .......... 51% 148M 12s
137200K .......... .......... .......... .......... .......... 51% 55.7M 12s
137250K .......... .......... .......... .......... .......... 51% 8.53M 12s
137300K .......... .......... .......... .......... .......... 51% 85.5M 12s
137350K .......... .......... .......... .......... .......... 51% 8.99M 12s
137400K .......... .......... .......... .......... .......... 51% 176M 12s
137450K .......... .......... .......... .......... .......... 51% 80.0M 12s
137500K .......... .......... .......... .......... .......... 51% 9.42M 12s
137550K .......... .......... .......... .......... .......... 51% 172M 12s
137600K .......... .......... .......... .......... .......... 51% 152M 12s
137650K .......... .......... .......... .......... .......... 51% 6.68M 12s
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137750K .......... .......... .......... .......... .......... 51% 8.88M 12s
137800K .......... .......... .......... .......... .......... 51% 106M 12s
137850K .......... .......... .......... .......... .......... 51% 81.2M 12s
137900K .......... .......... .......... .......... .......... 51% 7.83M 12s
137950K .......... .......... .......... .......... .......... 51% 94.6M 12s
138000K .......... .......... .......... .......... .......... 51% 166M 12s
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138100K .......... .......... .......... .......... .......... 51% 155M 12s
138150K .......... .......... .......... .......... .......... 52% 9.07M 12s
138200K .......... .......... .......... .......... .......... 52% 332K 12s
138250K .......... .......... .......... .......... .......... 52% 87.0M 12s
138300K .......... .......... .......... .......... .......... 52% 92.7M 12s
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138450K .......... .......... .......... .......... .......... 52% 61.6M 12s
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138600K .......... .......... .......... .......... .......... 52% 2.20M 12s
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138750K .......... .......... .......... .......... .......... 52% 1.92M 12s
138800K .......... .......... .......... .......... .......... 52% 75.5M 12s
138850K .......... .......... .......... .......... .......... 52% 99.6M 12s
138900K .......... .......... .......... .......... .......... 52% 2.03M 12s
138950K .......... .......... .......... .......... .......... 52% 67.3M 12s
139000K .......... .......... .......... .......... .......... 52% 126M 12s
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139100K .......... .......... .......... .......... .......... 52% 148M 12s
139150K .......... .......... .......... .......... .......... 52% 161M 12s
139200K .......... .......... .......... .......... .......... 52% 1.38M 12s
139250K .......... .......... .......... .......... .......... 52% 46.0M 12s
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140000K .......... .......... .......... .......... .......... 52% 155M 12s
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140100K .......... .......... .......... .......... .......... 52% 76.5M 12s
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140600K .......... .......... .......... .......... .......... 52% 90.6M 12s
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140800K .......... .......... .......... .......... .......... 53% 1.80M 12s
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141000K .......... .......... .......... .......... .......... 53% 121M 12s
141050K .......... .......... .......... .......... .......... 53% 28.1M 12s
141100K .......... .......... .......... .......... .......... 53% 1.85M 12s
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141200K .......... .......... .......... .......... .......... 53% 90.1M 12s
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141500K .......... .......... .......... .......... .......... 53% 154M 12s
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141600K .......... .......... .......... .......... .......... 53% 71.7M 12s
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141700K .......... .......... .......... .......... .......... 53% 2.06M 12s
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141800K .......... .......... .......... .......... .......... 53% 3.73M 12s
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141900K .......... .......... .......... .......... .......... 53% 3.63M 12s
141950K .......... .......... .......... .......... .......... 53% 98.2M 12s
142000K .......... .......... .......... .......... .......... 53% 31.9M 12s
142050K .......... .......... .......... .......... .......... 53% 2.10M 12s
142100K .......... .......... .......... .......... .......... 53% 103M 12s
142150K .......... .......... .......... .......... .......... 53% 1.57M 12s
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142250K .......... .......... .......... .......... .......... 53% 1.33M 12s
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142400K .......... .......... .......... .......... .......... 53% 218M 12s
142450K .......... .......... .......... .......... .......... 53% 4.45M 12s
142500K .......... .......... .......... .......... .......... 53% 115M 12s
142550K .......... .......... .......... .......... .......... 53% 2.52M 12s
142600K .......... .......... .......... .......... .......... 53% 94.3M 12s
142650K .......... .......... .......... .......... .......... 53% 118M 12s
142700K .......... .......... .......... .......... .......... 53% 2.69M 12s
142750K .......... .......... .......... .......... .......... 53% 115M 12s
142800K .......... .......... .......... .......... .......... 53% 1.75M 12s
142850K .......... .......... .......... .......... .......... 53% 123M 12s
142900K .......... .......... .......... .......... .......... 53% 1.71M 12s
142950K .......... .......... .......... .......... .......... 53% 74.8M 12s
143000K .......... .......... .......... .......... .......... 53% 3.24M 12s
143050K .......... .......... .......... .......... .......... 53% 52.7M 12s
143100K .......... .......... .......... .......... .......... 53% 30.7M 12s
143150K .......... .......... .......... .......... .......... 53% 2.07M 12s
143200K .......... .......... .......... .......... .......... 53% 12.1M 12s
143250K .......... .......... .......... .......... .......... 53% 4.20M 12s
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143350K .......... .......... .......... .......... .......... 53% 3.28M 12s
143400K .......... .......... .......... .......... .......... 53% 88.6M 12s
143450K .......... .......... .......... .......... .......... 53% 3.20M 12s
143500K .......... .......... .......... .......... .......... 54% 375K 12s
143550K .......... .......... .......... .......... .......... 54% 62.0M 12s
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143850K .......... .......... .......... .......... .......... 54% 24.3M 12s
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144000K .......... .......... .......... .......... .......... 54% 106M 12s
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144100K .......... .......... .......... .......... .......... 54% 76.4M 12s
144150K .......... .......... .......... .......... .......... 54% 116M 12s
144200K .......... .......... .......... .......... .......... 54% 9.38M 12s
144250K .......... .......... .......... .......... .......... 54% 102M 12s
144300K .......... .......... .......... .......... .......... 54% 7.72M 12s
144350K .......... .......... .......... .......... .......... 54% 88.1M 12s
144400K .......... .......... .......... .......... .......... 54% 7.03M 12s
144450K .......... .......... .......... .......... .......... 54% 89.1M 12s
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144550K .......... .......... .......... .......... .......... 54% 7.34M 12s
144600K .......... .......... .......... .......... .......... 54% 96.5M 12s
144650K .......... .......... .......... .......... .......... 54% 7.31M 12s
144700K .......... .......... .......... .......... .......... 54% 59.7M 12s
144750K .......... .......... .......... .......... .......... 54% 84.5M 12s
144800K .......... .......... .......... .......... .......... 54% 2.14M 12s
144850K .......... .......... .......... .......... .......... 54% 73.0M 12s
144900K .......... .......... .......... .......... .......... 54% 3.59M 12s
144950K .......... .......... .......... .......... .......... 54% 93.9M 12s
145000K .......... .......... .......... .......... .......... 54% 92.7M 12s
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145100K .......... .......... .......... .......... .......... 54% 82.9M 12s
145150K .......... .......... .......... .......... .......... 54% 3.15M 12s
145200K .......... .......... .......... .......... .......... 54% 74.4M 12s
145250K .......... .......... .......... .......... .......... 54% 114M 12s
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145350K .......... .......... .......... .......... .......... 54% 49.8M 12s
145400K .......... .......... .......... .......... .......... 54% 3.25M 12s
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145700K .......... .......... .......... .......... .......... 54% 3.89M 12s
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145850K .......... .......... .......... .......... .......... 54% 94.4M 12s
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146850K .......... .......... .......... .......... .......... 55% 68.1M 12s
146900K .......... .......... .......... .......... .......... 55% 5.73M 12s
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147000K .......... .......... .......... .......... .......... 55% 4.02M 12s
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147100K .......... .......... .......... .......... .......... 55% 86.1M 12s
147150K .......... .......... .......... .......... .......... 55% 3.96M 12s
147200K .......... .......... .......... .......... .......... 55% 132M 12s
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147400K .......... .......... .......... .......... .......... 55% 51.1M 12s
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147500K .......... .......... .......... .......... .......... 55% 111M 12s
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147600K .......... .......... .......... .......... .......... 55% 5.32M 12s
147650K .......... .......... .......... .......... .......... 55% 119M 11s
147700K .......... .......... .......... .......... .......... 55% 4.60M 11s
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147850K .......... .......... .......... .......... .......... 55% 5.12M 11s
147900K .......... .......... .......... .......... .......... 55% 90.6M 11s
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148000K .......... .......... .......... .......... .......... 55% 5.10M 11s
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148100K .......... .......... .......... .......... .......... 55% 119M 11s
148150K .......... .......... .......... .......... .......... 55% 5.21M 11s
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148400K .......... .......... .......... .......... .......... 55% 99.6M 11s
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148600K .......... .......... .......... .......... .......... 55% 8.68M 11s
148650K .......... .......... .......... .......... .......... 55% 76.8M 11s
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148750K .......... .......... .......... .......... .......... 55% 2.45M 11s
148800K .......... .......... .......... .......... .......... 56% 216M 11s
148850K .......... .......... .......... .......... .......... 56% 108M 11s
148900K .......... .......... .......... .......... .......... 56% 5.10M 11s
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149000K .......... .......... .......... .......... .......... 56% 130M 11s
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149100K .......... .......... .......... .......... .......... 56% 127M 11s
149150K .......... .......... .......... .......... .......... 56% 140M 11s
149200K .......... .......... .......... .......... .......... 56% 113M 11s
149250K .......... .......... .......... .......... .......... 56% 58.6M 11s
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149500K .......... .......... .......... .......... .......... 56% 7.74M 11s
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149600K .......... .......... .......... .......... .......... 56% 97.9M 11s
149650K .......... .......... .......... .......... .......... 56% 4.04M 11s
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149750K .......... .......... .......... .......... .......... 56% 8.62M 11s
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150000K .......... .......... .......... .......... .......... 56% 65.9M 11s
150050K .......... .......... .......... .......... .......... 56% 4.06M 11s
150100K .......... .......... .......... .......... .......... 56% 88.3M 11s
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150200K .......... .......... .......... .......... .......... 56% 5.98M 11s
150250K .......... .......... .......... .......... .......... 56% 174M 11s
150300K .......... .......... .......... .......... .......... 56% 5.53M 11s
150350K .......... .......... .......... .......... .......... 56% 170M 11s
150400K .......... .......... .......... .......... .......... 56% 6.82M 11s
150450K .......... .......... .......... .......... .......... 56% 147M 11s
150500K .......... .......... .......... .......... .......... 56% 4.64M 11s
150550K .......... .......... .......... .......... .......... 56% 100M 11s
150600K .......... .......... .......... .......... .......... 56% 5.14M 11s
150650K .......... .......... .......... .......... .......... 56% 147M 11s
150700K .......... .......... .......... .......... .......... 56% 85.1M 11s
150750K .......... .......... .......... .......... .......... 56% 4.49M 11s
150800K .......... .......... .......... .......... .......... 56% 154M 11s
150850K .......... .......... .......... .......... .......... 56% 170M 11s
150900K .......... .......... .......... .......... .......... 56% 6.38M 11s
150950K .......... .......... .......... .......... .......... 56% 161M 11s
151000K .......... .......... .......... .......... .......... 56% 6.59M 11s
151050K .......... .......... .......... .......... .......... 56% 4.88M 11s
151100K .......... .......... .......... .......... .......... 56% 117M 11s
151150K .......... .......... .......... .......... .......... 56% 2.71M 11s
151200K .......... .......... .......... .......... .......... 56% 65.0M 11s
151250K .......... .......... .......... .......... .......... 56% 4.50M 11s
151300K .......... .......... .......... .......... .......... 56% 182M 11s
151350K .......... .......... .......... .......... .......... 56% 3.90M 11s
151400K .......... .......... .......... .......... .......... 56% 3.68M 11s
151450K .......... .......... .......... .......... .......... 57% 138M 11s
151500K .......... .......... .......... .......... .......... 57% 6.77M 11s
151550K .......... .......... .......... .......... .......... 57% 60.5M 11s
151600K .......... .......... .......... .......... .......... 57% 4.33M 11s
151650K .......... .......... .......... .......... .......... 57% 4.46M 11s
151700K .......... .......... .......... .......... .......... 57% 44.2M 11s
151750K .......... .......... .......... .......... .......... 57% 4.32M 11s
151800K .......... .......... .......... .......... .......... 57% 45.4M 11s
151850K .......... .......... .......... .......... .......... 57% 11.1M 11s
151900K .......... .......... .......... .......... .......... 57% 97.7M 11s
151950K .......... .......... .......... .......... .......... 57% 8.33M 11s
152000K .......... .......... .......... .......... .......... 57% 10.3M 11s
152050K .......... .......... .......... .......... .......... 57% 178M 11s
152100K .......... .......... .......... .......... .......... 57% 10.5M 11s
152150K .......... .......... .......... .......... .......... 57% 96.9M 11s
152200K .......... .......... .......... .......... .......... 57% 8.62M 11s
152250K .......... .......... .......... .......... .......... 57% 200M 11s
152300K .......... .......... .......... .......... .......... 57% 11.0M 11s
152350K .......... .......... .......... .......... .......... 57% 117M 11s
152400K .......... .......... .......... .......... .......... 57% 11.6M 11s
152450K .......... .......... .......... .......... .......... 57% 9.59M 11s
152500K .......... .......... .......... .......... .......... 57% 103M 11s
152550K .......... .......... .......... .......... .......... 57% 1.84M 11s
152600K .......... .......... .......... .......... .......... 57% 96.5M 11s
152650K .......... .......... .......... .......... .......... 57% 11.3M 11s
152700K .......... .......... .......... .......... .......... 57% 72.7M 11s
152750K .......... .......... .......... .......... .......... 57% 11.8M 11s
152800K .......... .......... .......... .......... .......... 57% 76.9M 11s
152850K .......... .......... .......... .......... .......... 57% 9.37M 11s
152900K .......... .......... .......... .......... .......... 57% 180M 11s
152950K .......... .......... .......... .......... .......... 57% 1.01M 11s
153000K .......... .......... .......... .......... .......... 57% 149M 11s
153050K .......... .......... .......... .......... .......... 57% 3.20M 11s
153100K .......... .......... .......... .......... .......... 57% 155M 11s
153150K .......... .......... .......... .......... .......... 57% 5.43M 11s
153200K .......... .......... .......... .......... .......... 57% 131M 11s
153250K .......... .......... .......... .......... .......... 57% 6.49M 11s
153300K .......... .......... .......... .......... .......... 57% 137M 11s
153350K .......... .......... .......... .......... .......... 57% 4.29M 11s
153400K .......... .......... .......... .......... .......... 57% 83.9M 11s
153450K .......... .......... .......... .......... .......... 57% 5.49M 11s
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153550K .......... .......... .......... .......... .......... 57% 5.18M 11s
153600K .......... .......... .......... .......... .......... 57% 133M 11s
153650K .......... .......... .......... .......... .......... 57% 6.20M 11s
153700K .......... .......... .......... .......... .......... 57% 178M 11s
153750K .......... .......... .......... .......... .......... 57% 4.96M 11s
153800K .......... .......... .......... .......... .......... 57% 169M 11s
153850K .......... .......... .......... .......... .......... 57% 5.40M 11s
153900K .......... .......... .......... .......... .......... 57% 216M 11s
153950K .......... .......... .......... .......... .......... 57% 5.78M 11s
154000K .......... .......... .......... .......... .......... 57% 180M 11s
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154100K .......... .......... .......... .......... .......... 58% 184M 11s
154150K .......... .......... .......... .......... .......... 58% 6.32M 11s
154200K .......... .......... .......... .......... .......... 58% 147M 11s
154250K .......... .......... .......... .......... .......... 58% 6.40M 11s
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154350K .......... .......... .......... .......... .......... 58% 6.16M 11s
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154600K .......... .......... .......... .......... .......... 58% 5.29M 11s
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154700K .......... .......... .......... .......... .......... 58% 6.93M 11s
154750K .......... .......... .......... .......... .......... 58% 94.4M 11s
154800K .......... .......... .......... .......... .......... 58% 6.35M 11s
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154900K .......... .......... .......... .......... .......... 58% 10.9M 11s
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155100K .......... .......... .......... .......... .......... 58% 156M 11s
155150K .......... .......... .......... .......... .......... 58% 6.58M 11s
155200K .......... .......... .......... .......... .......... 58% 27.2M 11s
155250K .......... .......... .......... .......... .......... 58% 5.20M 11s
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155500K .......... .......... .......... .......... .......... 58% 7.06M 11s
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155600K .......... .......... .......... .......... .......... 58% 10.1M 11s
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155900K .......... .......... .......... .......... .......... 58% 74.9M 11s
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156100K .......... .......... .......... .......... .......... 58% 136M 11s
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156500K .......... .......... .......... .......... .......... 58% 95.7M 11s
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156900K .......... .......... .......... .......... .......... 59% 5.47M 11s
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157100K .......... .......... .......... .......... .......... 59% 63.2M 11s
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157500K .......... .......... .......... .......... .......... 59% 97.9M 11s
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157700K .......... .......... .......... .......... .......... 59% 136M 10s
157750K .......... .......... .......... .......... .......... 59% 96.7M 10s
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166500K .......... .......... .......... .......... .......... 62% 3.11M 10s
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181100K .......... .......... .......... .......... .......... 68% 4.20M 8s
181150K .......... .......... .......... .......... .......... 68% 150M 8s
181200K .......... .......... .......... .......... .......... 68% 92.3M 8s
181250K .......... .......... .......... .......... .......... 68% 4.50M 8s
181300K .......... .......... .......... .......... .......... 68% 63.9M 8s
181350K .......... .......... .......... .......... .......... 68% 92.3M 8s
181400K .......... .......... .......... .......... .......... 68% 4.55M 8s
181450K .......... .......... .......... .......... .......... 68% 166M 8s
181500K .......... .......... .......... .......... .......... 68% 184M 8s
181550K .......... .......... .......... .......... .......... 68% 6.28M 8s
181600K .......... .......... .......... .......... .......... 68% 102M 8s
181650K .......... .......... .......... .......... .......... 68% 116M 8s
181700K .......... .......... .......... .......... .......... 68% 7.41M 8s
181750K .......... .......... .......... .......... .......... 68% 71.2M 8s
181800K .......... .......... .......... .......... .......... 68% 117M 8s
181850K .......... .......... .......... .......... .......... 68% 8.56M 8s
181900K .......... .......... .......... .......... .......... 68% 253M 8s
181950K .......... .......... .......... .......... .......... 68% 277M 8s
182000K .......... .......... .......... .......... .......... 68% 9.75M 8s
182050K .......... .......... .......... .......... .......... 68% 123M 8s
182100K .......... .......... .......... .......... .......... 68% 118M 8s
182150K .......... .......... .......... .......... .......... 68% 6.85M 8s
182200K .......... .......... .......... .......... .......... 68% 88.5M 8s
182250K .......... .......... .......... .......... .......... 68% 107M 8s
182300K .......... .......... .......... .......... .......... 68% 7.82M 8s
182350K .......... .......... .......... .......... .......... 68% 140M 8s
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182450K .......... .......... .......... .......... .......... 68% 8.70M 8s
182500K .......... .......... .......... .......... .......... 68% 125M 8s
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182600K .......... .......... .......... .......... .......... 68% 6.13M 8s
182650K .......... .......... .......... .......... .......... 68% 122M 8s
182700K .......... .......... .......... .......... .......... 68% 8.44M 8s
182750K .......... .......... .......... .......... .......... 68% 100M 8s
182800K .......... .......... .......... .......... .......... 68% 146M 8s
182850K .......... .......... .......... .......... .......... 68% 5.04M 8s
182900K .......... .......... .......... .......... .......... 68% 111M 8s
182950K .......... .......... .......... .......... .......... 68% 67.2M 8s
183000K .......... .......... .......... .......... .......... 68% 103M 8s
183050K .......... .......... .......... .......... .......... 68% 7.65M 8s
183100K .......... .......... .......... .......... .......... 68% 173M 8s
183150K .......... .......... .......... .......... .......... 68% 238M 8s
183200K .......... .......... .......... .......... .......... 68% 7.10M 8s
183250K .......... .......... .......... .......... .......... 68% 108M 8s
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183350K .......... .......... .......... .......... .......... 69% 7.21M 8s
183400K .......... .......... .......... .......... .......... 69% 98.2M 8s
183450K .......... .......... .......... .......... .......... 69% 161M 8s
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183550K .......... .......... .......... .......... .......... 69% 86.6M 8s
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183650K .......... .......... .......... .......... .......... 69% 7.84M 8s
183700K .......... .......... .......... .......... .......... 69% 124M 8s
183750K .......... .......... .......... .......... .......... 69% 89.1M 8s
183800K .......... .......... .......... .......... .......... 69% 7.56M 8s
183850K .......... .......... .......... .......... .......... 69% 130M 8s
183900K .......... .......... .......... .......... .......... 69% 81.2M 8s
183950K .......... .......... .......... .......... .......... 69% 8.35M 8s
184000K .......... .......... .......... .......... .......... 69% 117M 8s
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184100K .......... .......... .......... .......... .......... 69% 8.09M 8s
184150K .......... .......... .......... .......... .......... 69% 134M 8s
184200K .......... .......... .......... .......... .......... 69% 98.4M 8s
184250K .......... .......... .......... .......... .......... 69% 7.44M 8s
184300K .......... .......... .......... .......... .......... 69% 90.6M 8s
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184400K .......... .......... .......... .......... .......... 69% 9.14M 8s
184450K .......... .......... .......... .......... .......... 69% 61.5M 8s
184500K .......... .......... .......... .......... .......... 69% 81.5M 8s
184550K .......... .......... .......... .......... .......... 69% 167M 8s
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184650K .......... .......... .......... .......... .......... 69% 96.7M 8s
184700K .......... .......... .......... .......... .......... 69% 85.8M 8s
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184800K .......... .......... .......... .......... .......... 69% 126M 8s
184850K .......... .......... .......... .......... .......... 69% 98.2M 8s
184900K .......... .......... .......... .......... .......... 69% 7.55M 8s
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185000K .......... .......... .......... .......... .......... 69% 129M 8s
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185100K .......... .......... .......... .......... .......... 69% 152M 8s
185150K .......... .......... .......... .......... .......... 69% 182M 8s
185200K .......... .......... .......... .......... .......... 69% 5.23M 8s
185250K .......... .......... .......... .......... .......... 69% 155M 8s
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185400K .......... .......... .......... .......... .......... 69% 6.61M 8s
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185500K .......... .......... .......... .......... .......... 69% 74.9M 8s
185550K .......... .......... .......... .......... .......... 69% 7.49M 8s
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185650K .......... .......... .......... .......... .......... 69% 192M 8s
185700K .......... .......... .......... .......... .......... 69% 5.77M 8s
185750K .......... .......... .......... .......... .......... 69% 40.0M 8s
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185900K .......... .......... .......... .......... .......... 69% 5.88M 8s
185950K .......... .......... .......... .......... .......... 69% 161M 8s
186000K .......... .......... .......... .......... .......... 70% 174M 8s
186050K .......... .......... .......... .......... .......... 70% 4.12M 8s
186100K .......... .......... .......... .......... .......... 70% 127M 8s
186150K .......... .......... .......... .......... .......... 70% 122M 8s
186200K .......... .......... .......... .......... .......... 70% 147M 8s
186250K .......... .......... .......... .......... .......... 70% 5.62M 8s
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186400K .......... .......... .......... .......... .......... 70% 7.06M 8s
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186650K .......... .......... .......... .......... .......... 70% 96.7M 8s
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186900K .......... .......... .......... .......... .......... 70% 8.07M 8s
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187000K .......... .......... .......... .......... .......... 70% 202M 8s
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187100K .......... .......... .......... .......... .......... 70% 3.42M 8s
187150K .......... .......... .......... .......... .......... 70% 149M 8s
187200K .......... .......... .......... .......... .......... 70% 96.7M 8s
187250K .......... .......... .......... .......... .......... 70% 5.98M 8s
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188000K .......... .......... .......... .......... .......... 70% 175M 7s
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188150K .......... .......... .......... .......... .......... 70% 6.98M 7s
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188250K .......... .......... .......... .......... .......... 70% 71.7M 7s
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188650K .......... .......... .......... .......... .......... 71% 8.45M 7s
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188850K .......... .......... .......... .......... .......... 71% 7.45M 7s
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189000K .......... .......... .......... .......... .......... 71% 7.70M 7s
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189100K .......... .......... .......... .......... .......... 71% 70.8M 7s
189150K .......... .......... .......... .......... .......... 71% 117M 7s
189200K .......... .......... .......... .......... .......... 71% 7.93M 7s
189250K .......... .......... .......... .......... .......... 71% 157M 7s
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189950K .......... .......... .......... .......... .......... 71% 69.4M 7s
190000K .......... .......... .......... .......... .......... 71% 29.2M 7s
190050K .......... .......... .......... .......... .......... 71% 54.1M 7s
190100K .......... .......... .......... .......... .......... 71% 7.35M 7s
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190250K .......... .......... .......... .......... .......... 71% 78.1M 7s
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191000K .......... .......... .......... .......... .......... 71% 8.11M 7s
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191100K .......... .......... .......... .......... .......... 71% 128M 7s
191150K .......... .......... .......... .......... .......... 71% 32.4M 7s
191200K .......... .......... .......... .......... .......... 71% 6.59M 7s
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191450K .......... .......... .......... .......... .......... 72% 55.6M 7s
191500K .......... .......... .......... .......... .......... 72% 141M 7s
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191600K .......... .......... .......... .......... .......... 72% 7.64M 7s
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191850K .......... .......... .......... .......... .......... 72% 81.7M 7s
191900K .......... .......... .......... .......... .......... 72% 95.0M 7s
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192000K .......... .......... .......... .......... .......... 72% 129M 7s
192050K .......... .......... .......... .......... .......... 72% 128M 7s
192100K .......... .......... .......... .......... .......... 72% 84.2M 7s
192150K .......... .......... .......... .......... .......... 72% 7.28M 7s
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192250K .......... .......... .......... .......... .......... 72% 167M 7s
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192500K .......... .......... .......... .......... .......... 72% 238M 7s
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192800K .......... .......... .......... .......... .......... 72% 105M 7s
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194200K .......... .......... .......... .......... .......... 73% 185M 7s
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195150K .......... .......... .......... .......... .......... 73% 89.4M 7s
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195850K .......... .......... .......... .......... .......... 73% 116M 7s
195900K .......... .......... .......... .......... .......... 73% 207M 7s
195950K .......... .......... .......... .......... .......... 73% 6.47M 7s
196000K .......... .......... .......... .......... .......... 73% 120M 7s
196050K .......... .......... .......... .......... .......... 73% 157M 7s
196100K .......... .......... .......... .......... .......... 73% 108M 7s
196150K .......... .......... .......... .......... .......... 73% 5.59M 7s
196200K .......... .......... .......... .......... .......... 73% 96.7M 7s
196250K .......... .......... .......... .......... .......... 73% 111M 7s
196300K .......... .......... .......... .......... .......... 73% 97.7M 7s
196350K .......... .......... .......... .......... .......... 73% 6.13M 7s
196400K .......... .......... .......... .......... .......... 73% 252M 7s
196450K .......... .......... .......... .......... .......... 73% 224M 7s
196500K .......... .......... .......... .......... .......... 73% 276M 7s
196550K .......... .......... .......... .......... .......... 73% 8.47M 7s
196600K .......... .......... .......... .......... .......... 73% 73.5M 7s
196650K .......... .......... .......... .......... .......... 74% 95.9M 7s
196700K .......... .......... .......... .......... .......... 74% 115M 6s
196750K .......... .......... .......... .......... .......... 74% 8.18M 6s
196800K .......... .......... .......... .......... .......... 74% 155M 6s
196850K .......... .......... .......... .......... .......... 74% 182M 6s
196900K .......... .......... .......... .......... .......... 74% 160M 6s
196950K .......... .......... .......... .......... .......... 74% 115M 6s
197000K .......... .......... .......... .......... .......... 74% 8.14M 6s
197050K .......... .......... .......... .......... .......... 74% 98.8M 6s
197100K .......... .......... .......... .......... .......... 74% 110M 6s
197150K .......... .......... .......... .......... .......... 74% 141M 6s
197200K .......... .......... .......... .......... .......... 74% 7.72M 6s
197250K .......... .......... .......... .......... .......... 74% 118M 6s
197300K .......... .......... .......... .......... .......... 74% 182M 6s
197350K .......... .......... .......... .......... .......... 74% 148M 6s
197400K .......... .......... .......... .......... .......... 74% 7.13M 6s
197450K .......... .......... .......... .......... .......... 74% 145M 6s
197500K .......... .......... .......... .......... .......... 74% 96.3M 6s
197550K .......... .......... .......... .......... .......... 74% 126M 6s
197600K .......... .......... .......... .......... .......... 74% 24.1M 6s
197650K .......... .......... .......... .......... .......... 74% 143M 6s
197700K .......... .......... .......... .......... .......... 74% 7.88M 6s
197750K .......... .......... .......... .......... .......... 74% 145M 6s
197800K .......... .......... .......... .......... .......... 74% 94.4M 6s
197850K .......... .......... .......... .......... .......... 74% 9.77M 6s
197900K .......... .......... .......... .......... .......... 74% 98.0M 6s
197950K .......... .......... .......... .......... .......... 74% 139M 6s
198000K .......... .......... .......... .......... .......... 74% 9.48M 6s
198050K .......... .......... .......... .......... .......... 74% 174M 6s
198100K .......... .......... .......... .......... .......... 74% 236M 6s
198150K .......... .......... .......... .......... .......... 74% 12.5M 6s
198200K .......... .......... .......... .......... .......... 74% 210M 6s
198250K .......... .......... .......... .......... .......... 74% 95.7M 6s
198300K .......... .......... .......... .......... .......... 74% 132M 6s
198350K .......... .......... .......... .......... .......... 74% 9.03M 6s
198400K .......... .......... .......... .......... .......... 74% 85.2M 6s
198450K .......... .......... .......... .......... .......... 74% 8.21M 6s
198500K .......... .......... .......... .......... .......... 74% 187M 6s
198550K .......... .......... .......... .......... .......... 74% 96.7M 6s
198600K .......... .......... .......... .......... .......... 74% 155M 6s
198650K .......... .......... .......... .......... .......... 74% 11.4M 6s
198700K .......... .......... .......... .......... .......... 74% 92.8M 6s
198750K .......... .......... .......... .......... .......... 74% 131M 6s
198800K .......... .......... .......... .......... .......... 74% 8.94M 6s
198850K .......... .......... .......... .......... .......... 74% 145M 6s
198900K .......... .......... .......... .......... .......... 74% 162M 6s
198950K .......... .......... .......... .......... .......... 74% 10.8M 6s
199000K .......... .......... .......... .......... .......... 74% 154M 6s
199050K .......... .......... .......... .......... .......... 74% 59.1M 6s
199100K .......... .......... .......... .......... .......... 74% 11.4M 6s
199150K .......... .......... .......... .......... .......... 74% 108M 6s
199200K .......... .......... .......... .......... .......... 74% 78.9M 6s
199250K .......... .......... .......... .......... .......... 74% 8.23M 6s
199300K .......... .......... .......... .......... .......... 75% 171M 6s
199350K .......... .......... .......... .......... .......... 75% 172M 6s
199400K .......... .......... .......... .......... .......... 75% 11.7M 6s
199450K .......... .......... .......... .......... .......... 75% 130M 6s
199500K .......... .......... .......... .......... .......... 75% 173M 6s
199550K .......... .......... .......... .......... .......... 75% 27.7M 6s
199600K .......... .......... .......... .......... .......... 75% 19.8M 6s
199650K .......... .......... .......... .......... .......... 75% 156M 6s
199700K .......... .......... .......... .......... .......... 75% 24.0M 6s
199750K .......... .......... .......... .......... .......... 75% 8.86M 6s
199800K .......... .......... .......... .......... .......... 75% 154M 6s
199850K .......... .......... .......... .......... .......... 75% 109M 6s
199900K .......... .......... .......... .......... .......... 75% 4.97M 6s
199950K .......... .......... .......... .......... .......... 75% 168M 6s
200000K .......... .......... .......... .......... .......... 75% 168M 6s
200050K .......... .......... .......... .......... .......... 75% 7.91M 6s
200100K .......... .......... .......... .......... .......... 75% 68.8M 6s
200150K .......... .......... .......... .......... .......... 75% 116M 6s
200200K .......... .......... .......... .......... .......... 75% 7.82M 6s
200250K .......... .......... .......... .......... .......... 75% 130M 6s
200300K .......... .......... .......... .......... .......... 75% 203M 6s
200350K .......... .......... .......... .......... .......... 75% 126M 6s
200400K .......... .......... .......... .......... .......... 75% 7.42M 6s
200450K .......... .......... .......... .......... .......... 75% 69.1M 6s
200500K .......... .......... .......... .......... .......... 75% 103M 6s
200550K .......... .......... .......... .......... .......... 75% 6.31M 6s
200600K .......... .......... .......... .......... .......... 75% 152M 6s
200650K .......... .......... .......... .......... .......... 75% 201M 6s
200700K .......... .......... .......... .......... .......... 75% 7.60M 6s
200750K .......... .......... .......... .......... .......... 75% 139M 6s
200800K .......... .......... .......... .......... .......... 75% 128M 6s
200850K .......... .......... .......... .......... .......... 75% 6.55M 6s
200900K .......... .......... .......... .......... .......... 75% 89.9M 6s
200950K .......... .......... .......... .......... .......... 75% 129M 6s
201000K .......... .......... .......... .......... .......... 75% 7.64M 6s
201050K .......... .......... .......... .......... .......... 75% 82.8M 6s
201100K .......... .......... .......... .......... .......... 75% 90.1M 6s
201150K .......... .......... .......... .......... .......... 75% 169M 6s
201200K .......... .......... .......... .......... .......... 75% 6.27M 6s
201250K .......... .......... .......... .......... .......... 75% 114M 6s
201300K .......... .......... .......... .......... .......... 75% 91.6M 6s
201350K .......... .......... .......... .......... .......... 75% 7.41M 6s
201400K .......... .......... .......... .......... .......... 75% 137M 6s
201450K .......... .......... .......... .......... .......... 75% 154M 6s
201500K .......... .......... .......... .......... .......... 75% 8.61M 6s
201550K .......... .......... .......... .......... .......... 75% 156M 6s
201600K .......... .......... .......... .......... .......... 75% 155M 6s
201650K .......... .......... .......... .......... .......... 75% 214M 6s
201700K .......... .......... .......... .......... .......... 75% 8.28M 6s
201750K .......... .......... .......... .......... .......... 75% 93.2M 6s
201800K .......... .......... .......... .......... .......... 75% 142M 6s
201850K .......... .......... .......... .......... .......... 75% 7.46M 6s
201900K .......... .......... .......... .......... .......... 75% 121M 6s
201950K .......... .......... .......... .......... .......... 76% 84.9M 6s
202000K .......... .......... .......... .......... .......... 76% 8.14M 6s
202050K .......... .......... .......... .......... .......... 76% 194M 6s
202100K .......... .......... .......... .......... .......... 76% 102M 6s
202150K .......... .......... .......... .......... .......... 76% 168M 6s
202200K .......... .......... .......... .......... .......... 76% 7.93M 6s
202250K .......... .......... .......... .......... .......... 76% 103M 6s
202300K .......... .......... .......... .......... .......... 76% 174M 6s
202350K .......... .......... .......... .......... .......... 76% 8.21M 6s
202400K .......... .......... .......... .......... .......... 76% 144M 6s
202450K .......... .......... .......... .......... .......... 76% 102M 6s
202500K .......... .......... .......... .......... .......... 76% 7.94M 6s
202550K .......... .......... .......... .......... .......... 76% 81.0M 6s
202600K .......... .......... .......... .......... .......... 76% 112M 6s
202650K .......... .......... .......... .......... .......... 76% 160M 6s
202700K .......... .......... .......... .......... .......... 76% 7.69M 6s
202750K .......... .......... .......... .......... .......... 76% 100M 6s
202800K .......... .......... .......... .......... .......... 76% 121M 6s
202850K .......... .......... .......... .......... .......... 76% 8.54M 6s
202900K .......... .......... .......... .......... .......... 76% 12.0M 6s
202950K .......... .......... .......... .......... .......... 76% 79.5M 6s
203000K .......... .......... .......... .......... .......... 76% 176M 6s
203050K .......... .......... .......... .......... .......... 76% 173M 6s
203100K .......... .......... .......... .......... .......... 76% 972K 6s
203150K .......... .......... .......... .......... .......... 76% 143M 6s
203200K .......... .......... .......... .......... .......... 76% 110M 6s
203250K .......... .......... .......... .......... .......... 76% 146M 6s
203300K .......... .......... .......... .......... .......... 76% 213M 6s
203350K .......... .......... .......... .......... .......... 76% 94.8M 6s
203400K .......... .......... .......... .......... .......... 76% 147M 6s
203450K .......... .......... .......... .......... .......... 76% 8.93M 6s
203500K .......... .......... .......... .......... .......... 76% 95.6M 6s
203550K .......... .......... .......... .......... .......... 76% 9.83M 6s
203600K .......... .......... .......... .......... .......... 76% 74.3M 6s
203650K .......... .......... .......... .......... .......... 76% 130M 6s
203700K .......... .......... .......... .......... .......... 76% 7.84M 6s
203750K .......... .......... .......... .......... .......... 76% 87.0M 6s
203800K .......... .......... .......... .......... .......... 76% 8.91M 6s
203850K .......... .......... .......... .......... .......... 76% 138M 6s
203900K .......... .......... .......... .......... .......... 76% 126M 6s
203950K .......... .......... .......... .......... .......... 76% 9.33M 6s
204000K .......... .......... .......... .......... .......... 76% 106M 6s
204050K .......... .......... .......... .......... .......... 76% 10.3M 6s
204100K .......... .......... .......... .......... .......... 76% 127M 6s
204150K .......... .......... .......... .......... .......... 76% 7.76M 6s
204200K .......... .......... .......... .......... .......... 76% 81.5M 6s
204250K .......... .......... .......... .......... .......... 76% 107M 6s
204300K .......... .......... .......... .......... .......... 76% 9.63M 6s
204350K .......... .......... .......... .......... .......... 76% 86.4M 6s
204400K .......... .......... .......... .......... .......... 76% 7.49M 6s
204450K .......... .......... .......... .......... .......... 76% 118M 6s
204500K .......... .......... .......... .......... .......... 76% 163M 6s
204550K .......... .......... .......... .......... .......... 76% 8.62M 6s
204600K .......... .......... .......... .......... .......... 77% 63.1M 6s
204650K .......... .......... .......... .......... .......... 77% 31.9M 6s
204700K .......... .......... .......... .......... .......... 77% 12.1M 6s
204750K .......... .......... .......... .......... .......... 77% 118M 6s
204800K .......... .......... .......... .......... .......... 77% 8.61M 6s
204850K .......... .......... .......... .......... .......... 77% 174M 6s
204900K .......... .......... .......... .......... .......... 77% 170M 6s
204950K .......... .......... .......... .......... .......... 77% 8.41M 6s
205000K .......... .......... .......... .......... .......... 77% 131M 6s
205050K .......... .......... .......... .......... .......... 77% 8.72M 6s
205100K .......... .......... .......... .......... .......... 77% 92.5M 6s
205150K .......... .......... .......... .......... .......... 77% 119M 6s
205200K .......... .......... .......... .......... .......... 77% 8.88M 6s
205250K .......... .......... .......... .......... .......... 77% 128M 6s
205300K .......... .......... .......... .......... .......... 77% 1.80M 6s
205350K .......... .......... .......... .......... .......... 77% 120M 6s
205400K .......... .......... .......... .......... .......... 77% 145M 6s
205450K .......... .......... .......... .......... .......... 77% 6.99M 6s
205500K .......... .......... .......... .......... .......... 77% 105M 6s
205550K .......... .......... .......... .......... .......... 77% 143M 6s
205600K .......... .......... .......... .......... .......... 77% 8.30M 6s
205650K .......... .......... .......... .......... .......... 77% 84.9M 6s
205700K .......... .......... .......... .......... .......... 77% 6.09M 6s
205750K .......... .......... .......... .......... .......... 77% 169M 6s
205800K .......... .......... .......... .......... .......... 77% 83.5M 6s
205850K .......... .......... .......... .......... .......... 77% 5.83M 6s
205900K .......... .......... .......... .......... .......... 77% 188M 6s
205950K .......... .......... .......... .......... .......... 77% 160M 6s
206000K .......... .......... .......... .......... .......... 77% 7.86M 6s
206050K .......... .......... .......... .......... .......... 77% 95.7M 5s
206100K .......... .......... .......... .......... .......... 77% 9.02M 5s
206150K .......... .......... .......... .......... .......... 77% 171M 5s
206200K .......... .......... .......... .......... .......... 77% 101M 5s
206250K .......... .......... .......... .......... .......... 77% 7.96M 5s
206300K .......... .......... .......... .......... .......... 77% 124M 5s
206350K .......... .......... .......... .......... .......... 77% 108M 5s
206400K .......... .......... .......... .......... .......... 77% 8.83M 5s
206450K .......... .......... .......... .......... .......... 77% 179M 5s
206500K .......... .......... .......... .......... .......... 77% 111M 5s
206550K .......... .......... .......... .......... .......... 77% 9.03M 5s
206600K .......... .......... .......... .......... .......... 77% 160M 5s
206650K .......... .......... .......... .......... .......... 77% 8.03M 5s
206700K .......... .......... .......... .......... .......... 77% 88.5M 5s
206750K .......... .......... .......... .......... .......... 77% 68.6M 5s
206800K .......... .......... .......... .......... .......... 77% 8.06M 5s
206850K .......... .......... .......... .......... .......... 77% 106M 5s
206900K .......... .......... .......... .......... .......... 77% 129M 5s
206950K .......... .......... .......... .......... .......... 77% 8.96M 5s
207000K .......... .......... .......... .......... .......... 77% 188M 5s
207050K .......... .......... .......... .......... .......... 77% 153M 5s
207100K .......... .......... .......... .......... .......... 77% 8.65M 5s
207150K .......... .......... .......... .......... .......... 77% 176M 5s
207200K .......... .......... .......... .......... .......... 77% 6.00M 5s
207250K .......... .......... .......... .......... .......... 78% 156M 5s
207300K .......... .......... .......... .......... .......... 78% 88.0M 5s
207350K .......... .......... .......... .......... .......... 78% 7.07M 5s
207400K .......... .......... .......... .......... .......... 78% 123M 5s
207450K .......... .......... .......... .......... .......... 78% 99.6M 5s
207500K .......... .......... .......... .......... .......... 78% 7.86M 5s
207550K .......... .......... .......... .......... .......... 78% 105M 5s
207600K .......... .......... .......... .......... .......... 78% 145M 5s
207650K .......... .......... .......... .......... .......... 78% 7.56M 5s
207700K .......... .......... .......... .......... .......... 78% 138M 5s
207750K .......... .......... .......... .......... .......... 78% 127M 5s
207800K .......... .......... .......... .......... .......... 78% 8.21M 5s
207850K .......... .......... .......... .......... .......... 78% 121M 5s
207900K .......... .......... .......... .......... .......... 78% 65.7M 5s
207950K .......... .......... .......... .......... .......... 78% 7.80M 5s
208000K .......... .......... .......... .......... .......... 78% 125M 5s
208050K .......... .......... .......... .......... .......... 78% 151M 5s
208100K .......... .......... .......... .......... .......... 78% 2.51M 5s
208150K .......... .......... .......... .......... .......... 78% 127M 5s
208200K .......... .......... .......... .......... .......... 78% 7.85M 5s
208250K .......... .......... .......... .......... .......... 78% 65.7M 5s
208300K .......... .......... .......... .......... .......... 78% 92.8M 5s
208350K .......... .......... .......... .......... .......... 78% 9.09M 5s
208400K .......... .......... .......... .......... .......... 78% 134M 5s
208450K .......... .......... .......... .......... .......... 78% 133M 5s
208500K .......... .......... .......... .......... .......... 78% 9.25M 5s
208550K .......... .......... .......... .......... .......... 78% 62.4M 5s
208600K .......... .......... .......... .......... .......... 78% 105M 5s
208650K .......... .......... .......... .......... .......... 78% 9.04M 5s
208700K .......... .......... .......... .......... .......... 78% 85.4M 5s
208750K .......... .......... .......... .......... .......... 78% 103M 5s
208800K .......... .......... .......... .......... .......... 78% 8.43M 5s
208850K .......... .......... .......... .......... .......... 78% 95.4M 5s
208900K .......... .......... .......... .......... .......... 78% 116M 5s
208950K .......... .......... .......... .......... .......... 78% 8.94M 5s
209000K .......... .......... .......... .......... .......... 78% 178M 5s
209050K .......... .......... .......... .......... .......... 78% 187M 5s
209100K .......... .......... .......... .......... .......... 78% 8.62M 5s
209150K .......... .......... .......... .......... .......... 78% 153M 5s
209200K .......... .......... .......... .......... .......... 78% 131M 5s
209250K .......... .......... .......... .......... .......... 78% 8.65M 5s
209300K .......... .......... .......... .......... .......... 78% 78.9M 5s
209350K .......... .......... .......... .......... .......... 78% 107M 5s
209400K .......... .......... .......... .......... .......... 78% 8.18M 5s
209450K .......... .......... .......... .......... .......... 78% 155M 5s
209500K .......... .......... .......... .......... .......... 78% 96.5M 5s
209550K .......... .......... .......... .......... .......... 78% 7.86M 5s
209600K .......... .......... .......... .......... .......... 78% 143M 5s
209650K .......... .......... .......... .......... .......... 78% 144M 5s
209700K .......... .......... .......... .......... .......... 78% 8.23M 5s
209750K .......... .......... .......... .......... .......... 78% 103M 5s
209800K .......... .......... .......... .......... .......... 78% 96.3M 5s
209850K .......... .......... .......... .......... .......... 78% 7.98M 5s
209900K .......... .......... .......... .......... .......... 79% 67.8M 5s
209950K .......... .......... .......... .......... .......... 79% 101M 5s
210000K .......... .......... .......... .......... .......... 79% 148M 5s
210050K .......... .......... .......... .......... .......... 79% 7.95M 5s
210100K .......... .......... .......... .......... .......... 79% 99.0M 5s
210150K .......... .......... .......... .......... .......... 79% 123M 5s
210200K .......... .......... .......... .......... .......... 79% 8.07M 5s
210250K .......... .......... .......... .......... .......... 79% 189M 5s
210300K .......... .......... .......... .......... .......... 79% 98.6M 5s
210350K .......... .......... .......... .......... .......... 79% 7.22M 5s
210400K .......... .......... .......... .......... .......... 79% 206M 5s
210450K .......... .......... .......... .......... .......... 79% 150M 5s
210500K .......... .......... .......... .......... .......... 79% 7.47M 5s
210550K .......... .......... .......... .......... .......... 79% 145M 5s
210600K .......... .......... .......... .......... .......... 79% 91.3M 5s
210650K .......... .......... .......... .......... .......... 79% 7.31M 5s
210700K .......... .......... .......... .......... .......... 79% 96.3M 5s
210750K .......... .......... .......... .......... .......... 79% 95.7M 5s
210800K .......... .......... .......... .......... .......... 79% 7.25M 5s
210850K .......... .......... .......... .......... .......... 79% 146M 5s
210900K .......... .......... .......... .......... .......... 79% 140M 5s
210950K .......... .......... .......... .......... .......... 79% 8.23M 5s
211000K .......... .......... .......... .......... .......... 79% 110M 5s
211050K .......... .......... .......... .......... .......... 79% 137M 5s
211100K .......... .......... .......... .......... .......... 79% 88.6M 5s
211150K .......... .......... .......... .......... .......... 79% 7.89M 5s
211200K .......... .......... .......... .......... .......... 79% 94.1M 5s
211250K .......... .......... .......... .......... .......... 79% 143M 5s
211300K .......... .......... .......... .......... .......... 79% 7.99M 5s
211350K .......... .......... .......... .......... .......... 79% 114M 5s
211400K .......... .......... .......... .......... .......... 79% 96.9M 5s
211450K .......... .......... .......... .......... .......... 79% 7.65M 5s
211500K .......... .......... .......... .......... .......... 79% 151M 5s
211550K .......... .......... .......... .......... .......... 79% 77.0M 5s
211600K .......... .......... .......... .......... .......... 79% 7.67M 5s
211650K .......... .......... .......... .......... .......... 79% 146M 5s
211700K .......... .......... .......... .......... .......... 79% 171M 5s
211750K .......... .......... .......... .......... .......... 79% 112M 5s
211800K .......... .......... .......... .......... .......... 79% 7.89M 5s
211850K .......... .......... .......... .......... .......... 79% 135M 5s
211900K .......... .......... .......... .......... .......... 79% 124M 5s
211950K .......... .......... .......... .......... .......... 79% 6.77M 5s
212000K .......... .......... .......... .......... .......... 79% 104M 5s
212050K .......... .......... .......... .......... .......... 79% 96.7M 5s
212100K .......... .......... .......... .......... .......... 79% 1.96M 5s
212150K .......... .......... .......... .......... .......... 79% 118M 5s
212200K .......... .......... .......... .......... .......... 79% 115M 5s
212250K .......... .......... .......... .......... .......... 79% 129M 5s
212300K .......... .......... .......... .......... .......... 79% 4.96M 5s
212350K .......... .......... .......... .......... .......... 79% 105M 5s
212400K .......... .......... .......... .......... .......... 79% 108M 5s
212450K .......... .......... .......... .......... .......... 79% 7.18M 5s
212500K .......... .......... .......... .......... .......... 79% 117M 5s
212550K .......... .......... .......... .......... .......... 80% 96.3M 5s
212600K .......... .......... .......... .......... .......... 80% 6.34M 5s
212650K .......... .......... .......... .......... .......... 80% 138M 5s
212700K .......... .......... .......... .......... .......... 80% 161M 5s
212750K .......... .......... .......... .......... .......... 80% 140M 5s
212800K .......... .......... .......... .......... .......... 80% 6.39M 5s
212850K .......... .......... .......... .......... .......... 80% 171M 5s
212900K .......... .......... .......... .......... .......... 80% 205M 5s
212950K .......... .......... .......... .......... .......... 80% 5.96M 5s
213000K .......... .......... .......... .......... .......... 80% 133M 5s
213050K .......... .......... .......... .......... .......... 80% 75.8M 5s
213100K .......... .......... .......... .......... .......... 80% 7.93M 5s
213150K .......... .......... .......... .......... .......... 80% 8.25M 5s
213200K .......... .......... .......... .......... .......... 80% 70.7M 5s
213250K .......... .......... .......... .......... .......... 80% 191M 5s
213300K .......... .......... .......... .......... .......... 80% 7.53M 5s
213350K .......... .......... .......... .......... .......... 80% 5.71M 5s
213400K .......... .......... .......... .......... .......... 80% 133M 5s
213450K .......... .......... .......... .......... .......... 80% 7.24M 5s
213500K .......... .......... .......... .......... .......... 80% 134M 5s
213550K .......... .......... .......... .......... .......... 80% 93.7M 5s
213600K .......... .......... .......... .......... .......... 80% 158M 5s
213650K .......... .......... .......... .......... .......... 80% 7.35M 5s
213700K .......... .......... .......... .......... .......... 80% 64.3M 5s
213750K .......... .......... .......... .......... .......... 80% 124M 5s
213800K .......... .......... .......... .......... .......... 80% 7.03M 5s
213850K .......... .......... .......... .......... .......... 80% 93.0M 5s
213900K .......... .......... .......... .......... .......... 80% 163M 5s
213950K .......... .......... .......... .......... .......... 80% 90.8M 5s
214000K .......... .......... .......... .......... .......... 80% 7.46M 5s
214050K .......... .......... .......... .......... .......... 80% 225M 5s
214100K .......... .......... .......... .......... .......... 80% 195M 5s
214150K .......... .......... .......... .......... .......... 80% 7.86M 5s
214200K .......... .......... .......... .......... .......... 80% 105M 5s
214250K .......... .......... .......... .......... .......... 80% 178M 5s
214300K .......... .......... .......... .......... .......... 80% 77.3M 5s
214350K .......... .......... .......... .......... .......... 80% 3.31M 5s
214400K .......... .......... .......... .......... .......... 80% 93.0M 5s
214450K .......... .......... .......... .......... .......... 80% 133M 5s
214500K .......... .......... .......... .......... .......... 80% 6.04M 5s
214550K .......... .......... .......... .......... .......... 80% 178M 5s
214600K .......... .......... .......... .......... .......... 80% 86.7M 5s
214650K .......... .......... .......... .......... .......... 80% 159M 5s
214700K .......... .......... .......... .......... .......... 80% 5.28M 5s
214750K .......... .......... .......... .......... .......... 80% 57.9M 5s
214800K .......... .......... .......... .......... .......... 80% 101M 5s
214850K .......... .......... .......... .......... .......... 80% 6.49M 5s
214900K .......... .......... .......... .......... .......... 80% 205M 5s
214950K .......... .......... .......... .......... .......... 80% 85.8M 5s
215000K .......... .......... .......... .......... .......... 80% 138M 5s
215050K .......... .......... .......... .......... .......... 80% 6.45M 5s
215100K .......... .......... .......... .......... .......... 80% 70.7M 5s
215150K .......... .......... .......... .......... .......... 80% 79.9M 5s
215200K .......... .......... .......... .......... .......... 80% 7.16M 5s
215250K .......... .......... .......... .......... .......... 81% 115M 5s
215300K .......... .......... .......... .......... .......... 81% 127M 5s
215350K .......... .......... .......... .......... .......... 81% 93.0M 5s
215400K .......... .......... .......... .......... .......... 81% 7.26M 5s
215450K .......... .......... .......... .......... .......... 81% 97.7M 5s
215500K .......... .......... .......... .......... .......... 81% 104M 5s
215550K .......... .......... .......... .......... .......... 81% 6.92M 5s
215600K .......... .......... .......... .......... .......... 81% 114M 5s
215650K .......... .......... .......... .......... .......... 81% 133M 5s
215700K .......... .......... .......... .......... .......... 81% 128M 5s
215750K .......... .......... .......... .......... .......... 81% 7.25M 5s
215800K .......... .......... .......... .......... .......... 81% 151M 5s
215850K .......... .......... .......... .......... .......... 81% 160M 5s
215900K .......... .......... .......... .......... .......... 81% 123M 4s
215950K .......... .......... .......... .......... .......... 81% 6.08M 4s
216000K .......... .......... .......... .......... .......... 81% 105M 4s
216050K .......... .......... .......... .......... .......... 81% 85.8M 4s
216100K .......... .......... .......... .......... .......... 81% 6.42M 4s
216150K .......... .......... .......... .......... .......... 81% 155M 4s
216200K .......... .......... .......... .......... .......... 81% 79.5M 4s
216250K .......... .......... .......... .......... .......... 81% 125M 4s
216300K .......... .......... .......... .......... .......... 81% 6.06M 4s
216350K .......... .......... .......... .......... .......... 81% 86.6M 4s
216400K .......... .......... .......... .......... .......... 81% 79.1M 4s
216450K .......... .......... .......... .......... .......... 81% 6.32M 4s
216500K .......... .......... .......... .......... .......... 81% 122M 4s
216550K .......... .......... .......... .......... .......... 81% 79.4M 4s
216600K .......... .......... .......... .......... .......... 81% 76.7M 4s
216650K .......... .......... .......... .......... .......... 81% 7.64M 4s
216700K .......... .......... .......... .......... .......... 81% 130M 4s
216750K .......... .......... .......... .......... .......... 81% 221M 4s
216800K .......... .......... .......... .......... .......... 81% 96.7M 4s
216850K .......... .......... .......... .......... .......... 81% 6.76M 4s
216900K .......... .......... .......... .......... .......... 81% 113M 4s
216950K .......... .......... .......... .......... .......... 81% 83.8M 4s
217000K .......... .......... .......... .......... .......... 81% 90.8M 4s
217050K .......... .......... .......... .......... .......... 81% 7.27M 4s
217100K .......... .......... .......... .......... .......... 81% 132M 4s
217150K .......... .......... .......... .......... .......... 81% 91.3M 4s
217200K .......... .......... .......... .......... .......... 81% 7.16M 4s
217250K .......... .......... .......... .......... .......... 81% 173M 4s
217300K .......... .......... .......... .......... .......... 81% 77.1M 4s
217350K .......... .......... .......... .......... .......... 81% 68.6M 4s
217400K .......... .......... .......... .......... .......... 81% 7.02M 4s
217450K .......... .......... .......... .......... .......... 81% 64.8M 4s
217500K .......... .......... .......... .......... .......... 81% 77.6M 4s
217550K .......... .......... .......... .......... .......... 81% 132M 4s
217600K .......... .......... .......... .......... .......... 81% 6.33M 4s
217650K .......... .......... .......... .......... .......... 81% 110M 4s
217700K .......... .......... .......... .......... .......... 81% 127M 4s
217750K .......... .......... .......... .......... .......... 81% 93.5M 4s
217800K .......... .......... .......... .......... .......... 81% 6.72M 4s
217850K .......... .......... .......... .......... .......... 81% 162M 4s
217900K .......... .......... .......... .......... .......... 82% 167M 4s
217950K .......... .......... .......... .......... .......... 82% 6.81M 4s
218000K .......... .......... .......... .......... .......... 82% 125M 4s
218050K .......... .......... .......... .......... .......... 82% 95.9M 4s
218100K .......... .......... .......... .......... .......... 82% 93.9M 4s
218150K .......... .......... .......... .......... .......... 82% 5.99M 4s
218200K .......... .......... .......... .......... .......... 82% 86.0M 4s
218250K .......... .......... .......... .......... .......... 82% 73.3M 4s
218300K .......... .......... .......... .......... .......... 82% 99.6M 4s
218350K .......... .......... .......... .......... .......... 82% 6.32M 4s
218400K .......... .......... .......... .......... .......... 82% 110M 4s
218450K .......... .......... .......... .......... .......... 82% 176M 4s
218500K .......... .......... .......... .......... .......... 82% 100M 4s
218550K .......... .......... .......... .......... .......... 82% 7.81M 4s
218600K .......... .......... .......... .......... .......... 82% 110M 4s
218650K .......... .......... .......... .......... .......... 82% 100M 4s
218700K .......... .......... .......... .......... .......... 82% 94.8M 4s
218750K .......... .......... .......... .......... .......... 82% 6.95M 4s
218800K .......... .......... .......... .......... .......... 82% 118M 4s
218850K .......... .......... .......... .......... .......... 82% 130M 4s
218900K .......... .......... .......... .......... .......... 82% 148M 4s
218950K .......... .......... .......... .......... .......... 82% 7.51M 4s
219000K .......... .......... .......... .......... .......... 82% 143M 4s
219050K .......... .......... .......... .......... .......... 82% 102M 4s
219100K .......... .......... .......... .......... .......... 82% 5.14M 4s
219150K .......... .......... .......... .......... .......... 82% 108M 4s
219200K .......... .......... .......... .......... .......... 82% 47.6M 4s
219250K .......... .......... .......... .......... .......... 82% 72.4M 4s
219300K .......... .......... .......... .......... .......... 82% 5.72M 4s
219350K .......... .......... .......... .......... .......... 82% 58.8M 4s
219400K .......... .......... .......... .......... .......... 82% 96.5M 4s
219450K .......... .......... .......... .......... .......... 82% 96.3M 4s
219500K .......... .......... .......... .......... .......... 82% 5.67M 4s
219550K .......... .......... .......... .......... .......... 82% 159M 4s
219600K .......... .......... .......... .......... .......... 82% 150M 4s
219650K .......... .......... .......... .......... .......... 82% 188M 4s
219700K .......... .......... .......... .......... .......... 82% 5.88M 4s
219750K .......... .......... .......... .......... .......... 82% 126M 4s
219800K .......... .......... .......... .......... .......... 82% 128M 4s
219850K .......... .......... .......... .......... .......... 82% 91.4M 4s
219900K .......... .......... .......... .......... .......... 82% 6.33M 4s
219950K .......... .......... .......... .......... .......... 82% 84.6M 4s
220000K .......... .......... .......... .......... .......... 82% 213M 4s
220050K .......... .......... .......... .......... .......... 82% 104M 4s
220100K .......... .......... .......... .......... .......... 82% 7.02M 4s
220150K .......... .......... .......... .......... .......... 82% 114M 4s
220200K .......... .......... .......... .......... .......... 82% 10.7M 4s
220250K .......... .......... .......... .......... .......... 82% 209M 4s
220300K .......... .......... .......... .......... .......... 82% 148M 4s
220350K .......... .......... .......... .......... .......... 82% 8.91M 4s
220400K .......... .......... .......... .......... .......... 82% 167M 4s
220450K .......... .......... .......... .......... .......... 82% 88.1M 4s
220500K .......... .......... .......... .......... .......... 82% 8.24M 4s
220550K .......... .......... .......... .......... .......... 83% 73.0M 4s
220600K .......... .......... .......... .......... .......... 83% 81.4M 4s
220650K .......... .......... .......... .......... .......... 83% 7.19M 4s
220700K .......... .......... .......... .......... .......... 83% 78.3M 4s
220750K .......... .......... .......... .......... .......... 83% 143M 4s
220800K .......... .......... .......... .......... .......... 83% 8.59M 4s
220850K .......... .......... .......... .......... .......... 83% 155M 4s
220900K .......... .......... .......... .......... .......... 83% 125M 4s
220950K .......... .......... .......... .......... .......... 83% 8.54M 4s
221000K .......... .......... .......... .......... .......... 83% 81.5M 4s
221050K .......... .......... .......... .......... .......... 83% 8.66M 4s
221100K .......... .......... .......... .......... .......... 83% 106M 4s
221150K .......... .......... .......... .......... .......... 83% 104M 4s
221200K .......... .......... .......... .......... .......... 83% 8.29M 4s
221250K .......... .......... .......... .......... .......... 83% 142M 4s
221300K .......... .......... .......... .......... .......... 83% 151M 4s
221350K .......... .......... .......... .......... .......... 83% 6.01M 4s
221400K .......... .......... .......... .......... .......... 83% 138M 4s
221450K .......... .......... .......... .......... .......... 83% 68.4M 4s
221500K .......... .......... .......... .......... .......... 83% 8.32M 4s
221550K .......... .......... .......... .......... .......... 83% 90.1M 4s
221600K .......... .......... .......... .......... .......... 83% 141M 4s
221650K .......... .......... .......... .......... .......... 83% 8.96M 4s
221700K .......... .......... .......... .......... .......... 83% 104M 4s
221750K .......... .......... .......... .......... .......... 83% 190M 4s
221800K .......... .......... .......... .......... .......... 83% 8.46M 4s
221850K .......... .......... .......... .......... .......... 83% 79.9M 4s
221900K .......... .......... .......... .......... .......... 83% 122M 4s
221950K .......... .......... .......... .......... .......... 83% 9.15M 4s
222000K .......... .......... .......... .......... .......... 83% 139M 4s
222050K .......... .......... .......... .......... .......... 83% 120M 4s
222100K .......... .......... .......... .......... .......... 83% 8.84M 4s
222150K .......... .......... .......... .......... .......... 83% 109M 4s
222200K .......... .......... .......... .......... .......... 83% 7.59M 4s
222250K .......... .......... .......... .......... .......... 83% 160M 4s
222300K .......... .......... .......... .......... .......... 83% 77.3M 4s
222350K .......... .......... .......... .......... .......... 83% 5.62M 4s
222400K .......... .......... .......... .......... .......... 83% 136M 4s
222450K .......... .......... .......... .......... .......... 83% 88.0M 4s
222500K .......... .......... .......... .......... .......... 83% 7.27M 4s
222550K .......... .......... .......... .......... .......... 83% 47.8M 4s
222600K .......... .......... .......... .......... .......... 83% 20.9M 4s
222650K .......... .......... .......... .......... .......... 83% 6.78M 4s
222700K .......... .......... .......... .......... .......... 83% 131M 4s
222750K .......... .......... .......... .......... .......... 83% 130M 4s
222800K .......... .......... .......... .......... .......... 83% 192M 4s
222850K .......... .......... .......... .......... .......... 83% 7.94M 4s
222900K .......... .......... .......... .......... .......... 83% 51.3M 4s
222950K .......... .......... .......... .......... .......... 83% 7.64M 4s
223000K .......... .......... .......... .......... .......... 83% 133M 4s
223050K .......... .......... .......... .......... .......... 83% 65.8M 4s
223100K .......... .......... .......... .......... .......... 83% 102M 4s
223150K .......... .......... .......... .......... .......... 83% 8.49M 4s
223200K .......... .......... .......... .......... .......... 84% 83.0M 4s
223250K .......... .......... .......... .......... .......... 84% 156M 4s
223300K .......... .......... .......... .......... .......... 84% 7.41M 4s
223350K .......... .......... .......... .......... .......... 84% 126M 4s
223400K .......... .......... .......... .......... .......... 84% 158M 4s
223450K .......... .......... .......... .......... .......... 84% 7.48M 4s
223500K .......... .......... .......... .......... .......... 84% 191M 4s
223550K .......... .......... .......... .......... .......... 84% 151M 4s
223600K .......... .......... .......... .......... .......... 84% 6.14M 4s
223650K .......... .......... .......... .......... .......... 84% 161M 4s
223700K .......... .......... .......... .......... .......... 84% 154M 4s
223750K .......... .......... .......... .......... .......... 84% 6.02M 4s
223800K .......... .......... .......... .......... .......... 84% 87.5M 4s
223850K .......... .......... .......... .......... .......... 84% 110M 4s
223900K .......... .......... .......... .......... .......... 84% 4.24M 4s
223950K .......... .......... .......... .......... .......... 84% 198M 4s
224000K .......... .......... .......... .......... .......... 84% 186M 4s
224050K .......... .......... .......... .......... .......... 84% 4.42M 4s
224100K .......... .......... .......... .......... .......... 84% 150M 4s
224150K .......... .......... .......... .......... .......... 84% 161M 4s
224200K .......... .......... .......... .......... .......... 84% 4.21M 4s
224250K .......... .......... .......... .......... .......... 84% 198M 4s
224300K .......... .......... .......... .......... .......... 84% 102M 4s
224350K .......... .......... .......... .......... .......... 84% 5.63M 4s
224400K .......... .......... .......... .......... .......... 84% 117M 4s
224450K .......... .......... .......... .......... .......... 84% 121M 4s
224500K .......... .......... .......... .......... .......... 84% 121M 4s
224550K .......... .......... .......... .......... .......... 84% 5.70M 4s
224600K .......... .......... .......... .......... .......... 84% 49.4M 4s
224650K .......... .......... .......... .......... .......... 84% 73.8M 4s
224700K .......... .......... .......... .......... .......... 84% 7.26M 4s
224750K .......... .......... .......... .......... .......... 84% 121M 4s
224800K .......... .......... .......... .......... .......... 84% 175M 4s
224850K .......... .......... .......... .......... .......... 84% 5.79M 4s
224900K .......... .......... .......... .......... .......... 84% 168M 4s
224950K .......... .......... .......... .......... .......... 84% 66.3M 4s
225000K .......... .......... .......... .......... .......... 84% 7.46M 4s
225050K .......... .......... .......... .......... .......... 84% 109M 4s
225100K .......... .......... .......... .......... .......... 84% 91.6M 4s
225150K .......... .......... .......... .......... .......... 84% 6.93M 4s
225200K .......... .......... .......... .......... .......... 84% 60.0M 4s
225250K .......... .......... .......... .......... .......... 84% 180M 4s
225300K .......... .......... .......... .......... .......... 84% 160M 4s
225350K .......... .......... .......... .......... .......... 84% 7.69M 4s
225400K .......... .......... .......... .......... .......... 84% 109M 4s
225450K .......... .......... .......... .......... .......... 84% 125M 4s
225500K .......... .......... .......... .......... .......... 84% 6.78M 4s
225550K .......... .......... .......... .......... .......... 84% 139M 4s
225600K .......... .......... .......... .......... .......... 84% 140M 4s
225650K .......... .......... .......... .......... .......... 84% 6.90M 4s
225700K .......... .......... .......... .......... .......... 84% 93.5M 4s
225750K .......... .......... .......... .......... .......... 84% 114M 4s
225800K .......... .......... .......... .......... .......... 84% 187M 4s
225850K .......... .......... .......... .......... .......... 85% 6.62M 4s
225900K .......... .......... .......... .......... .......... 85% 141M 4s
225950K .......... .......... .......... .......... .......... 85% 92.1M 4s
226000K .......... .......... .......... .......... .......... 85% 5.60M 4s
226050K .......... .......... .......... .......... .......... 85% 156M 4s
226100K .......... .......... .......... .......... .......... 85% 73.3M 4s
226150K .......... .......... .......... .......... .......... 85% 5.49M 4s
226200K .......... .......... .......... .......... .......... 85% 35.6M 3s
226250K .......... .......... .......... .......... .......... 85% 102M 3s
226300K .......... .......... .......... .......... .......... 85% 203M 3s
226350K .......... .......... .......... .......... .......... 85% 5.61M 3s
226400K .......... .......... .......... .......... .......... 85% 198M 3s
226450K .......... .......... .......... .......... .......... 85% 184M 3s
226500K .......... .......... .......... .......... .......... 85% 5.30M 3s
226550K .......... .......... .......... .......... .......... 85% 155M 3s
226600K .......... .......... .......... .......... .......... 85% 133M 3s
226650K .......... .......... .......... .......... .......... 85% 5.63M 3s
226700K .......... .......... .......... .......... .......... 85% 37.3M 3s
226750K .......... .......... .......... .......... .......... 85% 233M 3s
226800K .......... .......... .......... .......... .......... 85% 106M 3s
226850K .......... .......... .......... .......... .......... 85% 6.12M 3s
226900K .......... .......... .......... .......... .......... 85% 98.0M 3s
226950K .......... .......... .......... .......... .......... 85% 112M 3s
227000K .......... .......... .......... .......... .......... 85% 5.54M 3s
227050K .......... .......... .......... .......... .......... 85% 216M 3s
227100K .......... .......... .......... .......... .......... 85% 109M 3s
227150K .......... .......... .......... .......... .......... 85% 6.81M 3s
227200K .......... .......... .......... .......... .......... 85% 95.4M 3s
227250K .......... .......... .......... .......... .......... 85% 219M 3s
227300K .......... .......... .......... .......... .......... 85% 174M 3s
227350K .......... .......... .......... .......... .......... 85% 6.65M 3s
227400K .......... .......... .......... .......... .......... 85% 77.5M 3s
227450K .......... .......... .......... .......... .......... 85% 94.4M 3s
227500K .......... .......... .......... .......... .......... 85% 6.53M 3s
227550K .......... .......... .......... .......... .......... 85% 176M 3s
227600K .......... .......... .......... .......... .......... 85% 176M 3s
227650K .......... .......... .......... .......... .......... 85% 216M 3s
227700K .......... .......... .......... .......... .......... 85% 7.10M 3s
227750K .......... .......... .......... .......... .......... 85% 145M 3s
227800K .......... .......... .......... .......... .......... 85% 70.1M 3s
227850K .......... .......... .......... .......... .......... 85% 6.87M 3s
227900K .......... .......... .......... .......... .......... 85% 147M 3s
227950K .......... .......... .......... .......... .......... 85% 184M 3s
228000K .......... .......... .......... .......... .......... 85% 128M 3s
228050K .......... .......... .......... .......... .......... 85% 6.51M 3s
228100K .......... .......... .......... .......... .......... 85% 119M 3s
228150K .......... .......... .......... .......... .......... 85% 84.5M 3s
228200K .......... .......... .......... .......... .......... 85% 5.21M 3s
228250K .......... .......... .......... .......... .......... 85% 207M 3s
228300K .......... .......... .......... .......... .......... 85% 173M 3s
228350K .......... .......... .......... .......... .......... 85% 189M 3s
228400K .......... .......... .......... .......... .......... 85% 6.64M 3s
228450K .......... .......... .......... .......... .......... 85% 105M 3s
228500K .......... .......... .......... .......... .......... 86% 86.7M 3s
228550K .......... .......... .......... .......... .......... 86% 6.00M 3s
228600K .......... .......... .......... .......... .......... 86% 95.6M 3s
228650K .......... .......... .......... .......... .......... 86% 152M 3s
228700K .......... .......... .......... .......... .......... 86% 79.5M 3s
228750K .......... .......... .......... .......... .......... 86% 5.70M 3s
228800K .......... .......... .......... .......... .......... 86% 194M 3s
228850K .......... .......... .......... .......... .......... 86% 127M 3s
228900K .......... .......... .......... .......... .......... 86% 5.02M 3s
228950K .......... .......... .......... .......... .......... 86% 44.1M 3s
229000K .......... .......... .......... .......... .......... 86% 67.3M 3s
229050K .......... .......... .......... .......... .......... 86% 184M 3s
229100K .......... .......... .......... .......... .......... 86% 5.31M 3s
229150K .......... .......... .......... .......... .......... 86% 102M 3s
229200K .......... .......... .......... .......... .......... 86% 97.3M 3s
229250K .......... .......... .......... .......... .......... 86% 190M 3s
229300K .......... .......... .......... .......... .......... 86% 6.36M 3s
229350K .......... .......... .......... .......... .......... 86% 53.0M 3s
229400K .......... .......... .......... .......... .......... 86% 95.4M 3s
229450K .......... .......... .......... .......... .......... 86% 7.29M 3s
229500K .......... .......... .......... .......... .......... 86% 202M 3s
229550K .......... .......... .......... .......... .......... 86% 115M 3s
229600K .......... .......... .......... .......... .......... 86% 168M 3s
229650K .......... .......... .......... .......... .......... 86% 6.85M 3s
229700K .......... .......... .......... .......... .......... 86% 142M 3s
229750K .......... .......... .......... .......... .......... 86% 76.4M 3s
229800K .......... .......... .......... .......... .......... 86% 123M 3s
229850K .......... .......... .......... .......... .......... 86% 6.41M 3s
229900K .......... .......... .......... .......... .......... 86% 71.5M 3s
229950K .......... .......... .......... .......... .......... 86% 97.1M 3s
230000K .......... .......... .......... .......... .......... 86% 6.61M 3s
230050K .......... .......... .......... .......... .......... 86% 168M 3s
230100K .......... .......... .......... .......... .......... 86% 184M 3s
230150K .......... .......... .......... .......... .......... 86% 193M 3s
230200K .......... .......... .......... .......... .......... 86% 6.54M 3s
230250K .......... .......... .......... .......... .......... 86% 187M 3s
230300K .......... .......... .......... .......... .......... 86% 186M 3s
230350K .......... .......... .......... .......... .......... 86% 6.78M 3s
230400K .......... .......... .......... .......... .......... 86% 144M 3s
230450K .......... .......... .......... .......... .......... 86% 154M 3s
230500K .......... .......... .......... .......... .......... 86% 176M 3s
230550K .......... .......... .......... .......... .......... 86% 6.72M 3s
230600K .......... .......... .......... .......... .......... 86% 115M 3s
230650K .......... .......... .......... .......... .......... 86% 158M 3s
230700K .......... .......... .......... .......... .......... 86% 108M 3s
230750K .......... .......... .......... .......... .......... 86% 6.52M 3s
230800K .......... .......... .......... .......... .......... 86% 156M 3s
230850K .......... .......... .......... .......... .......... 86% 123M 3s
230900K .......... .......... .......... .......... .......... 86% 117M 3s
230950K .......... .......... .......... .......... .......... 86% 7.09M 3s
231000K .......... .......... .......... .......... .......... 86% 90.3M 3s
231050K .......... .......... .......... .......... .......... 86% 148M 3s
231100K .......... .......... .......... .......... .......... 86% 5.45M 3s
231150K .......... .......... .......... .......... .......... 87% 104M 3s
231200K .......... .......... .......... .......... .......... 87% 72.8M 3s
231250K .......... .......... .......... .......... .......... 87% 109M 3s
231300K .......... .......... .......... .......... .......... 87% 5.47M 3s
231350K .......... .......... .......... .......... .......... 87% 126M 3s
231400K .......... .......... .......... .......... .......... 87% 141M 3s
231450K .......... .......... .......... .......... .......... 87% 142M 3s
231500K .......... .......... .......... .......... .......... 87% 6.04M 3s
231550K .......... .......... .......... .......... .......... 87% 142M 3s
231600K .......... .......... .......... .......... .......... 87% 163M 3s
231650K .......... .......... .......... .......... .......... 87% 118M 3s
231700K .......... .......... .......... .......... .......... 87% 5.60M 3s
231750K .......... .......... .......... .......... .......... 87% 166M 3s
231800K .......... .......... .......... .......... .......... 87% 69.5M 3s
231850K .......... .......... .......... .......... .......... 87% 6.33M 3s
231900K .......... .......... .......... .......... .......... 87% 162M 3s
231950K .......... .......... .......... .......... .......... 87% 117M 3s
232000K .......... .......... .......... .......... .......... 87% 122M 3s
232050K .......... .......... .......... .......... .......... 87% 6.56M 3s
232100K .......... .......... .......... .......... .......... 87% 163M 3s
232150K .......... .......... .......... .......... .......... 87% 82.1M 3s
232200K .......... .......... .......... .......... .......... 87% 150M 3s
232250K .......... .......... .......... .......... .......... 87% 7.10M 3s
232300K .......... .......... .......... .......... .......... 87% 139M 3s
232350K .......... .......... .......... .......... .......... 87% 62.7M 3s
232400K .......... .......... .......... .......... .......... 87% 190M 3s
232450K .......... .......... .......... .......... .......... 87% 6.74M 3s
232500K .......... .......... .......... .......... .......... 87% 189M 3s
232550K .......... .......... .......... .......... .......... 87% 184M 3s
232600K .......... .......... .......... .......... .......... 87% 82.9M 3s
232650K .......... .......... .......... .......... .......... 87% 6.80M 3s
232700K .......... .......... .......... .......... .......... 87% 70.3M 3s
232750K .......... .......... .......... .......... .......... 87% 135M 3s
232800K .......... .......... .......... .......... .......... 87% 83.8M 3s
232850K .......... .......... .......... .......... .......... 87% 6.40M 3s
232900K .......... .......... .......... .......... .......... 87% 126M 3s
232950K .......... .......... .......... .......... .......... 87% 182M 3s
233000K .......... .......... .......... .......... .......... 87% 164M 3s
233050K .......... .......... .......... .......... .......... 87% 6.17M 3s
233100K .......... .......... .......... .......... .......... 87% 92.0M 3s
233150K .......... .......... .......... .......... .......... 87% 155M 3s
233200K .......... .......... .......... .......... .......... 87% 90.8M 3s
233250K .......... .......... .......... .......... .......... 87% 6.30M 3s
233300K .......... .......... .......... .......... .......... 87% 125M 3s
233350K .......... .......... .......... .......... .......... 87% 66.1M 3s
233400K .......... .......... .......... .......... .......... 87% 91.4M 3s
233450K .......... .......... .......... .......... .......... 87% 5.75M 3s
233500K .......... .......... .......... .......... .......... 87% 173M 3s
233550K .......... .......... .......... .......... .......... 87% 105M 3s
233600K .......... .......... .......... .......... .......... 87% 5.21M 3s
233650K .......... .......... .......... .......... .......... 87% 152M 3s
233700K .......... .......... .......... .......... .......... 87% 154M 3s
233750K .......... .......... .......... .......... .......... 87% 115M 3s
233800K .......... .......... .......... .......... .......... 87% 5.92M 3s
233850K .......... .......... .......... .......... .......... 88% 70.3M 3s
233900K .......... .......... .......... .......... .......... 88% 167M 3s
233950K .......... .......... .......... .......... .......... 88% 109M 3s
234000K .......... .......... .......... .......... .......... 88% 5.79M 3s
234050K .......... .......... .......... .......... .......... 88% 67.7M 3s
234100K .......... .......... .......... .......... .......... 88% 78.3M 3s
234150K .......... .......... .......... .......... .......... 88% 157M 3s
234200K .......... .......... .......... .......... .......... 88% 5.67M 3s
234250K .......... .......... .......... .......... .......... 88% 116M 3s
234300K .......... .......... .......... .......... .......... 88% 116M 3s
234350K .......... .......... .......... .......... .......... 88% 156M 3s
234400K .......... .......... .......... .......... .......... 88% 5.69M 3s
234450K .......... .......... .......... .......... .......... 88% 100M 3s
234500K .......... .......... .......... .......... .......... 88% 87.8M 3s
234550K .......... .......... .......... .......... .......... 88% 94.8M 3s
234600K .......... .......... .......... .......... .......... 88% 6.12M 3s
234650K .......... .......... .......... .......... .......... 88% 170M 3s
234700K .......... .......... .......... .......... .......... 88% 74.8M 3s
234750K .......... .......... .......... .......... .......... 88% 92.1M 3s
234800K .......... .......... .......... .......... .......... 88% 6.22M 3s
234850K .......... .......... .......... .......... .......... 88% 78.8M 3s
234900K .......... .......... .......... .......... .......... 88% 126M 3s
234950K .......... .......... .......... .......... .......... 88% 139M 3s
235000K .......... .......... .......... .......... .......... 88% 124M 3s
235050K .......... .......... .......... .......... .......... 88% 6.85M 3s
235100K .......... .......... .......... .......... .......... 88% 115M 3s
235150K .......... .......... .......... .......... .......... 88% 149M 3s
235200K .......... .......... .......... .......... .......... 88% 90.1M 3s
235250K .......... .......... .......... .......... .......... 88% 6.34M 3s
235300K .......... .......... .......... .......... .......... 88% 176M 3s
235350K .......... .......... .......... .......... .......... 88% 73.4M 3s
235400K .......... .......... .......... .......... .......... 88% 130M 3s
235450K .......... .......... .......... .......... .......... 88% 6.11M 3s
235500K .......... .......... .......... .......... .......... 88% 172M 3s
235550K .......... .......... .......... .......... .......... 88% 155M 3s
235600K .......... .......... .......... .......... .......... 88% 104M 3s
235650K .......... .......... .......... .......... .......... 88% 6.08M 3s
235700K .......... .......... .......... .......... .......... 88% 171M 3s
235750K .......... .......... .......... .......... .......... 88% 167M 3s
235800K .......... .......... .......... .......... .......... 88% 197M 3s
235850K .......... .......... .......... .......... .......... 88% 6.10M 3s
235900K .......... .......... .......... .......... .......... 88% 47.4M 3s
235950K .......... .......... .......... .......... .......... 88% 69.8M 3s
236000K .......... .......... .......... .......... .......... 88% 126M 3s
236050K .......... .......... .......... .......... .......... 88% 5.15M 3s
236100K .......... .......... .......... .......... .......... 88% 119M 3s
236150K .......... .......... .......... .......... .......... 88% 121M 3s
236200K .......... .......... .......... .......... .......... 88% 79.0M 3s
236250K .......... .......... .......... .......... .......... 88% 5.76M 3s
236300K .......... .......... .......... .......... .......... 88% 199M 3s
236350K .......... .......... .......... .......... .......... 88% 93.9M 3s
236400K .......... .......... .......... .......... .......... 88% 160M 3s
236450K .......... .......... .......... .......... .......... 88% 6.44M 3s
236500K .......... .......... .......... .......... .......... 89% 126M 3s
236550K .......... .......... .......... .......... .......... 89% 124M 3s
236600K .......... .......... .......... .......... .......... 89% 89.6M 3s
236650K .......... .......... .......... .......... .......... 89% 6.63M 3s
236700K .......... .......... .......... .......... .......... 89% 162M 3s
236750K .......... .......... .......... .......... .......... 89% 230M 3s
236800K .......... .......... .......... .......... .......... 89% 121M 3s
236850K .......... .......... .......... .......... .......... 89% 97.9M 3s
236900K .......... .......... .......... .......... .......... 89% 5.63M 2s
236950K .......... .......... .......... .......... .......... 89% 144M 2s
237000K .......... .......... .......... .......... .......... 89% 50.6M 2s
237050K .......... .......... .......... .......... .......... 89% 88.0M 2s
237100K .......... .......... .......... .......... .......... 89% 5.81M 2s
237150K .......... .......... .......... .......... .......... 89% 155M 2s
237200K .......... .......... .......... .......... .......... 89% 100M 2s
237250K .......... .......... .......... .......... .......... 89% 88.8M 2s
237300K .......... .......... .......... .......... .......... 89% 5.87M 2s
237350K .......... .......... .......... .......... .......... 89% 89.6M 2s
237400K .......... .......... .......... .......... .......... 89% 146M 2s
237450K .......... .......... .......... .......... .......... 89% 95.7M 2s
237500K .......... .......... .......... .......... .......... 89% 6.17M 2s
237550K .......... .......... .......... .......... .......... 89% 101M 2s
237600K .......... .......... .......... .......... .......... 89% 123M 2s
237650K .......... .......... .......... .......... .......... 89% 164M 2s
237700K .......... .......... .......... .......... .......... 89% 6.20M 2s
237750K .......... .......... .......... .......... .......... 89% 104M 2s
237800K .......... .......... .......... .......... .......... 89% 157M 2s
237850K .......... .......... .......... .......... .......... 89% 111M 2s
237900K .......... .......... .......... .......... .......... 89% 62.9M 2s
237950K .......... .......... .......... .......... .......... 89% 6.10M 2s
238000K .......... .......... .......... .......... .......... 89% 161M 2s
238050K .......... .......... .......... .......... .......... 89% 99.6M 2s
238100K .......... .......... .......... .......... .......... 89% 164M 2s
238150K .......... .......... .......... .......... .......... 89% 6.32M 2s
238200K .......... .......... .......... .......... .......... 89% 89.8M 2s
238250K .......... .......... .......... .......... .......... 89% 88.9M 2s
238300K .......... .......... .......... .......... .......... 89% 138M 2s
238350K .......... .......... .......... .......... .......... 89% 5.33M 2s
238400K .......... .......... .......... .......... .......... 89% 103M 2s
238450K .......... .......... .......... .......... .......... 89% 88.1M 2s
238500K .......... .......... .......... .......... .......... 89% 68.7M 2s
238550K .......... .......... .......... .......... .......... 89% 115M 2s
238600K .......... .......... .......... .......... .......... 89% 6.62M 2s
238650K .......... .......... .......... .......... .......... 89% 101M 2s
238700K .......... .......... .......... .......... .......... 89% 160M 2s
238750K .......... .......... .......... .......... .......... 89% 202M 2s
238800K .......... .......... .......... .......... .......... 89% 5.62M 2s
238850K .......... .......... .......... .......... .......... 89% 152M 2s
238900K .......... .......... .......... .......... .......... 89% 116M 2s
238950K .......... .......... .......... .......... .......... 89% 58.2M 2s
239000K .......... .......... .......... .......... .......... 89% 6.10M 2s
239050K .......... .......... .......... .......... .......... 89% 193M 2s
239100K .......... .......... .......... .......... .......... 89% 93.2M 2s
239150K .......... .......... .......... .......... .......... 90% 160M 2s
239200K .......... .......... .......... .......... .......... 90% 156M 2s
239250K .......... .......... .......... .......... .......... 90% 6.29M 2s
239300K .......... .......... .......... .......... .......... 90% 169M 2s
239350K .......... .......... .......... .......... .......... 90% 126M 2s
239400K .......... .......... .......... .......... .......... 90% 181M 2s
239450K .......... .......... .......... .......... .......... 90% 6.39M 2s
239500K .......... .......... .......... .......... .......... 90% 117M 2s
239550K .......... .......... .......... .......... .......... 90% 94.3M 2s
239600K .......... .......... .......... .......... .......... 90% 129M 2s
239650K .......... .......... .......... .......... .......... 90% 162M 2s
239700K .......... .......... .......... .......... .......... 90% 6.45M 2s
239750K .......... .......... .......... .......... .......... 90% 107M 2s
239800K .......... .......... .......... .......... .......... 90% 216M 2s
239850K .......... .......... .......... .......... .......... 90% 107M 2s
239900K .......... .......... .......... .......... .......... 90% 6.48M 2s
239950K .......... .......... .......... .......... .......... 90% 70.9M 2s
240000K .......... .......... .......... .......... .......... 90% 25.5M 2s
240050K .......... .......... .......... .......... .......... 90% 89.3M 2s
240100K .......... .......... .......... .......... .......... 90% 5.13M 2s
240150K .......... .......... .......... .......... .......... 90% 217M 2s
240200K .......... .......... .......... .......... .......... 90% 130M 2s
240250K .......... .......... .......... .......... .......... 90% 125M 2s
240300K .......... .......... .......... .......... .......... 90% 133M 2s
240350K .......... .......... .......... .......... .......... 90% 5.19M 2s
240400K .......... .......... .......... .......... .......... 90% 124M 2s
240450K .......... .......... .......... .......... .......... 90% 92.5M 2s
240500K .......... .......... .......... .......... .......... 90% 114M 2s
240550K .......... .......... .......... .......... .......... 90% 5.39M 2s
240600K .......... .......... .......... .......... .......... 90% 173M 2s
240650K .......... .......... .......... .......... .......... 90% 195M 2s
240700K .......... .......... .......... .......... .......... 90% 162M 2s
240750K .......... .......... .......... .......... .......... 90% 217M 2s
240800K .......... .......... .......... .......... .......... 90% 5.18M 2s
240850K .......... .......... .......... .......... .......... 90% 192M 2s
240900K .......... .......... .......... .......... .......... 90% 183M 2s
240950K .......... .......... .......... .......... .......... 90% 170M 2s
241000K .......... .......... .......... .......... .......... 90% 4.24M 2s
241050K .......... .......... .......... .......... .......... 90% 212M 2s
241100K .......... .......... .......... .......... .......... 90% 159M 2s
241150K .......... .......... .......... .......... .......... 90% 162M 2s
241200K .......... .......... .......... .......... .......... 90% 4.43M 2s
241250K .......... .......... .......... .......... .......... 90% 154M 2s
241300K .......... .......... .......... .......... .......... 90% 167M 2s
241350K .......... .......... .......... .......... .......... 90% 130M 2s
241400K .......... .......... .......... .......... .......... 90% 141M 2s
241450K .......... .......... .......... .......... .......... 90% 5.33M 2s
241500K .......... .......... .......... .......... .......... 90% 105M 2s
241550K .......... .......... .......... .......... .......... 90% 158M 2s
241600K .......... .......... .......... .......... .......... 90% 78.4M 2s
241650K .......... .......... .......... .......... .......... 90% 159M 2s
241700K .......... .......... .......... .......... .......... 90% 4.78M 2s
241750K .......... .......... .......... .......... .......... 90% 112M 2s
241800K .......... .......... .......... .......... .......... 91% 156M 2s
241850K .......... .......... .......... .......... .......... 91% 145M 2s
241900K .......... .......... .......... .......... .......... 91% 5.13M 2s
241950K .......... .......... .......... .......... .......... 91% 91.3M 2s
242000K .......... .......... .......... .......... .......... 91% 141M 2s
242050K .......... .......... .......... .......... .......... 91% 9.35M 2s
242100K .......... .......... .......... .......... .......... 91% 8.66M 2s
242150K .......... .......... .......... .......... .......... 91% 206M 2s
242200K .......... .......... .......... .......... .......... 91% 134M 2s
242250K .......... .......... .......... .......... .......... 91% 161M 2s
242300K .......... .......... .......... .......... .......... 91% 8.56M 2s
242350K .......... .......... .......... .......... .......... 91% 139M 2s
242400K .......... .......... .......... .......... .......... 91% 182M 2s
242450K .......... .......... .......... .......... .......... 91% 9.77M 2s
242500K .......... .......... .......... .......... .......... 91% 84.2M 2s
242550K .......... .......... .......... .......... .......... 91% 8.43M 2s
242600K .......... .......... .......... .......... .......... 91% 141M 2s
242650K .......... .......... .......... .......... .......... 91% 56.8M 2s
242700K .......... .......... .......... .......... .......... 91% 124M 2s
242750K .......... .......... .......... .......... .......... 91% 7.70M 2s
242800K .......... .......... .......... .......... .......... 91% 149M 2s
242850K .......... .......... .......... .......... .......... 91% 103M 2s
242900K .......... .......... .......... .......... .......... 91% 8.44M 2s
242950K .......... .......... .......... .......... .......... 91% 186M 2s
243000K .......... .......... .......... .......... .......... 91% 206M 2s
243050K .......... .......... .......... .......... .......... 91% 4.76M 2s
243100K .......... .......... .......... .......... .......... 91% 176M 2s
243150K .......... .......... .......... .......... .......... 91% 121M 2s
243200K .......... .......... .......... .......... .......... 91% 4.03M 2s
243250K .......... .......... .......... .......... .......... 91% 171M 2s
243300K .......... .......... .......... .......... .......... 91% 215M 2s
243350K .......... .......... .......... .......... .......... 91% 7.93M 2s
243400K .......... .......... .......... .......... .......... 91% 156M 2s
243450K .......... .......... .......... .......... .......... 91% 155M 2s
243500K .......... .......... .......... .......... .......... 91% 139M 2s
243550K .......... .......... .......... .......... .......... 91% 6.13M 2s
243600K .......... .......... .......... .......... .......... 91% 190M 2s
243650K .......... .......... .......... .......... .......... 91% 65.8M 2s
243700K .......... .......... .......... .......... .......... 91% 8.19M 2s
243750K .......... .......... .......... .......... .......... 91% 155M 2s
243800K .......... .......... .......... .......... .......... 91% 136M 2s
243850K .......... .......... .......... .......... .......... 91% 4.07M 2s
243900K .......... .......... .......... .......... .......... 91% 173M 2s
243950K .......... .......... .......... .......... .......... 91% 112M 2s
244000K .......... .......... .......... .......... .......... 91% 6.38M 2s
244050K .......... .......... .......... .......... .......... 91% 186M 2s
244100K .......... .......... .......... .......... .......... 91% 125M 2s
244150K .......... .......... .......... .......... .......... 91% 139M 2s
244200K .......... .......... .......... .......... .......... 91% 6.80M 2s
244250K .......... .......... .......... .......... .......... 91% 221M 2s
244300K .......... .......... .......... .......... .......... 91% 179M 2s
244350K .......... .......... .......... .......... .......... 91% 6.88M 2s
244400K .......... .......... .......... .......... .......... 91% 122M 2s
244450K .......... .......... .......... .......... .......... 92% 90.6M 2s
244500K .......... .......... .......... .......... .......... 92% 7.05M 2s
244550K .......... .......... .......... .......... .......... 92% 112M 2s
244600K .......... .......... .......... .......... .......... 92% 225M 2s
244650K .......... .......... .......... .......... .......... 92% 277M 2s
244700K .......... .......... .......... .......... .......... 92% 8.57M 2s
244750K .......... .......... .......... .......... .......... 92% 106M 2s
244800K .......... .......... .......... .......... .......... 92% 90.6M 2s
244850K .......... .......... .......... .......... .......... 92% 7.25M 2s
244900K .......... .......... .......... .......... .......... 92% 149M 2s
244950K .......... .......... .......... .......... .......... 92% 144M 2s
245000K .......... .......... .......... .......... .......... 92% 180M 2s
245050K .......... .......... .......... .......... .......... 92% 6.00M 2s
245100K .......... .......... .......... .......... .......... 92% 70.7M 2s
245150K .......... .......... .......... .......... .......... 92% 54.3M 2s
245200K .......... .......... .......... .......... .......... 92% 7.26M 2s
245250K .......... .......... .......... .......... .......... 92% 113M 2s
245300K .......... .......... .......... .......... .......... 92% 105M 2s
245350K .......... .......... .......... .......... .......... 92% 6.92M 2s
245400K .......... .......... .......... .......... .......... 92% 177M 2s
245450K .......... .......... .......... .......... .......... 92% 133M 2s
245500K .......... .......... .......... .......... .......... 92% 153M 2s
245550K .......... .......... .......... .......... .......... 92% 5.86M 2s
245600K .......... .......... .......... .......... .......... 92% 113M 2s
245650K .......... .......... .......... .......... .......... 92% 166M 2s
245700K .......... .......... .......... .......... .......... 92% 6.95M 2s
245750K .......... .......... .......... .......... .......... 92% 56.9M 2s
245800K .......... .......... .......... .......... .......... 92% 147M 2s
245850K .......... .......... .......... .......... .......... 92% 118M 2s
245900K .......... .......... .......... .......... .......... 92% 7.52M 2s
245950K .......... .......... .......... .......... .......... 92% 127M 2s
246000K .......... .......... .......... .......... .......... 92% 147M 2s
246050K .......... .......... .......... .......... .......... 92% 6.79M 2s
246100K .......... .......... .......... .......... .......... 92% 195M 2s
246150K .......... .......... .......... .......... .......... 92% 151M 2s
246200K .......... .......... .......... .......... .......... 92% 142M 2s
246250K .......... .......... .......... .......... .......... 92% 5.93M 2s
246300K .......... .......... .......... .......... .......... 92% 139M 2s
246350K .......... .......... .......... .......... .......... 92% 159M 2s
246400K .......... .......... .......... .......... .......... 92% 6.80M 2s
246450K .......... .......... .......... .......... .......... 92% 98.0M 2s
246500K .......... .......... .......... .......... .......... 92% 168M 2s
246550K .......... .......... .......... .......... .......... 92% 124M 2s
246600K .......... .......... .......... .......... .......... 92% 6.03M 2s
246650K .......... .......... .......... .......... .......... 92% 200M 2s
246700K .......... .......... .......... .......... .......... 92% 177M 2s
246750K .......... .......... .......... .......... .......... 92% 7.17M 2s
246800K .......... .......... .......... .......... .......... 92% 198M 2s
246850K .......... .......... .......... .......... .......... 92% 89.3M 2s
246900K .......... .......... .......... .......... .......... 92% 210M 2s
246950K .......... .......... .......... .......... .......... 92% 7.07M 2s
247000K .......... .......... .......... .......... .......... 92% 91.1M 2s
247050K .......... .......... .......... .......... .......... 92% 164M 2s
247100K .......... .......... .......... .......... .......... 93% 5.88M 2s
247150K .......... .......... .......... .......... .......... 93% 68.5M 2s
247200K .......... .......... .......... .......... .......... 93% 94.8M 2s
247250K .......... .......... .......... .......... .......... 93% 124M 2s
247300K .......... .......... .......... .......... .......... 93% 7.00M 2s
247350K .......... .......... .......... .......... .......... 93% 148M 2s
247400K .......... .......... .......... .......... .......... 93% 167M 2s
247450K .......... .......... .......... .......... .......... 93% 125M 2s
247500K .......... .......... .......... .......... .......... 93% 6.98M 2s
247550K .......... .......... .......... .......... .......... 93% 189M 2s
247600K .......... .......... .......... .......... .......... 93% 179M 2s
247650K .......... .......... .......... .......... .......... 93% 7.24M 2s
247700K .......... .......... .......... .......... .......... 93% 191M 2s
247750K .......... .......... .......... .......... .......... 93% 241M 2s
247800K .......... .......... .......... .......... .......... 93% 236M 2s
247850K .......... .......... .......... .......... .......... 93% 6.05M 2s
247900K .......... .......... .......... .......... .......... 93% 74.8M 2s
247950K .......... .......... .......... .......... .......... 93% 161M 2s
248000K .......... .......... .......... .......... .......... 93% 6.94M 2s
248050K .......... .......... .......... .......... .......... 93% 4.35M 2s
248100K .......... .......... .......... .......... .......... 93% 119M 1s
248150K .......... .......... .......... .......... .......... 93% 84.3M 1s
248200K .......... .......... .......... .......... .......... 93% 7.36M 1s
248250K .......... .......... .......... .......... .......... 93% 174M 1s
248300K .......... .......... .......... .......... .......... 93% 114M 1s
248350K .......... .......... .......... .......... .......... 93% 152M 1s
248400K .......... .......... .......... .......... .......... 93% 7.56M 1s
248450K .......... .......... .......... .......... .......... 93% 87.2M 1s
248500K .......... .......... .......... .......... .......... 93% 109M 1s
248550K .......... .......... .......... .......... .......... 93% 126M 1s
248600K .......... .......... .......... .......... .......... 93% 6.68M 1s
248650K .......... .......... .......... .......... .......... 93% 77.3M 1s
248700K .......... .......... .......... .......... .......... 93% 72.8M 1s
248750K .......... .......... .......... .......... .......... 93% 5.44M 1s
248800K .......... .......... .......... .......... .......... 93% 99.4M 1s
248850K .......... .......... .......... .......... .......... 93% 109M 1s
248900K .......... .......... .......... .......... .......... 93% 84.6M 1s
248950K .......... .......... .......... .......... .......... 93% 7.02M 1s
249000K .......... .......... .......... .......... .......... 93% 102M 1s
249050K .......... .......... .......... .......... .......... 93% 114M 1s
249100K .......... .......... .......... .......... .......... 93% 135M 1s
249150K .......... .......... .......... .......... .......... 93% 7.49M 1s
249200K .......... .......... .......... .......... .......... 93% 401K 1s
249250K .......... .......... .......... .......... .......... 93% 107M 1s
249300K .......... .......... .......... .......... .......... 93% 86.1M 1s
249350K .......... .......... .......... .......... .......... 93% 103M 1s
249400K .......... .......... .......... .......... .......... 93% 109M 1s
249450K .......... .......... .......... .......... .......... 93% 35.2M 1s
249500K .......... .......... .......... .......... .......... 93% 76.7M 1s
249550K .......... .......... .......... .......... .......... 93% 128M 1s
249600K .......... .......... .......... .......... .......... 93% 82.9M 1s
249650K .......... .......... .......... .......... .......... 93% 100M 1s
249700K .......... .......... .......... .......... .......... 93% 5.78M 1s
249750K .......... .......... .......... .......... .......... 94% 136M 1s
249800K .......... .......... .......... .......... .......... 94% 191M 1s
249850K .......... .......... .......... .......... .......... 94% 82.5M 1s
249900K .......... .......... .......... .......... .......... 94% 6.24M 1s
249950K .......... .......... .......... .......... .......... 94% 148M 1s
250000K .......... .......... .......... .......... .......... 94% 184M 1s
250050K .......... .......... .......... .......... .......... 94% 135M 1s
250100K .......... .......... .......... .......... .......... 94% 5.06M 1s
250150K .......... .......... .......... .......... .......... 94% 134M 1s
250200K .......... .......... .......... .......... .......... 94% 95.6M 1s
250250K .......... .......... .......... .......... .......... 94% 140M 1s
250300K .......... .......... .......... .......... .......... 94% 6.93M 1s
250350K .......... .......... .......... .......... .......... 94% 104M 1s
250400K .......... .......... .......... .......... .......... 94% 190M 1s
250450K .......... .......... .......... .......... .......... 94% 6.91M 1s
250500K .......... .......... .......... .......... .......... 94% 138M 1s
250550K .......... .......... .......... .......... .......... 94% 178M 1s
250600K .......... .......... .......... .......... .......... 94% 114M 1s
250650K .......... .......... .......... .......... .......... 94% 4.80M 1s
250700K .......... .......... .......... .......... .......... 94% 41.5M 1s
250750K .......... .......... .......... .......... .......... 94% 181M 1s
250800K .......... .......... .......... .......... .......... 94% 221M 1s
250850K .......... .......... .......... .......... .......... 94% 6.31M 1s
250900K .......... .......... .......... .......... .......... 94% 99.9M 1s
250950K .......... .......... .......... .......... .......... 94% 150M 1s
251000K .......... .......... .......... .......... .......... 94% 224M 1s
251050K .......... .......... .......... .......... .......... 94% 5.57M 1s
251100K .......... .......... .......... .......... .......... 94% 111M 1s
251150K .......... .......... .......... .......... .......... 94% 193M 1s
251200K .......... .......... .......... .......... .......... 94% 127M 1s
251250K .......... .......... .......... .......... .......... 94% 5.86M 1s
251300K .......... .......... .......... .......... .......... 94% 114M 1s
251350K .......... .......... .......... .......... .......... 94% 140M 1s
251400K .......... .......... .......... .......... .......... 94% 179M 1s
251450K .......... .......... .......... .......... .......... 94% 5.87M 1s
251500K .......... .......... .......... .......... .......... 94% 168M 1s
251550K .......... .......... .......... .......... .......... 94% 131M 1s
251600K .......... .......... .......... .......... .......... 94% 71.9M 1s
251650K .......... .......... .......... .......... .......... 94% 6.75M 1s
251700K .......... .......... .......... .......... .......... 94% 108M 1s
251750K .......... .......... .......... .......... .......... 94% 72.4M 1s
251800K .......... .......... .......... .......... .......... 94% 119M 1s
251850K .......... .......... .......... .......... .......... 94% 6.70M 1s
251900K .......... .......... .......... .......... .......... 94% 175M 1s
251950K .......... .......... .......... .......... .......... 94% 190M 1s
252000K .......... .......... .......... .......... .......... 94% 133M 1s
252050K .......... .......... .......... .......... .......... 94% 6.26M 1s
252100K .......... .......... .......... .......... .......... 94% 60.7M 1s
252150K .......... .......... .......... .......... .......... 94% 141M 1s
252200K .......... .......... .......... .......... .......... 94% 83.5M 1s
252250K .......... .......... .......... .......... .......... 94% 5.79M 1s
252300K .......... .......... .......... .......... .......... 94% 207M 1s
252350K .......... .......... .......... .......... .......... 94% 192M 1s
252400K .......... .......... .......... .......... .......... 94% 82.5M 1s
252450K .......... .......... .......... .......... .......... 95% 5.89M 1s
252500K .......... .......... .......... .......... .......... 95% 197M 1s
252550K .......... .......... .......... .......... .......... 95% 142M 1s
252600K .......... .......... .......... .......... .......... 95% 121M 1s
252650K .......... .......... .......... .......... .......... 95% 6.74M 1s
252700K .......... .......... .......... .......... .......... 95% 211M 1s
252750K .......... .......... .......... .......... .......... 95% 281M 1s
252800K .......... .......... .......... .......... .......... 95% 284M 1s
252850K .......... .......... .......... .......... .......... 95% 6.70M 1s
252900K .......... .......... .......... .......... .......... 95% 228M 1s
252950K .......... .......... .......... .......... .......... 95% 203M 1s
253000K .......... .......... .......... .......... .......... 95% 238M 1s
253050K .......... .......... .......... .......... .......... 95% 2.75M 1s
253100K .......... .......... .......... .......... .......... 95% 178M 1s
253150K .......... .......... .......... .......... .......... 95% 199M 1s
253200K .......... .......... .......... .......... .......... 95% 150M 1s
253250K .......... .......... .......... .......... .......... 95% 3.63M 1s
253300K .......... .......... .......... .......... .......... 95% 104M 1s
253350K .......... .......... .......... .......... .......... 95% 71.9M 1s
253400K .......... .......... .......... .......... .......... 95% 176M 1s
253450K .......... .......... .......... .......... .......... 95% 2.66M 1s
253500K .......... .......... .......... .......... .......... 95% 207M 1s
253550K .......... .......... .......... .......... .......... 95% 229M 1s
253600K .......... .......... .......... .......... .......... 95% 52.2M 1s
253650K .......... .......... .......... .......... .......... 95% 3.41M 1s
253700K .......... .......... .......... .......... .......... 95% 100M 1s
253750K .......... .......... .......... .......... .......... 95% 104M 1s
253800K .......... .......... .......... .......... .......... 95% 194M 1s
253850K .......... .......... .......... .......... .......... 95% 3.30M 1s
253900K .......... .......... .......... .......... .......... 95% 131M 1s
253950K .......... .......... .......... .......... .......... 95% 148M 1s
254000K .......... .......... .......... .......... .......... 95% 121M 1s
254050K .......... .......... .......... .......... .......... 95% 3.94M 1s
254100K .......... .......... .......... .......... .......... 95% 125M 1s
254150K .......... .......... .......... .......... .......... 95% 178M 1s
254200K .......... .......... .......... .......... .......... 95% 89.6M 1s
254250K .......... .......... .......... .......... .......... 95% 7.46M 1s
254300K .......... .......... .......... .......... .......... 95% 50.9M 1s
254350K .......... .......... .......... .......... .......... 95% 1.27M 1s
254400K .......... .......... .......... .......... .......... 95% 150M 1s
254450K .......... .......... .......... .......... .......... 95% 7.76M 1s
254500K .......... .......... .......... .......... .......... 95% 173M 1s
254550K .......... .......... .......... .......... .......... 95% 184M 1s
254600K .......... .......... .......... .......... .......... 95% 85.7M 1s
254650K .......... .......... .......... .......... .......... 95% 183M 1s
254700K .......... .......... .......... .......... .......... 95% 7.02M 1s
254750K .......... .......... .......... .......... .......... 95% 92.7M 1s
254800K .......... .......... .......... .......... .......... 95% 96.5M 1s
254850K .......... .......... .......... .......... .......... 95% 151M 1s
254900K .......... .......... .......... .......... .......... 95% 40.6M 1s
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265700K .......... .......... .......... .......... ... 100% 144M=22s
2024-05-30 12:19:38 (11.7 MB/s) - ‘ESPbeta.tgz’ saved [272121672/272121672]
+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.5
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/config/
+ ./makeEnv
ESP runtime AutoConfigurator
CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 with contents:
bin
include
lib
share
Info: Python exec /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python found!
Info: Python header /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11/Python.h found!
Info: Python library /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin/libpython3.11.dylib found!
ESP_ARCH = DARWIN64
ESP_ROOT = /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad
EFCOMP = gfortran
CARCH = DARWIN64
CASROOT = /Users/jenkins/util/ESP/OpenCASCADE-7.8.0
CASARCH = .
CASREV = 7.8
PYTHONINC= /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11
PYTHONLIB= -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
+ source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad
++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11
++ PYTHONINC=/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11
++ export 'PYTHONLIB=-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11'
++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=
++ CAPS_GLYPH=
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/ESP/ESP.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/ESP/ESP.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/wvClient/wv.html'
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src
+ make
(cd EGADS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/DARWIN64
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/DARWIN64
cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/DARWIN64
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/STANALYZER.make
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/STANALYZER.make
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads_dot.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads_dot.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.inc
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egads.inc
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/emp.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/emp.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/prm.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/prm.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.inc
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsserver.inc
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsss.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/wsss.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTris.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsTris.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineFit.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineFit.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineVels.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsSplineVels.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsf90.inc
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egadsf90.inc
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/Surreal/always_inline.h
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsGeom.cpp -o ./egadsGeom.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsHLevel.cpp -o ./egadsHLevel.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTopo.cpp -o ./egadsTopo.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsCopy.cpp -o ./egadsCopy.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSpline.cpp -o ./egadsSpline.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsIO.cpp -o ./egadsIO.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSkinning.cpp -o ./egadsSkinning.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTessSens.cpp -o ./egadsTessSens.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsBase.c -o ./egadsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTess.c -o ./egadsTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTris.c -o ./egadsTris.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsFit.c -o ./egadsFit.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmCfit.c -o ./prmCfit.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmGrid.c -o ./prmGrid.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmUV.c -o ./prmUV.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsExport.c -o ./egadsExport.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include ../util/emp.c \
-o ./emp.o
clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/evaluate.c -o ./evaluate.o
clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/rational.c -o ./rational.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
../util/regQuads.c -o ./regQuads.o
clang++ -g -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1
SurrealD1_test_suite Complete!
clang++ -g -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4
SurrealD4_test_suite Complete!
clang++ -g -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1
SurrealS1_test_suite Complete!
clang++ -g -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
./SurrealS4
SurrealS4_test_suite Complete!
/Library/Developer/CommandLineTools/usr/bin/make -C ../util
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
-o ./uvmap.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 egadsUVmap.c -Iuvmap \
-o ./egadsUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a
clang -g -o ./uvmap.exe ./uvmap.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -luvmap -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegads.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegads.dylib
(cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \
egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -lc++ \
-install_name '@rpath/libegads.dylib' \
-compatibility_version 7.8 \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadstatic.a
cp /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libuvmap.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadstatic.a
(cd .; \
ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \
evaluate.o rational.o regQuads.o; )
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsBase.c -o ./fgadsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsMemory.c -o ./fgadsMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsAttrs.c -o ./fgadsAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTess.c -o ./fgadsTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsHLevel.c -o ./fgadsHLevel.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsGeom.c -o ./fgadsGeom.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libfgads.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libfgads.a
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a emp.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libemp.a
*** EGADS Build Complete! ***
(cd EGADS/lite; make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o ./liteBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o ./liteMemory.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o ./liteGeom.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o ./liteTopo.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o ./liteAttrs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o ./liteImport.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o ./liteString.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o ./liteTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o ./liteTris.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src \
../src/egadsQuads.c -o ./liteQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o ./liteTessInp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 ../src/egadsRobust.c \
-o ./egadsRobust.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DDARWIN64 -I../include ../util/emp.c \
-o ./emp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o ./evaLite.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE ../util/rational.c \
-o ./ratLite.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I../util \
../util/regQuads.c -o ./liteRegQuads.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o ./liteEffect.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslite.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslite.dylib
(cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslite.dylib \
liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \
egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \
liteEffect.o liteUVmap.o \
-install_name '@rpath/libegadslite.dylib' \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
liteUVmap.o ; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libegadslitestatic.a
(cd wvServer; make)
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 map.cpp -o ./map.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include handshake.c -o ./handshake.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include md5.c -o ./md5.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include parsers.c -o ./parsers.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include extension.c -o ./extension.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include sha-1.c -o ./sha-1.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include server.c -o ./server.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include wv.c -o ./wv.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include fwv.c -o ./fwv.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
./fwv.o; )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \
-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -o ./servertest.o
clang++ -g -o ./server ./servertest.o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.a \
-lpthread -lz -lm
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.dylib
(cd .; clang++ -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libwsserver.dylib \
base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \
-install_name '@rpath/libwsserver.dylib' \
-compatibility_version 7.8 \
-current_version 1.0.25 )
(cd EGADS/examples; make -f egads2cart.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include egads2cart.c \
-o ./egads2cart.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
(cd EGADS/examples; make -f vCurvature.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vCurvature ./vCurvature.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
(cd EGADS/examples; make -f vGeom.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vGeom.c -o ./vGeom.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vGeom ./vGeom.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
(cd EGADS/examples; make -f vTess.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vTess.c -o ./vTess.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include ../util/retessFaces.c \
-o ./retessFaces.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet \
-lpthread -lz -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
(cd OpenCSM; make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udp.c -o ./udp.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libocsm.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libocsm.dylib
clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libocsm.dylib ./OpenCSM.o ./udp.o ./tim.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveESP ./serveESP.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bezier.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bezier.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/biconvex.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/biconvex.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/box.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/box.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/box.so ./udpBox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bspline.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bspline.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/catmull.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/catmull.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/compare.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/compare.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/compare.so ./udfCompare.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createBEM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createBEM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createPoly.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createPoly.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/csm.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/csm.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/csm.so ./udpCsm.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/deform.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/deform.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/deform.so ./udfDeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/droop.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/droop.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/droop.so ./udfDroop.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/dumpPmtrs.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/dumpPmtrs.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/editAttr.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/editAttr.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ellipse.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ellipse.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/eqn2body.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/eqn2body.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fitcurve.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fitcurve.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flend.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flend.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flend.so ./udfFlend.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/freeform.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/freeform.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ganged.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ganged.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/guide.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/guide.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/guide.so ./udfGuide.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hex.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hex.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hex.so ./udpHex.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/import.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/import.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/import.so ./udpImport.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/kulfan.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/kulfan.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/linalg.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/linalg.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/matchBodys.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/matchBodys.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mechanism.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mechanism.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca.so ./udpNaca.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca6mc.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca6mc.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nacelle.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nacelle.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nurbbody.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nurbbody.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nuscale.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nuscale.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/offset.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/offset.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/offset.so ./udfOffset.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parabaloid.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parabaloid.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parsec.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parsec.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pod.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pod.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pod.so ./udpPod.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/poly.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/poly.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/poly.so ./udpPoly.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBbox.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBbox.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBrep.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBrep.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printEgo.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printEgo.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/prop.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/prop.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/prop.so ./udpProp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/radwaf.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/radwaf.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sample.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sample.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sample.so ./udpSample.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sew.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sew.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/sew.so ./udpSew.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/shadow.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/shadow.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slices.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slices.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slices.so ./udfSlices.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stag.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stag.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stag.so ./udpStag.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stiffener.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stiffener.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/supell.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/supell.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/supell.so ./udpSupell.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester1.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester1.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester2.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester2.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vsp3.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vsp3.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/waffle.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/waffle.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/warp.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/warp.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/warp.so ./udpWarp.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/PDT2.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/PDT2.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca456.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca456.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads -lm -Wl,-w
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ereped.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ereped.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ereped.so ./timEreped.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mitten.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mitten.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mitten.so ./timMitten.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plotter.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plotter.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plugs.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slugs.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slugs.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vspSetup.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vspSetup.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/OpenCSM.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/OpenCSM.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/common.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/common.h
cp -p common.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/common.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udp.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udp.h
cp -p udp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udp.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/esp.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/esp.h
cp -p esp.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/esp.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/tim.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/tim.h
cp -p tim.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/tim.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egg.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egg.h
cp -p egg.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/egg.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.c
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/udpUtilities.c
(cd Slugs; make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. Fitter.c \
-o ./Fitter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. RedBlackTree.c \
-o ./RedBlackTree.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. Tessellate.c \
-o ./Tessellate.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
./Tessellate.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lwsserver -legads \
-lpthread -lz -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads \
-lpthread -lz -lm
(cd CAPS; make)
/bin/cp Cart3D/OSX64_CLANG/libc3dio.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/OSX64_CLANG/libCart3D.a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/DARWIN64/avl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/avl
/bin/cp Executables/DARWIN64/pplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/pplot
/bin/cp Executables/DARWIN64/pxplot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/pxplot
/bin/cp Executables/DARWIN64/xfoil /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/xfoil
/bin/cp Executables/DARWIN64/mastros.exe /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/DARWIN64/ASTRO.D01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/DARWIN64/ASTRO.IDX /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/DARWIN64/mses /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/mses
/bin/cp Executables/DARWIN64/mset /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/mset
/bin/cp udunits/include/*.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include
/bin/cp udunits/DARWIN64/libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib
/bin/ln -sf libudunits2.0.dylib /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libudunits2.dylib
/bin/cp Libraries/DARWIN64/aflr2AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/DARWIN64/aflr3AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/DARWIN64/aflr4AIM.so /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/aflr4AIM.so
(cd CAPS/src; make)
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/caps.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/caps.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsErrors.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsErrors.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsTypes.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/capsTypes.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimUtil.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimUtil.h
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimMesh.h
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aimMesh.h
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o ./aimTransferUtil.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../include \
aimMesh.c -o ./aimMesh.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a
ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
./aimTransferUtil.o
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libaimUtil.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. \
-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcaps.dylib
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcaps.dylib
(cd .; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
-install_name '@rpath/libcaps.dylib' \
-compatibility_version 1.0.25 \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcapsstatic.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libcapsstatic.a
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include testingAIM.c \
-o ./testingAIM.o
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so
rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include testingWriter.c \
-o ./testingWriter.o
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so
rm: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include phaseUtil.c \
-o ./phaseUtil.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
(cd ../CAPSexamples; make)
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include avlTest.c -o ./avlTest.o
clang -g -o ./avlTest ./avlTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
clang -g -o ./awaveTest ./awaveTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
clang -g -o ./frictionTest ./frictionTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
clang -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
clang -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
clang -g -o ./aeroelasticTest ./aeroelasticTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmTest.c -o ./hsmTest.o
clang -g -o ./hsmTest ./hsmTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o
clang -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o
clang -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o
clang -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include interferenceTest.c \
-o ./interferenceTest.o
clang -g -o ./interferenceTest ./interferenceTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include msesTest.c -o ./msesTest.o
clang -g -o ./msesTest ./msesTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include mystranTest.c -o ./mystranTest.o
clang -g -o ./mystranTest ./mystranTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
clang -g -o ./pointwiseTest ./pointwiseTest.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(cd CAPS/aim; make)
/Library/Developer/CommandLineTools/usr/bin/make -C utils
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a
/Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libutils.a(attrUtils.o) has no symbols
mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils
cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/aim/utils/vlmUtils.h
/Library/Developer/CommandLineTools/usr/bin/make -C abaqus
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \
abaqusAIM.c -o ./abaqusAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \
abaqusUtils.c -o ./abaqusUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \
-I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -lm -ldl -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin
/Library/Developer/CommandLineTools/usr/bin/make -C aflr2
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr3
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C aflr4
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C astros
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils astrosAIM.c \
-o ./astrosAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils astrosUtils.c \
-o ./astrosUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils astrosCards.c \
-o ./astrosCards.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C avl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/avlAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/avlAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C awave
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils awaveAIM.c \
-o ./awaveAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cart3d
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \
cart3dAIM.c -o ./cart3dAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/c3dio \
-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/libCart3D -I./xddm \
writeTrix.c -o ./writeTrix.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/c3dio \
-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/libCart3D \
surfTrix.c -o ./surfTrix.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -pedantic -I./xddm -I. \
`xml2-config --cflags` ./xddm/xddm.c \
-o ./xddm.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include bodyTess.c -o ./bodyTess.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \
./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/ \
-lc3dio -lCart3D -ldl -lxml2 -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include cart3dTest.c \
-o ./cart3dTest.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/cart3dTest ./cart3dTest.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I./xddm \
-I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o
clang -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \
./surfTrix.o ./xddm.o ./bodyTess.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -locsm -legads \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include/ -lc3dio -lCart3D \
-lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lxml2 -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cbaero
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
clang -g -bundle cbaeroAIM.o -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C cgt
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include egads2cgt.c \
-o ./egads2cgt.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include aflr4egads.c \
-o ./aflr4egads.o
clang++ -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C custom
make[2]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C delaundo
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils delaundoAIM.c \
-o ./delaundoAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/delaundoAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/delaundoAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C egadsTess
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils egadsTessAIM.c \
-o ./egadsTessAIM.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/egadsTessAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/egadsTessAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C friction
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -Wno-format -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils frictionAIM.c \
-o ./frictionAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/friction ./friction.o -Wl,-w -static-libgfortran -static-libgcc
/Library/Developer/CommandLineTools/usr/bin/make -C fun3d
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
-I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o ./fun3dUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \
-I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
./fun3dNamelist.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -lm -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin
/Library/Developer/CommandLineTools/usr/bin/make -C hsm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils hsmAIM.c \
-o src/hsmAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils hsmUtils.c \
-o src/hsmUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils hsmAdj.c \
-o src/hsmAdj.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
-o src/rcm.o
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \
-o src/genrcmi.o
/Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o
/Library/Developer/CommandLineTools/usr/bin/make -C src cross.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o
/Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o
/Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o
/Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating archive /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hsmAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hsmAIM.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/hsmAIM.so \
src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
src/rcm.o src/genrcmi.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C interference
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include interferenceAIM.c \
-o ./interferenceAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. cloudFns.c \
-o ./cloudFns.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/interferenceAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/interferenceAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/interferenceAIM.so \
./interferenceAIM.o ./cloudFns.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C masstran
clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils masstranAIM.cpp \
-o ./masstranAIM.o
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C meshWriter
/Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include bstlWriter.c \
-o ./bstlWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C bvtkWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include bvtkWriter.c \
-o ./bvtkWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter
make[3]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C fastWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include fastWriter.c \
-o ./fastWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C libmeshbWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include libmeshbWriter.c \
-o ./libmeshbWriter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C stlWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include stlWriter.c \
-o ./stlWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2Writer
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include su2Writer.c \
-o ./su2Writer.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tecplotWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include tecplotWriter.c \
-o ./tecplotWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include ugridWriter.c \
-o ./ugridWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C vtkWriter
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include vtkWriter.c \
-o ./vtkWriter.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mses
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mystran
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils mystranAIM.c \
-o ./mystranAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils mystranUtils.c \
-o ./mystranUtils.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C nastran
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils nastranAIM.c \
-o ./nastranAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C plato
Not compiling platoAIM: SEACAS must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C pointwise
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils pointwiseAIM.c \
-o ./pointwiseAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils hashElement.c \
-o ./hashElement.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pointwiseAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pointwiseAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -lpthread
/Library/Developer/CommandLineTools/usr/bin/make -C refine
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o ./refineAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/refineAIM.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/refineAIM.so
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSD
Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSM
Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment....
/Library/Developer/CommandLineTools/usr/bin/make -C skeleton
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils skeletonAIM.c \
-o ./skeletonAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker
make[2]: Nothing to be done for `default'.
/Library/Developer/CommandLineTools/usr/bin/make -C su2
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o ./su2AIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2Utils.c \
-o ./su2Utils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
-o ./su2_4_Cardinal.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2_5_Raven.c \
-o ./su2_5_Raven.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2_6_Falcon.c \
-o ./su2_6_Falcon.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
-o ./su2_7_Blackbird.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils su2_801_Harrier.c \
-o ./su2_801_Harrier.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tacs
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils tacsAIM.c \
-o ./tacsAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11
/Library/Developer/CommandLineTools/usr/bin/make -C tetgen
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils tetgenAIM.cpp \
-o ./tetgenAIM.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
./tetgen_Interface.o ./tetgen.o \
./predicates.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tsfoil
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \
tsfoilAIM.c -o ./tsfoilAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C unitTest
make[2]: Nothing to be done for `all'.
/Library/Developer/CommandLineTools/usr/bin/make -C xfoil
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils \
xfoilAIM.c -o ./xfoilAIM.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
-L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C zaero
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
clang -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
(cd OpenCSM; make -f serveESP.make)
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/capsMode.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flowchart.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/viewer.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/viewer.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/viewer.so ./timViewer.o -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/include -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pyscript.so
clang++ -g -bundle -o /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -L/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin
*** Build Completed! ***
+ export CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin
++ uname -a
+ [[ Darwin macys-VM 20.6.0 Darwin Kernel Version 20.6.0: Thu Sep 29 20:15:11 PDT 2022; root:xnu-7195.141.42~1/RELEASE_X86_64 x86_64 == *\D\a\r\w\i\n* ]]
+ sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==> serveESP completed successfully with no verification data
real 0m2.268s
user 0m0.051s
sys 0m0.041s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.293s
user 0m0.342s
sys 0m0.033s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m4.146s
user 0m4.541s
sys 0m0.652s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.702s
user 0m0.799s
sys 0m0.042s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.724s
user 0m1.017s
sys 0m0.067s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.640s
user 0m0.902s
sys 0m0.036s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m6.161s
user 0m8.959s
sys 0m0.469s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m55.945s
user 1m23.756s
sys 0m3.665s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.664s
user 0m0.830s
sys 0m0.036s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m51.990s
user 1m33.903s
sys 0m7.222s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
==> serveESP completed successfully with 1 warnings and no verification data
real 0m0.362s
user 0m0.286s
sys 0m0.042s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.525s
user 0m0.824s
sys 0m0.021s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.174s
user 0m0.248s
sys 0m0.018s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data
real 0m0.453s
user 0m0.529s
sys 0m0.028s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.5
python -u -m unittest discover
.................................................... PCurve Map: 48 (alloc 48)!
Surface Map: 12 (alloc 24)!
Curve Map: 28 (alloc 28)!
Writing PCurves...
Writing Curves...
Writing Surfaces...
Writing 16 Nodes...
Writing 28 Edges...
Writing 12 Loops...
Writing 12 Faces...
Writing 1 Shells...
EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 2.983s
OK
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m12.869s
user 0m12.632s
sys 0m0.427s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.5
python -u -m unittest discover
..Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 143
Number of elements = 282
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 282
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 155
Number of elements = 306
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 306
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 298
Combined Number of elements = 588
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 588
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library - d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing1, index = 1
Name = Wing2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 209
Number of elements = 414
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 414
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 186
Number of elements = 368
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 368
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 395
Combined Number of elements = 782
Combined Elemental Nodes = 0
Combined Elemental Rods = 0
Combined Elemental Tria3 = 782
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Wing1
Property name - Wing2
Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> _body (EG_attributeDel)!
EGADS Error: No Attribute -> _nface (EG_attributeDel)!
EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
updating CFGPMTR series [ 1, 1] = 8412.000000
updating CFGPMTR series2 [ 1, 1] = 20.000000
updating CFGPMTR VIEW:CFD [ 1, 1] = 1.000000
updating CFGPMTR nrow [ 1, 1] = 3.000000
updating CFGPMTR ncol [ 1, 1] = 2.000000
updating DESPMTR area [ 1, 1] = 40.000000
updating DESPMTR aspect [ 1, 1] = 5.000000
updating DESPMTR taper [ 1, 1] = 0.500000
updating DESPMTR twist [ 1, 1] = 15.000000
updating DESPMTR wing:lesweep [ 1, 1] = 30.000000
updating DESPMTR wing:dihedral [ 1, 1] = 1.000000
updating DESPMTR wing:chord:root [ 1, 1] = 1.560000
updating DESPMTR htail [ 1, 1] = 1.000000
updating DESPMTR htail:chord [ 1, 1] = 2.000000
updating DESPMTR vtail:chord [ 1, 1] = 3.000000
updating DESPMTR vtail [ 1, 1] = 4.000000
updating DESPMTR sphereR [ 1, 1] = 80.000000
updating DESPMTR v@1:d_name [ 1, 1] = 1.000000
updating DESPMTR despMat [ 1, 1] = 11.000000
updating DESPMTR despMat [ 1, 2] = 12.000000
updating DESPMTR despMat [ 2, 1] = 13.000000
updating DESPMTR despMat [ 2, 2] = 14.000000
updating DESPMTR despMat [ 3, 1] = 15.000000
updating DESPMTR despMat [ 3, 2] = 16.000000
updating DESPMTR despCol [ 1, 1] = 11.000000
updating DESPMTR despCol [ 2, 1] = 13.000000
updating DESPMTR despCol [ 3, 1] = 15.000000
updating DESPMTR despRow [ 1, 1] = 11.000000
updating DESPMTR despRow [ 1, 2] = 12.000000
updating DESPMTR despRow [ 1, 3] = 13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
----------------------------------------------------------------------
Ran 100 tests in 35.280s
OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.5
python -u -m unittest discover --verbose
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.033 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 = 0.088 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.008 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2224 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2224 2224
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 446 894
AFLR2 IG : Nodes, Faces = 892 1786
AFLR2 IG : Nodes, Faces = 918 1838
AFLR2 IG : Nodes, Faces = 1033 2068
AFLR2 IG : Nodes, Faces = 1133 2268
AFLR2 IG : Nodes, Faces = 1233 2468
AFLR2 IG : Nodes, Faces = 1333 2668
AFLR2 IG : Nodes, Faces = 1338 2678
AFLR2 IG : Nodes, Faces = 1433 2868
AFLR2 IG : Nodes, Faces = 1533 3068
AFLR2 IG : Nodes, Faces = 1633 3268
AFLR2 IG : Nodes, Faces = 1733 3468
AFLR2 IG : Nodes, Faces = 1784 3570
AFLR2 IG : Nodes, Faces = 1833 3668
AFLR2 IG : Nodes, Faces = 1858 3718
AFLR2 IG : Nodes, Faces = 2224 4450
AFLR2 IG : Nodes, Faces = 2228 4450
AFLR2 IG : Nodes, Faces = 2224 2224
AFLR2 : CPU Time = 0.032 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 = 0.083 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.009 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 = 0.032 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 = 0.088 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.009 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
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 = 0.033 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 = 0.085 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 = 0.080 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.007 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 48 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 10 22
AFLR2 IG : Nodes, Faces = 20 42
AFLR2 IG : Nodes, Faces = 30 62
AFLR2 IG : Nodes, Faces = 40 82
AFLR2 IG : Nodes, Faces = 45 92
AFLR2 IG : Nodes, Faces = 46 94
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 98
AFLR2 IG : Nodes, Faces = 48 48
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 48 48
AFLR2 GG : Nodes, Faces = 88 128
AFLR2 GG : Nodes, Faces = 109 170
AFLR2 GG : Nodes, Faces = 124 200
AFLR2 GG : Nodes, Faces = 136 224
AFLR2 GG : Nodes, Faces = 148 248
AFLR2 GG : Nodes, Faces = 161 274
AFLR2 GG : Nodes, Faces = 171 294
AFLR2 GG : Nodes, Faces = 181 314
AFLR2 GG : Nodes, Faces = 187 326
AFLR2 GG : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 344 344
AFLR2 GG : Nodes, Faces = 679 1014
AFLR2 GG : Nodes, Faces = 1006 1668
AFLR2 GG : Nodes, Faces = 1321 2298
AFLR2 GG : Nodes, Faces = 1604 2864
AFLR2 GG : Nodes, Faces = 1886 3428
AFLR2 GG : Nodes, Faces = 2155 3966
AFLR2 GG : Nodes, Faces = 2409 4474
AFLR2 GG : Nodes, Faces = 2649 4954
AFLR2 GG : Nodes, Faces = 2867 5390
AFLR2 GG : Nodes, Faces = 3063 5782
AFLR2 GG : Nodes, Faces = 3243 6142
AFLR2 GG : Nodes, Faces = 3400 6456
AFLR2 GG : Nodes, Faces = 3540 6736
AFLR2 GG : Nodes, Faces = 3665 6986
AFLR2 GG : Nodes, Faces = 3786 7228
AFLR2 GG : Nodes, Faces = 3900 7456
AFLR2 GG : Nodes, Faces = 4010 7676
AFLR2 GG : Nodes, Faces = 4114 7884
AFLR2 GG : Nodes, Faces = 4209 8074
AFLR2 GG : Nodes, Faces = 4292 8240
AFLR2 GG : Nodes, Faces = 4368 8392
AFLR2 GG : Nodes, Faces = 4439 8534
AFLR2 GG : Nodes, Faces = 4503 8662
AFLR2 GG : Nodes, Faces = 4560 8776
AFLR2 GG : Nodes, Faces = 4611 8878
AFLR2 GG : Nodes, Faces = 4650 8956
AFLR2 GG : Nodes, Faces = 4677 9010
AFLR2 GG : Nodes, Faces = 4695 9046
AFLR2 GG : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.012 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 = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.012 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4058 7772
AFLR2 QI : Nodes, Faces = 4057 364
AFLR2 QI : Nodes, Faces = 4057 3703
AFLR2 QI : Nodes, Faces = 4057 7770
AFLR2 QI : Nodes, Faces = 4056 344
AFLR2 QI : Nodes, Faces = 4056 3712
AFLR2 QI : Nodes, Faces = 4056 7768
AFLR2 QI : Nodes, Faces = 4055 348
AFLR2 QI : Nodes, Faces = 4055 3709
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 392
AFLR2 QI : Nodes, Faces = 4055 3687
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 : CPU Time = 0.008 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_aflr2.TestAFLR2.test_setInput) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 339 680
AFLR2 IG : Nodes, Faces = 340 682
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 682 1020
AFLR2 GGp: Nodes, Faces = 1010 1676
AFLR2 GGp: Nodes, Faces = 1316 2288
AFLR2 GGp: Nodes, Faces = 1592 2840
AFLR2 GGp: Nodes, Faces = 1855 3366
AFLR2 GGp: Nodes, Faces = 2106 3868
AFLR2 GGp: Nodes, Faces = 2341 4338
AFLR2 GGp: Nodes, Faces = 2551 4758
AFLR2 GGp: Nodes, Faces = 2741 5138
AFLR2 GGp: Nodes, Faces = 2917 5490
AFLR2 GGp: Nodes, Faces = 3082 5820
AFLR2 GGp: Nodes, Faces = 3240 6136
AFLR2 GGp: Nodes, Faces = 3379 6414
AFLR2 GGp: Nodes, Faces = 3513 6682
AFLR2 GGp: Nodes, Faces = 3642 6940
AFLR2 GGp: Nodes, Faces = 3748 7152
AFLR2 GGp: Nodes, Faces = 3846 7348
AFLR2 GGp: Nodes, Faces = 3931 7518
AFLR2 GGp: Nodes, Faces = 3999 7654
AFLR2 GGp: Nodes, Faces = 4044 7744
AFLR2 GGp: Nodes, Faces = 4058 7772
AFLR2 : CPU Time = 0.013 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4058 7772
AFLR2 QI : Nodes, Faces = 4057 364
AFLR2 QI : Nodes, Faces = 4057 3703
AFLR2 QI : Nodes, Faces = 4057 7770
AFLR2 QI : Nodes, Faces = 4056 344
AFLR2 QI : Nodes, Faces = 4056 3712
AFLR2 QI : Nodes, Faces = 4056 7768
AFLR2 QI : Nodes, Faces = 4055 348
AFLR2 QI : Nodes, Faces = 4055 3709
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 392
AFLR2 QI : Nodes, Faces = 4055 3687
AFLR2 QI : Nodes, Faces = 4055 7766
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 QI : Nodes, Faces = 4055 386
AFLR2 QI : Nodes, Faces = 4055 3690
AFLR2 : CPU Time = 0.008 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1189
Number of elements = 6249
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6237
Number of elements = 34620
Number of triangles = 4438
Number of quadrilatarals = 0
Number of tetrahedrals = 30182
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13613
Number of elements = 76414
Number of triangles = 8142
Number of quadrilatarals = 0
Number of tetrahedrals = 68272
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 41618
Number of elements = 236483
Number of triangles = 19838
Number of quadrilatarals = 0
Number of tetrahedrals = 216645
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4369
Number of elements = 24223
Number of triangles = 3016
Number of quadrilatarals = 0
Number of tetrahedrals = 21207
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 11007
Number of elements = 60837
Number of triangles = 8632
Number of quadrilatarals = 0
Number of tetrahedrals = 52205
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10474
Number of elements = 58678
Number of triangles = 6352
Number of quadrilatarals = 0
Number of tetrahedrals = 52326
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 88507
Number of elements = 497504
Number of triangles = 51750
Number of quadrilatarals = 0
Number of tetrahedrals = 445754
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16456
Number of elements = 93635
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 85709
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2589
Number of elements = 13809
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11051
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3654
Number of elements = 19800
Number of triangles = 3394
Number of quadrilatarals = 0
Number of tetrahedrals = 16406
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_bullet (test_aflr3.TestAFLR3.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5456
Number of elements = 30308
Number of triangles = 3656
Number of quadrilatarals = 0
Number of tetrahedrals = 26652
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cone (test_aflr3.TestAFLR3.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4694
Number of elements = 25935
Number of triangles = 3326
Number of quadrilatarals = 0
Number of tetrahedrals = 22609
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5554
Number of elements = 30862
Number of triangles = 3756
Number of quadrilatarals = 0
Number of tetrahedrals = 27106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2260
Number of elements = 12133
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2392
Number of elements = 12577
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3341
Number of elements = 18069
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3606
Number of elements = 18961
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4414
Number of elements = 23974
Number of triangles = 3998
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4811
Number of elements = 25310
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5490
Number of elements = 29891
Number of triangles = 4886
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6019
Number of elements = 31671
Number of triangles = 6666
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6542
Number of elements = 35667
Number of triangles = 5774
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7203
Number of elements = 37891
Number of triangles = 7998
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7601
Number of elements = 41489
Number of triangles = 6662
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8394
Number of elements = 44157
Number of triangles = 9330
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19800
Number of elements = 109798
Number of triangles = 15540
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22741
Number of elements = 119570
Number of triangles = 25312
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1193
Number of elements = 6272
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4940
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1176
Number of elements = 6165
Number of triangles = 1330
Number of quadrilatarals = 0
Number of tetrahedrals = 4835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1203
Number of elements = 6314
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4982
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1198
Number of elements = 6296
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4964
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1223
Number of elements = 6443
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5111
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1184
Number of elements = 6224
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4892
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1195
Number of elements = 6287
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4955
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1197
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1203
Number of elements = 6310
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4978
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1191
Number of elements = 6253
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4921
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8857
Number of elements = 49191
Number of triangles = 6284
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8989
Number of elements = 49635
Number of triangles = 6728
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7796
Number of elements = 43368
Number of triangles = 5396
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6267
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4935
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9944
Number of elements = 55193
Number of triangles = 7174
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10218
Number of elements = 56081
Number of triangles = 8062
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7818
Number of elements = 43469
Number of triangles = 5398
Number of quadrilatarals = 0
Number of tetrahedrals = 38071
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1202
Number of elements = 6320
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4988
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1198
Number of elements = 6292
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4960
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9609
Number of elements = 53228
Number of triangles = 6994
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9829
Number of elements = 53956
Number of triangles = 7722
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7789
Number of elements = 43295
Number of triangles = 5394
Number of quadrilatarals = 0
Number of tetrahedrals = 37901
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1186
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 854
Number of elements = 4431
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3435
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9348
Number of elements = 51734
Number of triangles = 6812
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9531
Number of elements = 52330
Number of triangles = 7408
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7804
Number of elements = 43358
Number of triangles = 5386
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1200
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9183
Number of elements = 50871
Number of triangles = 6632
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9322
Number of elements = 51307
Number of triangles = 7068
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7927
Number of elements = 44116
Number of triangles = 5382
Number of quadrilatarals = 0
Number of tetrahedrals = 38734
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 868
Number of elements = 4530
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3534
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10181
Number of elements = 56797
Number of triangles = 6782
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10671
Number of elements = 58561
Number of triangles = 8546
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7741
Number of elements = 43010
Number of triangles = 5362
Number of quadrilatarals = 0
Number of tetrahedrals = 37648
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2692
Number of elements = 14435
Number of triangles = 2800
Number of quadrilatarals = 0
Number of tetrahedrals = 11635
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 238
Number of elements = 1116
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 732
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1500
Number of elements = 7757
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1564
Number of elements = 7881
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1160
Number of elements = 6087
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4779
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1635
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 159
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 75
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5075
Number of elements = 27761
Number of triangles = 4072
Number of quadrilatarals = 0
Number of tetrahedrals = 23689
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5221
Number of elements = 28313
Number of triangles = 4624
Number of quadrilatarals = 0
Number of tetrahedrals = 23689
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4882
Number of elements = 26790
Number of triangles = 4040
Number of quadrilatarals = 0
Number of tetrahedrals = 22750
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 339
Number of elements = 1523
Number of triangles = 584
Number of quadrilatarals = 0
Number of tetrahedrals = 939
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 32776
Number of elements = 189806
Number of triangles = 8496
Number of quadrilatarals = 0
Number of tetrahedrals = 181310
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36115
Number of elements = 203130
Number of triangles = 21820
Number of quadrilatarals = 0
Number of tetrahedrals = 181310
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28584
Number of elements = 162362
Number of triangles = 15158
Number of quadrilatarals = 0
Number of tetrahedrals = 147204
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1425
Number of elements = 7592
Number of triangles = 1456
Number of quadrilatarals = 0
Number of tetrahedrals = 6136
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4138
Number of elements = 22901
Number of triangles = 2938
Number of quadrilatarals = 0
Number of tetrahedrals = 19963
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 711
Number of elements = 3685
Number of triangles = 844
Number of quadrilatarals = 0
Number of tetrahedrals = 2841
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1257
Number of elements = 6590
Number of triangles = 1424
Number of quadrilatarals = 0
Number of tetrahedrals = 5166
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16639
Number of elements = 94369
Number of triangles = 8800
Number of quadrilatarals = 0
Number of tetrahedrals = 85569
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18563
Number of elements = 101745
Number of triangles = 16176
Number of quadrilatarals = 0
Number of tetrahedrals = 85569
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12009
Number of elements = 67436
Number of triangles = 7140
Number of quadrilatarals = 0
Number of tetrahedrals = 60296
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6554
Number of elements = 34309
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25273
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2865
Number of elements = 12676
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7224
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2477
Number of elements = 10753
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6201
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4989
Number of elements = 27641
Number of triangles = 3462
Number of quadrilatarals = 0
Number of tetrahedrals = 24179
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_torus (test_aflr3.TestAFLR3.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6401
Number of elements = 35742
Number of triangles = 4048
Number of quadrilatarals = 0
Number of tetrahedrals = 31694
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59702
Number of elements = 348382
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 335454
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 58332
Number of elements = 339688
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 327260
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59702
Number of elements = 347882
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 335454
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Binary STL file ....
Finished writing Binary STL file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 44
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 3
Surface 2: Number of points found for aero-spline = 6
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
8 automatic connections were made for capsConnect Rib_Root (node id 1)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
ok
test_MassProp_Units (test_avl.TestAVL.test_MassProp_Units) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_MassProp_noUnits (test_avl.TestAVL.test_MassProp_noUnits) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing mass properties file: caps.mass
Parsing MassProp
ok
test_alpha_custom_increment (test_avl.TestAVL.test_alpha_custom_increment) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_geom_change (test_avl.TestAVL.test_geom_change) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_numSpan (test_avl.TestAVL.test_numSpan) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
ok
test_phase (test_avl.TestAVL.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
ok
test_wing_Vtail (test_avl.TestAVL.test_wing_Vtail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
ok
test_wing_tail (test_avl.TestAVL.test_wing_tail) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control RightAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control LeftAileron not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Elevator not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Warning: Control Rudder not found in controls tuple! Only defaults will be used.
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_wing_tail_control (test_avl.TestAVL.test_wing_tail_control) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice control surface data
VLM control surface name - Elevator
VLM control surface name - LeftAileron
VLM control surface name - RightAileron
VLM control surface name - Rudder
Done getting vortex lattice control surface data
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Control surface 1 of 1
Section 2 of 4 (ID = 2)
Control surface 1 of 1
Section 3 of 4 (ID = 1)
Control surface 1 of 1
Section 4 of 4 (ID = 0)
Control surface 1 of 1
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Control surface 1 of 1
Section 2 of 3 (ID = 1)
Control surface 1 of 1
Section 3 of 3 (ID = 0)
Control surface 1 of 1
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Control surface 1 of 1
Section 2 of 2 (ID = 1)
Control surface 1 of 1
ok
test_TargetCL (test_cart3d.TestCart3D.test_TargetCL) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Wing1, index = 1
Name = trailingEdge, index = 2
Writing FAST file ....
Finished writing FAST file
Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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
70000DD1C000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000DD1C000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
10F2ABE00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
10F2ABE00 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
10F2ABE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
10F2ABE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000DD1C000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000DD1C000 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
10F2ABE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
10F2ABE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000DD1C000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000DD1C000 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
10F2ABE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
10F2ABE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000DD1C000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000DD1C000 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:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
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:62030)
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:62030)
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: 0.259776
Creating surface mesh ...
Surface mesh seconds: 0.053102
Recovering boundaries...
Boundary recovery seconds: 0.16487
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.078723
Recovering Delaunayness...
Delaunay recovery seconds: 0.081652
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: 3.63755
Smoothing vertices...
Mesh smoothing seconds: 3.68719
Improving mesh...
Mesh improvement seconds: 0.078543
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.022713
Total running seconds: 8.06515
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: 0.261656
Creating surface mesh ...
Surface mesh seconds: 0.056473
Recovering boundaries...
Boundary recovery seconds: 0.181279
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.070538
Recovering Delaunayness...
Delaunay recovery seconds: 0.084381
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: 3.32631
Smoothing vertices...
Mesh smoothing seconds: 3.13392
Improving mesh...
Mesh improvement seconds: 0.069184
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.020895
Total running seconds: 7.20578
Statistics:
Input points: 14233
Input facets: 28454
Input segments: 42681
Input holes: 2
Input regions: 0
Mesh points: 33078
Mesh tetrahedra: 159812
Mesh faces: 333851
Mesh faces on exterior boundary: 28454
Mesh faces on input facets: 28454
Mesh edges on input segments: 42681
Steiner points inside domain: 18845
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM4/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_cythonNMLError (test_fun3d.TestFUN3D.test_cythonNMLError) ... ok
test_cythonNMLReentrance (test_fun3d.TestFUN3D.test_cythonNMLReentrance) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/fun3dAIM6/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
ok
test_invalidBoundary (test_fun3d.TestFUN3D.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_fun3d.TestFUN3D.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_fun3d.TestFUN3D.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5079, elements - 10146
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5079, elements - 10146
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14233, elements - 28454
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ...
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - alowervar
Design Variable name - auppervar
Design Variable name - classvar
Design Variable name - ztailvar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - avar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 54 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 54 54
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 12 26
AFLR2 IG : Nodes, Faces = 24 50
AFLR2 IG : Nodes, Faces = 36 74
AFLR2 IG : Nodes, Faces = 48 98
AFLR2 IG : Nodes, Faces = 52 106
AFLR2 IG : Nodes, Faces = 53 108
AFLR2 IG : Nodes, Faces = 54 110
AFLR2 IG : Nodes, Faces = 58 110
AFLR2 IG : Nodes, Faces = 54 54
AFLR2 : CPU Time = 0.000 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 54 54
AFLR2 GG : Nodes, Faces = 100 146
AFLR2 GG : Nodes, Faces = 122 190
AFLR2 GG : Nodes, Faces = 138 222
AFLR2 GG : Nodes, Faces = 153 252
AFLR2 GG : Nodes, Faces = 168 282
AFLR2 GG : Nodes, Faces = 180 306
AFLR2 GG : Nodes, Faces = 192 330
AFLR2 GG : Nodes, Faces = 201 348
AFLR2 GG : Nodes, Faces = 210 366
AFLR2 GG : Nodes, Faces = 216 378
AFLR2 GG : Nodes, Faces = 221 388
AFLR2 GG : Nodes, Faces = 224 394
AFLR2 GG : Nodes, Faces = 225 396
AFLR2 : CPU Time = 0.001 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 225 396
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 225
Number of elements = 450
Number of tris = 396
Number of quad = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
ok
test_all (test_refine.TestREFINE.test_all) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1602
Number of elements = 8758
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7518
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_box_volume (test_refine.TestREFINE.test_box_volume) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2600
Number of elements = 13864
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = boxhole, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1071
Number of elements = 5705
Number of triangles = 998
Number of quadrilatarals = 0
Number of tetrahedrals = 4707
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 15544
Number of elements = 89331
Number of triangles = 4632
Number of quadrilatarals = 0
Number of tetrahedrals = 84699
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_fun3d (test_refine.TestREFINE.test_fun3d) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = farfield, index = 1
Name = box, index = 2
Name = sphere, index = 3
Name = boxhole, index = 4
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1602
Number of elements = 8758
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7518
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_refine.TestREFINE.test_inputs) ... ok
test_phase (test_refine.TestREFINE.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 438
Number of elements = 2179
Number of triangles = 644
Number of quadrilatarals = 0
Number of tetrahedrals = 1535
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = farfield, index = 1
Name = sphere, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 936
Number of elements = 4999
Number of triangles = 758
Number of quadrilatarals = 0
Number of tetrahedrals = 4241
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 3 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 8 Faces
EGADS : Body 0 has 15 Edges
EGADS : Body 0 has 8 Loops
EGADS : Body 0 has 9 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 8 Faces
EGADS : Body 1 has 15 Edges
EGADS : Body 1 has 8 Loops
EGADS : Body 1 has 9 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 2 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 2 Loops
EGADS : Body 2 has 2 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4 5
EGADS : 2 Yes 0 0 1 1 1 1 3 4 6
EGADS : 3 Yes 0 0 1 1 1 1 2 4 7
EGADS : 4 Yes 0 0 1 1 1 1 2 3
EGADS : 5 Yes 0 0 1 1 1 1 6 7 8
EGADS : 6 Yes 0 0 1 1 1 2 5 7 8
EGADS : 7 Yes 0 0 1 1 1 3 5 6 8
EGADS : 8 Yes 0 0 1 1 1 5 6 7
EGADS : 9 Yes 1 0 1 0 10 10 11 12 13
EGADS : 10 Yes 1 0 1 0 10 9 11 12 14
EGADS : 11 Yes 1 0 1 0 10 9 10 12 15
EGADS : 12 Yes 1 0 1 0 10 9 10 11
EGADS : 13 Yes 1 0 1 0 10 9 14 15 16
EGADS : 14 Yes 1 0 1 0 10 10 13 15 16
EGADS : 15 Yes 1 0 1 0 10 11 13 14 16
EGADS : 16 Yes 1 0 1 0 10 13 14 15
EGADS : 17 Yes 2 0 1 NA NA 18
EGADS : 18 Yes 2 0 1 NA NA 17
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 4 -3 -2
EGADS : 2 3 7 -6 -5
EGADS : 3 6 9 -1 -8
EGADS : 4 -4 -9 -7
EGADS : 5 -10 2 11 -12
EGADS : 6 -11 5 13 -14
EGADS : 7 -13 8 10 -15
EGADS : 8 12 14 15
EGADS : 9 16 19 -18 -17
EGADS : 10 18 22 -21 -20
EGADS : 11 21 24 -16 -23
EGADS : 12 -19 -24 -22
EGADS : 13 -25 17 26 -27
EGADS : 14 -26 20 28 -29
EGADS : 15 -28 23 25 -30
EGADS : 16 27 29 30
EGADS : 17 -31 -32 33 34
EGADS : 18 -35 -34 36 32
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 4 -3 -2
EGADS : 2 Yes 3 7 -6 -5
EGADS : 3 Yes 6 9 -1 -8
EGADS : 4 Yes -4 -9 -7
EGADS : 5 Yes -10 2 11 -12
EGADS : 6 Yes -11 5 13 -14
EGADS : 7 Yes -13 8 10 -15
EGADS : 8 Yes 12 14 15
EGADS : 9 Yes 16 19 -18 -17
EGADS : 10 Yes 18 22 -21 -20
EGADS : 11 Yes 21 24 -16 -23
EGADS : 12 Yes -19 -24 -22
EGADS : 13 Yes -25 17 26 -27
EGADS : 14 Yes -26 20 28 -29
EGADS : 15 Yes -28 23 25 -30
EGADS : 16 Yes 27 29 30
EGADS : 17 Yes -31 -32 33 34
EGADS : 18 Yes -35 -34 36 32
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 5
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 5 1 2 6
EGADS : 6 0 Yes 5 6 1 2 3
EGADS : 7 0 Yes 4 6 1 2 4
EGADS : 8 0 Yes 5 1 1 3 7
EGADS : 9 0 Yes 6 2 1 3 4
EGADS : 10 0 Yes 1 7 1 5 7
EGADS : 11 0 Yes 3 8 1 5 6
EGADS : 12 0 Yes 7 8 1 5 8
EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 DEGEN 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 DEGEN 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 DEGEN 19 19 - 18
EGADS : 36 2 DEGEN 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 3.77246052 0 0.00459131419
EGADS : 2 Yes 5.90487498 7.07106781 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.0824829 7.07106781 0.123425948
EGADS : 5 Yes 3.77001182 0 0
EGADS : 6 Yes 5.90282524 7.07106781 0
EGADS : 7 Yes 5.90487498 0 0
EGADS : 8 Yes 4.0824829 0 0.123425948
EGADS : 9 Yes 5.90282524 0 0
EGADS : 10 Yes 11.5089842 0 0.00183652568
EGADS : 11 Yes 12.36195 2.82842712 0
EGADS : 12 Yes 10 0 0
EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791
EGADS : 14 Yes 11.5080047 0 0
EGADS : 15 Yes 12.3611301 2.82842712 0
EGADS : 16 Yes 12.36195 0 0
EGADS : 17 Yes 11.6329932 0 0.0493703791
EGADS : 18 Yes 12.3611301 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 15.6122
AFLR4 : Abs Min Surf Spacing = 0.00222722
AFLR4 : Min Surf Spacing = 0.00445444
AFLR4 : Max Surf Spacing = 0.0890888
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 FARFIELD
AFLR4 : 18 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 12428
AFLR43 : Nodes = 6220
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6220 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 Solid
UG3 : 12 Solid
UG3 : 13 Solid
UG3 : 14 Solid
UG3 : 15 Solid
UG3 : 16 Solid
UG3 : 17 FarField
UG3 : 18 FarField
AFLR3 : CPU Time = 0.020 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6220 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1246 7333
AFLR3 IG : Nodes, Elements = 2492 16261
AFLR3 IG : Nodes, Elements = 3738 25021
AFLR3 IG : Nodes, Elements = 4984 34304
AFLR3 IG : Nodes, Elements = 6227 43518
AFLR3 IG : Nodes, Elements = 6227 43440
AFLR3 IG : Nodes, Elements = 6227 43474
AFLR3 IG : Nodes, Elements = 6227 43437
AFLR3 IG : Nodes, Elements = 6220 26107
AFLR3 IG : Nodes, Elements = 6220 26133
AFLR3 IG : Nodes, Elements = 6220 21538
AFLR3 IG : Nodes, Elements = 6220 19141
AFLR3 : CPU Time = 0.204 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6220 19141
AFLR3 GG : Nodes, Elements = 9092 27970
AFLR3 GG : Nodes, Elements = 9092 39349
AFLR3 GG : Nodes, Elements = 9092 36380
AFLR3 GG : Nodes, Elements = 9092 34923
AFLR3 GG : Nodes, Elements = 11659 42981
AFLR3 GG : Nodes, Elements = 11659 53807
AFLR3 GG : Nodes, Elements = 11659 50702
AFLR3 GG : Nodes, Elements = 11659 49815
AFLR3 GG : Nodes, Elements = 14477 58553
AFLR3 GG : Nodes, Elements = 14477 70855
AFLR3 GG : Nodes, Elements = 14477 67465
AFLR3 GG : Nodes, Elements = 14477 66533
AFLR3 GG : Nodes, Elements = 17443 75634
AFLR3 GG : Nodes, Elements = 17443 88707
AFLR3 GG : Nodes, Elements = 17443 85026
AFLR3 GG : Nodes, Elements = 17443 84166
AFLR3 GG : Nodes, Elements = 20625 93912
AFLR3 GG : Nodes, Elements = 20625 107483
AFLR3 GG : Nodes, Elements = 20625 103837
AFLR3 GG : Nodes, Elements = 20625 103014
AFLR3 GG : Nodes, Elements = 23983 113245
AFLR3 GG : Nodes, Elements = 23983 127691
AFLR3 GG : Nodes, Elements = 23983 123762
AFLR3 GG : Nodes, Elements = 23983 122939
AFLR3 GG : Nodes, Elements = 27471 133562
AFLR3 GG : Nodes, Elements = 27471 148246
AFLR3 GG : Nodes, Elements = 27471 144367
AFLR3 GG : Nodes, Elements = 27471 143483
AFLR3 GG : Nodes, Elements = 31049 154330
AFLR3 GG : Nodes, Elements = 31049 169629
AFLR3 GG : Nodes, Elements = 31049 165573
AFLR3 GG : Nodes, Elements = 31049 164719
AFLR3 GG : Nodes, Elements = 34642 175591
AFLR3 GG : Nodes, Elements = 34642 190772
AFLR3 GG : Nodes, Elements = 34642 186857
AFLR3 GG : Nodes, Elements = 34642 186049
AFLR3 GG : Nodes, Elements = 38204 196811
AFLR3 GG : Nodes, Elements = 38204 211769
AFLR3 GG : Nodes, Elements = 38204 208011
AFLR3 GG : Nodes, Elements = 38204 207203
AFLR3 GG : Nodes, Elements = 41735 217867
AFLR3 GG : Nodes, Elements = 41735 232734
AFLR3 GG : Nodes, Elements = 41735 228893
AFLR3 GG : Nodes, Elements = 41735 228199
AFLR3 GG : Nodes, Elements = 45118 238407
AFLR3 GG : Nodes, Elements = 45118 252771
AFLR3 GG : Nodes, Elements = 45118 249083
AFLR3 GG : Nodes, Elements = 45118 248399
AFLR3 GG : Nodes, Elements = 48432 258383
AFLR3 GG : Nodes, Elements = 48432 272398
AFLR3 GG : Nodes, Elements = 48432 268767
AFLR3 GG : Nodes, Elements = 48432 268040
AFLR3 GG : Nodes, Elements = 51632 277673
AFLR3 GG : Nodes, Elements = 51632 291124
AFLR3 GG : Nodes, Elements = 51632 287737
AFLR3 GG : Nodes, Elements = 51632 287138
AFLR3 GG : Nodes, Elements = 54742 296489
AFLR3 GG : Nodes, Elements = 54742 309545
AFLR3 GG : Nodes, Elements = 54742 306294
AFLR3 GG : Nodes, Elements = 54742 305700
AFLR3 GG : Nodes, Elements = 57753 314750
AFLR3 GG : Nodes, Elements = 57753 327393
AFLR3 GG : Nodes, Elements = 57753 324205
AFLR3 GG : Nodes, Elements = 57753 323671
AFLR3 GG : Nodes, Elements = 60589 332185
AFLR3 GG : Nodes, Elements = 60589 344195
AFLR3 GG : Nodes, Elements = 60589 341132
AFLR3 GG : Nodes, Elements = 60589 340678
AFLR3 GG : Nodes, Elements = 63303 348823
AFLR3 GG : Nodes, Elements = 63303 360078
AFLR3 GG : Nodes, Elements = 63303 357259
AFLR3 GG : Nodes, Elements = 63303 356861
AFLR3 GG : Nodes, Elements = 65821 364418
AFLR3 GG : Nodes, Elements = 65821 375019
AFLR3 GG : Nodes, Elements = 65821 372315
AFLR3 GG : Nodes, Elements = 65821 371973
AFLR3 GG : Nodes, Elements = 68056 378682
AFLR3 GG : Nodes, Elements = 68056 387933
AFLR3 GG : Nodes, Elements = 68056 385584
AFLR3 GG : Nodes, Elements = 68056 385301
AFLR3 GG : Nodes, Elements = 69951 390988
AFLR3 GG : Nodes, Elements = 69951 398948
AFLR3 GG : Nodes, Elements = 69951 396934
AFLR3 GG : Nodes, Elements = 69951 396704
AFLR3 GG : Nodes, Elements = 71446 401190
AFLR3 GG : Nodes, Elements = 71446 407532
AFLR3 GG : Nodes, Elements = 71446 405836
AFLR3 GG : Nodes, Elements = 71446 405665
AFLR3 GG : Nodes, Elements = 72588 409091
AFLR3 GG : Nodes, Elements = 72588 414051
AFLR3 GG : Nodes, Elements = 72588 412698
AFLR3 GG : Nodes, Elements = 72588 412555
AFLR3 GG : Nodes, Elements = 73412 415028
AFLR3 GG : Nodes, Elements = 73412 418465
AFLR3 GG : Nodes, Elements = 73412 417560
AFLR3 GG : Nodes, Elements = 73412 417491
AFLR3 GG : Nodes, Elements = 73970 419165
AFLR3 GG : Nodes, Elements = 73970 421515
AFLR3 GG : Nodes, Elements = 73970 420850
AFLR3 GG : Nodes, Elements = 73970 420801
AFLR3 GG : Nodes, Elements = 74329 421878
AFLR3 GG : Nodes, Elements = 74329 423409
AFLR3 GG : Nodes, Elements = 74329 422967
AFLR3 GG : Nodes, Elements = 74329 422934
AFLR3 GG : Nodes, Elements = 74527 423528
AFLR3 GG : Nodes, Elements = 74527 424406
AFLR3 GG : Nodes, Elements = 74527 424145
AFLR3 GG : Nodes, Elements = 74527 424123
AFLR3 GG : Nodes, Elements = 74619 424399
AFLR3 GG : Nodes, Elements = 74619 424805
AFLR3 GG : Nodes, Elements = 74619 424686
AFLR3 GG : Nodes, Elements = 74619 424681
AFLR3 GG : Nodes, Elements = 74657 424795
AFLR3 GG : Nodes, Elements = 74657 424951
AFLR3 GG : Nodes, Elements = 74657 424897
AFLR3 GG : Nodes, Elements = 74672 424942
AFLR3 GG : Nodes, Elements = 74672 425006
AFLR3 GG : Nodes, Elements = 74672 424985
AFLR3 GG : Nodes, Elements = 74672 424986
AFLR3 GG : Nodes, Elements = 74673 424989
AFLR3 GG : Nodes, Elements = 74673 424992
AFLR3 GG : Nodes, Elements = 74673 424991
AFLR3 GG : Nodes, Elements = 74696 425060
AFLR3 GG : Nodes, Elements = 74696 425133
AFLR3 GG : Nodes, Elements = 74696 425114
AFLR3 GG : Nodes, Elements = 74696 425117
AFLR3 GG : Nodes, Elements = 74700 425129
AFLR3 GG : Nodes, Elements = 74700 425145
AFLR3 GG : Nodes, Elements = 74700 425140
AFLR3 GG : Nodes, Elements = 74702 425146
AFLR3 GG : Nodes, Elements = 74702 425155
AFLR3 GG : Nodes, Elements = 74702 425152
AFLR3 GG : Nodes, Elements = 74702 425150
AFLR3 : CPU Time = 6.104 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 = 1.926 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 = 0.068 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 = 8.937 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Ang = 1.137 170.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 61
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 414152
UG3 : Min Vol = 6.36e-10
UG3 : Average Vol = 5.12
UG3 : Total-Tet-Vol = 2.12e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 414152
UG3 : Min, Max Q = 0.223 1
UG3 : Average Q = 0.859
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 73007
Number of elements = 426580
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 414152
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 2
Design_Variable name - plateLength
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - plateWidth
Number of design variable relations - 0
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 1
Design_Variable name - thick1
Design_Variable_Relation name - thick1
Number of design variable relations - 1
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing design variable cards
Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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)
70000DD1C000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
10F2ABE00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000DD1C000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
10F2ABE00 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 144 tests in 807.546s
OK (skipped=15)
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
(make -C cCAPS -f avlTest.make)
make[1]: `avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[1]: `awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[1]: `frictionTest' is up to date.
(make -C cCAPS -f fun3d.make)
make[1]: Nothing to be done for `fun3d'.
(make -C cCAPS -f hsm.make)
make[1]: `hsm' is up to date.
(make -C cCAPS -f interferenceTest.make)
make[1]: `interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[1]: `msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[1]: `mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[1]: `pointwiseTest' is up to date.
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests
All tests pass!
=================================================
=================================================
(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Using python : /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/ESP_venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 3 (ID = 0)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 2)
CXtot 0.0006119078685748102
CYtot -6.295467348382128e-15
CZtot -0.3012861394885953
Cltot -4.784258926526785e-14
Cmtot -0.1945055953450382
Cntot -2.338191252215186e-15
Cl'tot -4.787610967125373e-14
Cn'tot -1.502866821492718e-15
CLtot 0.3012509314150635
CDtot 0.004646353488232475
CDvis 0.0
CLff 0.3009503023520388
CYff -7.723329422293541e-15
CDind 0.004646353488232475
CDff 0.004968969500907922
e 0.9669902146157789
StripForces
Wing cl = [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.3101221284189, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422921, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408]
Wing cd = [-0.004234137763162, -0.004494543653192, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946409, 0.000511459807839, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080993, -0.0007386538944077, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653162, -0.004234137764545]
real 0m2.155s
user 0m1.069s
sys 0m0.635s
+ 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/7.8/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/7.8/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 0m5.824s
user 0m5.125s
sys 0m0.330s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837932402995744
Cd = 0.0077758580442312715
Cm = 0.005262576090327783
real 0m6.499s
user 0m5.049s
sys 0m0.637s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
XLE: 1.571946 -3.872983 0.249728
XTE: 2.536563 -3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 2, units m
XLE: 0.000000 0.000000 0.000000
XTE: 1.614012 0.000000 0.002015
Chord: 1.614013
Arc: 3.308635
T/C: 0.127839
Type: Wing
Lifting Surface: Body = 3, units m
XLE: 1.571946 3.872983 0.249728
XTE: 2.536563 3.872983 0.335335
Chord: 0.968408
Arc: 1.985181
T/C: 0.155975
Type: Wing
Lifting Surface: Body = 4, units m
XLE: 5.484123 0.000000 1.468246
XTE: 6.210307 0.000915 1.468246
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 5, units m
XLE: 5.000000 0.000000 0.500000
XTE: 6.210307 0.001525 0.500000
Chord: 1.210308
Arc: 2.471195
T/C: 0.120035
Type: VTail
Lifting Surface: Body = 6, units m
XLE: 5.484123 -0.968246 0.500000
XTE: 6.210307 -0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Lifting Surface: Body = 7, units m
XLE: 5.484123 0.968246 0.500000
XTE: 6.210307 0.968246 0.500915
Chord: 0.726185
Arc: 1.482717
T/C: 0.120035
Type: HTail
Body of Revolution: Body = 8, units m
Arc: 0.000000
Diameter: 0.000000
Type: Fuse
Body of Revolution: Body = 9, units m
Arc: 3.714180
Diameter: 1.020621
Type: Fuse
Body of Revolution: Body = 10, units m
Arc: 2.771209
Diameter: 0.645497
Type: Fuse
Body of Revolution: Body = 11, units m
Arc: 1.013945
Diameter: 0.322749
Type: Fuse
Body of Revolution: Body = 12, units m
Arc: 0.101394
Diameter: 0.032275
Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
real 0m1.250s
user 0m0.842s
sys 0m0.296s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u tsfoil_PyTest.py -outLevel=0
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 0m1.089s
user 0m0.918s
sys 0m0.236s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m1.307s
user 0m1.158s
sys 0m0.473s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Name = Rib_Root_Point, index = 6
Name = Wing, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Getting mesh sizing parameters
Mesh sizing name - LeadingEdge
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes = 3793
Number of elements = 4001
Number of triangle elements = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes = 76
Number of elements = 55
Number of triangle elements = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes = 100
Number of elements = 73
Number of triangle elements = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes = 3970
Total number of elements = 4129
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
real 0m12.395s
user 0m25.950s
sys 0m3.060s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.022 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.010 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
real 0m1.334s
user 0m1.309s
sys 0m0.461s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing Tecplot file ....
Finished writing Tecplot file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing ugrid file ....
Finished writing ugrid file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 x86_64
AFLR4 : Compile Date 04/23/24 @ 11:49AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 150173
Number of elements = 449915
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 214483
Number of pyramids = 425
Number of prisms = 220627
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m19.859s
user 0m18.838s
sys 0m0.995s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3139
Total number of elements = 6266
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.037862
Creating surface mesh ...
Surface mesh seconds: 0.011527
Recovering boundaries...
Boundary recovery seconds: 0.103589
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.013156
Suppressing Steiner points ...
Steiner suppression seconds: 4.3e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.016277
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: 0.965617
Smoothing vertices...
Mesh smoothing seconds: 0.644922
Improving mesh...
Mesh improvement seconds: 0.010969
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.003882
Total running seconds: 1.80829
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 0m10.514s
user 0m10.135s
sys 0m0.498s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 04/23/24 @ 11:49AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.021 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 = 0.045 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 = 0.018 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 49.3184| 90|
| CV Face Area Aspect Ratio| 1.00035| 33.4982|
| CV Sub-Volume Ratio| 1.00001| 7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11153| 1/1.00| 10|
| 1| 2702| 1/4.13| 7.38309|
| 2| 549| 1/4.92| 4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.1411e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.1151e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.1099e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.1115e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.1102e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.1007e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.1040e-01| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.1080e-01| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.1091e-01| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.1105e-01| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22124| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_su2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_su2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+
--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.072253 Cd = -0.01151
Cmz = 0.070975
Cx = -0.01151 Cy = 0.072253
Pressure Contribution
Cl_p = 0.072253 Cd_p = -0.01151
Cmz_p = 0.070975
Cx_p = -0.01151 Cy_p = 0.072253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m4.133s
user 0m3.291s
sys 0m0.854s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
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 0m1.466s
user 0m1.062s
sys 0m0.425s
+ 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/7.8/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/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = Root_Point, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = WingSurface, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Edge, index = 1
Name = Body, index = 2
Name = Root, index = 3
Name = Wing, index = 4
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 96
Number of elements = 77
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 77
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 97
Combined Number of elements = 78
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 77
Getting vortex lattice surface data
VLM surface name - WingSurface
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 96
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Body
Property name - Edge
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - PointConstraint
No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Root
No "groupName" specified for Connection tuple Root!
Looking for automatic connections from the use of capsConnectLink for Root
8 automatic connections were made for capsConnect Root (node id 97)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Flutter
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aero card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing material cards
Writing property cards
Writing unsteady aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
real 0m1.721s
user 0m1.311s
sys 0m0.512s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results mass properties.....
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 1159
Number of elements = 798
Number of triangle elements = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes = 1159
Total number of elements = 798
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Ribs_and_Spars, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1159
Number of elements = 798
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 798
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - Ribs_and_Spars
No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Area 3.428666259747
Mass 5383.006027803
Centroid [1.222256036874, 0.1634981473778, -4.234492548615e-11]
CG [1.222256036874, 0.1634981473778, -4.234574416087e-11]
Ixx 22133.97306033
Iyy 23448.30046709
Izz 1389.213122582
Ixy 164.2055275657
Ixz -7.454849830627e-06
Iyz 1.707682983295e-06
I [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454849830627e-06, 1.707682983295e-06]
II [[22133.97306033, -164.2055275657, 7.454849830627e-06], [-164.2055275657, 23448.30046709, -1.707682983295e-06], [7.454849830627e-06, -1.707682983295e-06, 1389.213122582]]
real 0m7.254s
user 0m11.306s
sys 0m5.119s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Creating HSM BEM
Getting quads for BEM!
Number of nodal coordinates = 81
Number of elements = 96
Elemental Tria3 = 0
Elemental Quad4 = 64
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file
Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
Matrix Non-zero Entries = 5741
Converging HSM equation system ...
iter dr dd dp rlx max
1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00)
1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00)
2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00)
2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00)
3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00)
4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00)
5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00)
6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00)
7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
Converging e1,e2 vectors ...
it = 1 de = 0.691E-03 rlx = 1.000 ( 45 )
it = 2 de = 0.404E-04 rlx = 1.000 ( 9 )
it = 3 de = 0.142E-07 rlx = 1.000 ( 46 )
it = 4 de = 0.521E-11 rlx = 1.000 ( 62 )
Calculating strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat
real 0m1.515s
user 0m1.283s
sys 0m0.211s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Objective
---------
-21.56250 dimensionless
Variables
---------
x : 1.62500 [-] The X variable
y : 1.37500 [-] The Y variable
Constants
---------
c : 3 [-] A constant
c2 : 2 [-] A constant
Sensitivities
-------------
c : + 0.46957 A constant
c2 : - 0.22338 A constant
Solve Report
------------
Solve Method : Quadratic Program
Classification : Convex
Solver : cvxopt
real 0m43.014s
user 0m2.513s
sys 0m0.430s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
awave
Cart3D
Mystran
=================================================
All tests pass!
=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64
+ mkdir -p /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/test/plugs
+ cd /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/test/plugs
+ find /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
data/Plugs/plugs0a.csm
data/Plugs/plugs0b.csm
data/Plugs/plugs0c.csm
data/Plugs/plugs0d.csm
total 51928
-rw-r--r-- 1 jenkins staff 1.2M May 30 12:24 ASTRO.D01
-rw-r--r-- 1 jenkins staff 277K May 30 12:24 ASTRO.IDX
-rwxr-xr-x 1 jenkins staff 131K May 30 12:25 ESPxddm
-rwxr-xr-x 1 jenkins staff 229K May 30 12:24 Slugs
-rwxr-xr-x 1 jenkins staff 102K May 30 12:24 TestFit
-rwxr-xr-x 1 jenkins staff 1.8M May 30 12:24 avl
-rwxr-xr-x 1 jenkins staff 50K May 30 12:25 cart3dTest
-rwxr-xr-x 1 jenkins staff 50K May 30 12:22 egads2cart
-rwxr-xr-x 1 jenkins staff 86K May 30 12:25 egads2cgt
-rwxr-xr-x 1 jenkins staff 383K May 30 12:25 friction
-rwxr-xr-x 1 jenkins staff 8.9M May 30 12:24 mastros.exe
-rwxr-xr-x 1 jenkins staff 2.2M May 30 12:24 mses
-rwxr-xr-x 1 jenkins staff 2.5M May 30 12:24 mset
-rwxr-xr-x 1 jenkins staff 51K May 30 12:24 phaseUtil
-rw-r--r-- 1 jenkins staff 1.6K May 30 12:28 pod.egads
-rw-r--r-- 1 jenkins staff 0B May 30 12:28 port7681.jrnl
-rwxr-xr-x 1 jenkins staff 1.2M May 30 12:24 pplot
-rwxr-xr-x 1 jenkins staff 1.2M May 30 12:24 pxplot
-rwxr-xr-x 1 jenkins staff 84K May 30 12:23 sensCSM
-rwxr-xr-x 1 jenkins staff 224K May 30 12:23 serveCSM
-rwxr-xr-x 1 jenkins staff 192K May 30 12:23 serveESP
-rwxr-xr-x 1 jenkins staff 68K May 30 12:22 vCurvature
-rwxr-xr-x 1 jenkins staff 51K May 30 12:22 vGeom
-rwxr-xr-x 1 jenkins staff 52K May 30 12:22 vTess
-rwxr-xr-x 1 jenkins staff 2.3M May 30 12:22 vTesstatic
-rw-r--r-- 1 jenkins staff 195K May 30 12:28 wingMultiModel.bdf
-rwxr-xr-x 1 jenkins staff 1.8M May 30 12:24 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 5.416e-07, rmsbest= 6.132e-04, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 2, unclass= 0
Starting pass 3 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m14.098s
user 0m12.022s
sys 0m0.783s
++ set +x
data/Plugs/plugs0a passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 converged, dmax= 3.039e-07, rmsbest= 4.036e-02, reclass= 4562, unclass= 0
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 2.814e-07, rmsbest= 1.924e-03, reclass= 1033, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 4.494e-07, rmsbest= 5.920e-04, reclass= 473, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 5.366e-07, rmsbest= 7.097e-04, reclass= 17, unclass= 0
Starting pass 5 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m12.083s
user 0m14.741s
sys 0m0.177s
++ set +x
data/Plugs/plugs0b passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m43.665s
user 1m0.450s
sys 0m0.819s
++ set +x
data/Plugs/plugs0c passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped
===================================
PLUGS with 4562 points in the cloud
===================================
PLUGS phase1: match bounding boxes
PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
Pass 1 ran out of iterations, rmsbest= 1.677e-01, reclass= 4562, unclass= 554
Starting pass 2 (of 25) of phase2
Pass 2 converged, dmax= 4.016e-07, rmsbest= 6.330e-02, reclass= 1676, unclass= 0
Starting pass 3 (of 25) of phase2
Pass 3 converged, dmax= 1.881e-07, rmsbest= 8.736e-03, reclass= 791, unclass= 0
Starting pass 4 (of 25) of phase2
Pass 4 converged, dmax= 3.081e-07, rmsbest= 1.037e-03, reclass= 428, unclass= 0
Starting pass 5 (of 25) of phase2
Pass 5 converged, dmax= 5.816e-07, rmsbest= 7.097e-04, reclass= 109, unclass= 0
Starting pass 6 (of 25) of phase2
Phase2 passes converged because points are classified same as previous pass
==> Opening input journal file "/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64/EngSketchPad/data/Plugs/buildFinal.jrnl"
==> Closing input journal file
==> serveCSM completed successfully with no verification data
real 0m38.222s
user 0m56.117s
sys 0m0.951s
++ set +x
data/Plugs/plugs0d passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [macys_VM] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [macys_VM] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_Beta/7.8/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.8,ESP_ARCH=DARWIN64,buildnode=macys_VM #720'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS